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A

A - Static variable in enum org.orekit.orbits.OrbitType
Name for semi major axis.
a - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
final semi major axis.
a - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final semi major axis.
a0dp - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
original recovered semi major axis.
a0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original recovered semi major axis.
A2B - Static variable in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Constant for A → B diraction.
A3OVK2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
AbsoluteDate - Class in org.orekit.time
This class represents a specific instant in time.
AbsoluteDate() - Constructor for class org.orekit.time.AbsoluteDate
Create an instance with a default value (AbsoluteDate.J2000_EPOCH).
AbsoluteDate(String, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location (parsed from a string) in a time scale.
AbsoluteDate(DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(DateComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, int, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, Month, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(Date, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(AbsoluteDate, double) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an elapsed duration since to another instant.
AbsoluteDate(AbsoluteDate, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.
AbsoluteJacobiansMapper - Class in org.orekit.propagation.numerical
Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
AbsoluteJacobiansMapper(String, ParameterDriversList) - Constructor for class org.orekit.propagation.numerical.AbsoluteJacobiansMapper
Simple constructor.
AbsolutePartialDerivativesEquations - Class in org.orekit.propagation.numerical
Deprecated.
as of 11.1, this class is not used anymore
AbsolutePartialDerivativesEquations(String, NumericalPropagator) - Constructor for class org.orekit.propagation.numerical.AbsolutePartialDerivativesEquations
Deprecated.
Simple constructor.
AbsolutePVCoordinates - Class in org.orekit.utils
Position - Velocity - Acceleration linked to a date and a frame.
AbsolutePVCoordinates(Frame, AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Build from position, velocity, acceleration.
AbsolutePVCoordinates(Frame, AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Build from position and velocity.
AbsolutePVCoordinates(Frame, AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Build from frame, date and PVA coordinates.
AbsolutePVCoordinates(Frame, TimeStampedPVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Build from frame and TimeStampedPVCoordinates.
AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Multiplicative constructor
AbsolutePVCoordinates(AbsoluteDate, AbsolutePVCoordinates, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Subtractive constructor
AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Linear constructor
AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Linear constructor
AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Linear constructor
AbsolutePVCoordinates(Frame, AbsoluteDate, FieldVector3D<U>) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Builds a AbsolutePVCoordinates triplet from a FieldVector3D<Derivative>.
ABSORPTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive
Parameter name for absorption coefficient.
AbstractAlmanac - Class in org.orekit.propagation.analytical.gnss.data
Base class for GNSS almanacs.
AbstractAlmanac(double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Constructor.
AbstractAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers
Base class for phase ambiguity modifier.
AbstractAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier
Constructor.
AbstractAnalyticalGradientConverter - Class in org.orekit.propagation.analytical
Converter for analytical orbit propagator.
AbstractAnalyticalGradientConverter(AbstractAnalyticalPropagator, double, int) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter
Constructor.
AbstractAnalyticalMatricesHarvester - Class in org.orekit.propagation.analytical
Base class harvester between two-dimensional Jacobian matrices and analytical orbit propagator.
AbstractAnalyticalMatricesHarvester(AbstractAnalyticalPropagator, String, RealMatrix, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Simple constructor.
AbstractAnalyticalPropagator - Class in org.orekit.propagation.analytical
Common handling of Propagator methods for analytical propagators.
AbstractAnalyticalPropagator(AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Build a new instance.
AbstractBatchLSModel - Class in org.orekit.estimation.leastsquares
AbstractBatchLSModel(OrbitDeterminationPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, MatricesHarvester[], ModelObserver) - Constructor for class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Deprecated.
as of 11.1, replaced by [@link #AbstractBatchLSModel(OrbitDeterminationPropagatorBuilder[], List, ParameterDriversList, ModelObserver)}
AbstractBatchLSModel(OrbitDeterminationPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Constructor for class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Constructor.
AbstractBuilder<T extends AbstractBuilder<T>> - Class in org.orekit.files.ccsds.ndm
Abstract builder for all CCSDS Message files parsers/writers.
AbstractBuilder(IERSConventions, DataContext, AbsoluteDate, RangeUnitsConverter) - Constructor for class org.orekit.files.ccsds.ndm.AbstractBuilder
Complete constructor.
AbstractConstantThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion
This abstract class simply serve as a container for a constant thrust maneuver.
AbstractConstantThrustPropulsionModel(double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Generic constructor.
AbstractConstituentParser<T extends NdmConstituent<?,?>,P extends AbstractConstituentParser<T,?>> - Class in org.orekit.files.ccsds.utils.parsing
Parser for CCSDS messages.
AbstractConstituentParser(String, String, IERSConventions, boolean, DataContext, ParsedUnitsBehavior) - Constructor for class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Complete constructor.
AbstractCovarianceMatrixProvider - Class in org.orekit.estimation.sequential
Abstract provider handling a predefined initial covariance matrix.
AbstractCovarianceMatrixProvider(RealMatrix) - Constructor for class org.orekit.estimation.sequential.AbstractCovarianceMatrixProvider
Simple constructor.
AbstractCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss
Base class for cycle-slip detectors.
AbstractDetector<T extends AbstractDetector<T>> - Class in org.orekit.propagation.events
Common parts shared by several orbital events finders.
AbstractDetector(double, double, int, EventHandler<? super T>) - Constructor for class org.orekit.propagation.events.AbstractDetector
Build a new instance.
AbstractDragForceModel - Class in org.orekit.forces.drag
Base class for drag force models.
AbstractDragForceModel(Atmosphere) - Constructor for class org.orekit.forces.drag.AbstractDragForceModel
Constructor.
AbstractDualFrequencyCombination - Class in org.orekit.estimation.measurements.gnss
Base class for dual frequency combination of measurements.
AbstractDualFrequencyCombination(CombinationType, SatelliteSystem) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Constructor.
AbstractEncodedMessages - Class in org.orekit.gnss.metric.parser
Encoded messages as a sequence of bytes.
AbstractEncodedMessages() - Constructor for class org.orekit.gnss.metric.parser.AbstractEncodedMessages
 
AbstractEopLoader - Class in org.orekit.frames
Base class for EOP loaders.
AbstractEopLoader(String, DataProvidersManager, Supplier<TimeScale>) - Constructor for class org.orekit.frames.AbstractEopLoader
Simple constructor.
AbstractEphemerisMessage - Class in org.orekit.propagation.analytical.gnss.data
Base class for ephemeris-based navigation messages.
AbstractEphemerisMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Constructor.
AbstractFieldOfView - Class in org.orekit.geometry.fov
Abstract class representing a spacecraft sensor Field Of View.
AbstractFieldOfView(double) - Constructor for class org.orekit.geometry.fov.AbstractFieldOfView
Build a new instance.
AbstractForceModel - Class in org.orekit.forces
Base class for force models.
AbstractForceModel() - Constructor for class org.orekit.forces.AbstractForceModel
 
AbstractFrames - Class in org.orekit.frames
This class is an implementation of Frames that creates frames when they are first used and uses synchronization to ensure that each frame is only created once.
AbstractFrames(TimeScales, Supplier<Frame>) - Constructor for class org.orekit.frames.AbstractFrames
Simple constructor.
AbstractGaussianContribution - Class in org.orekit.propagation.semianalytical.dsst.forces
Common handling of DSSTForceModel methods for Gaussian contributions to DSST propagation.
AbstractGaussianContribution(String, double, ForceModel, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Build a new instance.
AbstractGaussianContribution.FieldFourierCjSjCoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
Compute the Cij and the Sij coefficients with field elements.
AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class handles the short periodic coefficients described in Danielson 2.5.3-26.
AbstractGaussianContribution.FieldIntegrableFunction<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
Internal class for numerical quadrature.
AbstractGaussianContribution.FieldSlot<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
Coefficients valid for one time slot.
AbstractGaussianContribution.FieldUijVijCoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
The Uij and Vij coefficients described by equations 2.5.3-(21) and 2.5.3-(22) from Danielson.
AbstractGaussianContribution.FourierCjSjCoefficients - Class in org.orekit.propagation.semianalytical.dsst.forces
Compute the Cij and the Sij coefficients.
AbstractGaussianContribution.GaussianShortPeriodicCoefficients - Class in org.orekit.propagation.semianalytical.dsst.forces
This class handles the short periodic coefficients described in Danielson 2.5.3-26.
AbstractGaussianContribution.GaussQuadrature - Class in org.orekit.propagation.semianalytical.dsst.forces
Class used to integrate a function of the orbital elements using the Gaussian quadrature rule to get the acceleration.
AbstractGaussianContribution.IntegrableFunction - Class in org.orekit.propagation.semianalytical.dsst.forces
Internal class for numerical quadrature.
AbstractGaussianContribution.Slot - Class in org.orekit.propagation.semianalytical.dsst.forces
Coefficients valid for one time slot.
AbstractGaussianContribution.UijVijCoefficients - Class in org.orekit.propagation.semianalytical.dsst.forces
The Uij and Vij coefficients described by equations 2.5.3-(21) and 2.5.3-(22) from Danielson.
AbstractGaussianContributionContext - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in AbstractGaussianContribution.
AbstractGenerator - Class in org.orekit.files.ccsds.utils.generation
Base class for both Key-Value Notation and eXtended Markup Language generators for CCSDS messages.
AbstractGenerator(Appendable, String, boolean) - Constructor for class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Simple constructor.
AbstractGradientConverter - Class in org.orekit.propagation.integration
Converter for states and parameters arrays.
AbstractGradientConverter(int) - Constructor for class org.orekit.propagation.integration.AbstractGradientConverter
Simple constructor.
AbstractIntegratedPropagator - Class in org.orekit.propagation.integration
Common handling of Propagator methods for both numerical and semi-analytical propagators.
AbstractIntegratedPropagator(ODEIntegrator, PropagationType) - Constructor for class org.orekit.propagation.integration.AbstractIntegratedPropagator
Build a new instance.
AbstractIntegratedPropagator.MainStateEquations - Interface in org.orekit.propagation.integration
Differential equations for the main state (orbit, attitude and mass).
AbstractJacobiansMapper - Class in org.orekit.propagation.integration
Base class for jacobian mapper.
AbstractJacobiansMapper(String, ParameterDriversList) - Constructor for class org.orekit.propagation.integration.AbstractJacobiansMapper
Simple constructor.
AbstractKalmanModel - Class in org.orekit.estimation.sequential
Abstract class defining the process model dynamics to use with a KalmanEstimator.
AbstractKalmanModel(List<OrbitDeterminationPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider, MatricesHarvester[]) - Constructor for class org.orekit.estimation.sequential.AbstractKalmanModel
Kalman process model constructor (package private).
AbstractKalmanModel(List<OrbitDeterminationPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider, MatricesHarvester[], PropagationType, PropagationType) - Constructor for class org.orekit.estimation.sequential.AbstractKalmanModel
Kalman process model constructor (package private).
AbstractLambdaMethod - Class in org.orekit.estimation.measurements.gnss
Base class for decorrelation/reduction engine for LAMBDA type methods.
AbstractLambdaMethod() - Constructor for class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Constructor.
AbstractListCrawler<T> - Class in org.orekit.data
Provider for data files defined in a list.
AbstractListCrawler(T...) - Constructor for class org.orekit.data.AbstractListCrawler
Build a data classpath crawler.
AbstractManeuverTriggers - Class in org.orekit.forces.maneuvers.trigger
Base class for triggers.
AbstractManeuverTriggers() - Constructor for class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Simple constructor.
AbstractMatricesHarvester - Class in org.orekit.propagation
Base harvester between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
AbstractMatricesHarvester(String, RealMatrix, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.AbstractMatricesHarvester
Simple constructor.
AbstractMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements
Abstract class handling measurements boilerplate.
AbstractMeasurement(AbsoluteDate, double, double, double, List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement
Simple constructor for mono-dimensional measurements.
AbstractMeasurement(AbsoluteDate, double[], double[], double[], List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement
Simple constructor, for multi-dimensional measurements.
AbstractMeasurementBuilder<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation
Base class for measurements builders.
AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator, double, double, ObservableSatellite...) - Constructor for class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Simple constructor.
AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator, double[], double[], ObservableSatellite...) - Constructor for class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Simple constructor.
AbstractMessageParser<T> - Class in org.orekit.files.ccsds.utils.parsing
Parser for CCSDS messages.
AbstractMessageParser(String, String) - Constructor for class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Simple constructor.
AbstractMessageWriter<H extends Header,S extends Segment<?,?>,F extends NdmConstituent<H,S>> - Class in org.orekit.files.ccsds.utils.generation
Base class for Navigation Data Message (NDM) files.
AbstractMessageWriter(String, String, double, ContextBinding) - Constructor for class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Constructor used to create a new NDM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
AbstractMultipleShooting - Class in org.orekit.utils
Multiple shooting method using only constraints on state vectors of patch points (and possibly on epoch and integration time).
AbstractMultipleShooting(List<SpacecraftState>, List<NumericalPropagator>, List<AdditionalEquations>, double, double, String) - Constructor for class org.orekit.utils.AbstractMultipleShooting
AbstractMultipleShooting(List<SpacecraftState>, List<NumericalPropagator>, double, double, int, String) - Constructor for class org.orekit.utils.AbstractMultipleShooting
Simple Constructor.
AbstractNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Base class for GNSS navigation messages.
AbstractNavigationMessage(double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Constructor.
AbstractPropagator - Class in org.orekit.propagation
Common handling of Propagator methods for analytical propagators.
AbstractPropagator() - Constructor for class org.orekit.propagation.AbstractPropagator
Build a new instance.
AbstractPropagatorBuilder - Class in org.orekit.propagation.conversion
Base class for propagator builders.
AbstractPropagatorBuilder(Orbit, PositionAngle, double, boolean) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Build a new instance.
AbstractPropagatorBuilder(Orbit, PositionAngle, double, boolean, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Build a new instance.
AbstractPropagatorConverter - Class in org.orekit.propagation.conversion
Common handling of PropagatorConverter methods for propagators conversions.
AbstractPropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorConverter
Build a new instance.
AbstractRadiationForceModel - Class in org.orekit.forces.radiation
Base class for radiation force models.
AbstractRadiationForceModel(ExtendedPVCoordinatesProvider, double) - Constructor for class org.orekit.forces.radiation.AbstractRadiationForceModel
Default constructor.
AbstractRelativisticClockModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical measurements with relativistic clock correction.
AbstractRelativisticClockModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockModifier
Simple constructor.
AbstractRelativisticJ2ClockModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical measurements with relativistic J2 clock correction.
AbstractRelativisticJ2ClockModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractRelativisticJ2ClockModifier
Constructor for the Relativistic J2 Clock modifier.
AbstractScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation
Base implementation of Scheduler managing dates selection.
AbstractScheduler(MeasurementBuilder<T>, DatesSelector) - Constructor for class org.orekit.estimation.measurements.generation.AbstractScheduler
Simple constructor.
AbstractSelfFeedingLoader - Class in org.orekit.data
Abstract class that combines a DataProvidersManager with a supported names regular expression for DataProvidersManager.feed(String, DataLoader).
AbstractSelfFeedingLoader(String, DataProvidersManager) - Constructor for class org.orekit.data.AbstractSelfFeedingLoader
Create an abstract data loader that can feed itself.
AbstractShapiroBaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with Shapiro time delay.
AbstractShapiroBaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier
Simple constructor.
AbstractSingleFrequencyCombination - Class in org.orekit.estimation.measurements.gnss
Base class for single frequency combination of measurements.
AbstractSingleFrequencyCombination(CombinationType, SatelliteSystem) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Constructor.
AbstractTimeScales - Class in org.orekit.time
Abstract base class for TimeScales that implements some common functionality.
AbstractTimeScales() - Constructor for class org.orekit.time.AbstractTimeScales
Simple constructor.
AbstractWriter - Class in org.orekit.files.ccsds.section
Top level class for writing CCSDS message sections.
AbstractWriter(String, String) - Constructor for class org.orekit.files.ccsds.section.AbstractWriter
Simple constructor.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.DragForce
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.DragForce
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.ParametricAcceleration
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.ParametricAcceleration
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in interface org.orekit.forces.ForceModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.ForceModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.DeSitterRelativity
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.DeSitterRelativity
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.LenseThirringRelativity
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.LenseThirringRelativity
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.OceanTides
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.OceanTides
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.Relativity
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.Relativity
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SolidTides
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SolidTides
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.inertia.InertialForces
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.inertia.InertialForces
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.Maneuver
 
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.Maneuver
 
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.ECOM2
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.ECOM2
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Compute acceleration.
AccelerationModel - Interface in org.orekit.forces.empirical
Acceleration model used by empirical force.
accept(IntegerLeastSquareSolution[]) - Method in interface org.orekit.estimation.measurements.gnss.AmbiguityAcceptance
Check if one of the candidate solutions can be accepted.
accept(IntegerLeastSquareSolution[]) - Method in class org.orekit.estimation.measurements.gnss.SimpleRatioAmbiguityAcceptance
Check if one of the candidate solutions can be accepted.
accept(RotationOrder) - Method in interface org.orekit.files.ccsds.ndm.adm.AdmParser.RotationOrderConsumer
Consume a data.
accept(MessageParser<T>) - Method in class org.orekit.files.ccsds.utils.lexical.KvnLexicalAnalyzer
Parse a CCSDS Message.
accept(MessageParser<T>) - Method in interface org.orekit.files.ccsds.utils.lexical.LexicalAnalyzer
Parse a CCSDS Message.
accept(boolean) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.BooleanConsumer
Consume a boolean.
accept(BodyFacade) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CenterConsumer
Consume a body center.
accept(List<BodyFacade>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CenterListConsumer
Consume a body center.
accept(char) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CharConsumer
Consume a character.
accept(AbsoluteDate) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DateConsumer
Consume a date.
accept(double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DoubleConsumer
Consume a double.
accept(int, int, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DoublyIndexedDoubleConsumer
Consume a doubly indexed double.
accept(T) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.EnumConsumer
Consume an enum.
accept(List<T>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.EnumListConsumer
Consume an enum.
accept(FrameFacade) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.FrameConsumer
Consume a frame.
accept(int, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedDoubleConsumer
Consume an indexed double.
accept(int, String) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedStringConsumer
Consume an indexed string.
accept(int) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IntConsumer
Consume an integer.
accept(int[]) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IntegerArrayConsumer
Consume an array of integers.
accept(char, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.LabeledDoubleConsumer
Consume an indexed double.
accept(String) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.StringConsumer
Consume a string.
accept(List<String>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.StringListConsumer
Consume a list of strings.
accept(TimeSystem) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.TimeSystemConsumer
Consume a time system.
accept(List<Unit>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.UnitListConsumer
Consume a list of units.
accept(Vector3D) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.VectorConsumer
Consume a vector.
accept(MessageParser<T>) - Method in class org.orekit.files.ccsds.utils.lexical.XmlLexicalAnalyzer
Parse a CCSDS Message.
acceptComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer
Check if container is still accepting comments.
acceptStep(OrekitStepInterpolator, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Accept a step, triggering events and step handlers.
acceptStep(FieldAbstractAnalyticalPropagator<T>.FieldBasicStepInterpolator, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Accept a step, triggering events and step handlers.
AccuracyProvider - Interface in org.orekit.gnss.metric.messages.rtcm.ephemeris.utils
This interface represents an accuracy providerused to validate RTCM ephemeris messages.
AccurateFormatter - Class in org.orekit.utils
Formatter used to produce strings from data with high accuracy.
AdamsBashforthIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for AdamsBashforthIntegrator.
AdamsBashforthIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder
Build a new instance.
AdamsMoultonIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for AdamsMoultonIntegrator.
AdamsMoultonIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder
Build a new instance.
AdapterDetector - Class in org.orekit.propagation.events
Base class for adapting an existing detector.
AdapterDetector(EventDetector) - Constructor for class org.orekit.propagation.events.AdapterDetector
Build an adaptor wrapping an existing detector.
AdapterPropagator - Class in org.orekit.propagation.analytical
Orbit propagator that adapts an underlying propagator, adding differential effects.
AdapterPropagator(Propagator) - Constructor for class org.orekit.propagation.analytical.AdapterPropagator
Build a propagator from an underlying reference propagator.
AdapterPropagator.DifferentialEffect - Interface in org.orekit.propagation.analytical
Interface for orbit differential effects.
add(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Add a handler for variable size step.
add(T, FieldOrekitFixedStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Add a handler for fixed size step.
add(OrekitStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Add a handler for variable size step.
add(double, OrekitFixedStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Add a handler for fixed size step.
add(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Add the argument matrix with the current matrix.
add(ParameterDriver) - Method in class org.orekit.utils.ParameterDriversList
Add a driver.
addAccelerationModelValidAfter(AccelerationModel, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Add a AccelerationModel entry valid after a limit date.
addAccelerationModelValidBefore(AccelerationModel, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Add an AccelerationModel entry valid before a limit date.
addAdditionalDerivativesProvider(AdditionalDerivativesProvider) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Add a set of user-specified equations to be integrated along with the orbit propagation (author Shiva Iyer).
addAdditionalDerivativesProvider(AdditionalDerivativesProvider) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Add a provider for user-specified state derivatives to be integrated along with the orbit propagation.
addAdditionalDerivativesProvider(FieldAdditionalDerivativesProvider<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Add a provider for user-specified state derivatives to be integrated along with the orbit propagation.
addAdditionalEquations(AdditionalEquations) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
addAdditionalEquations(AdditionalEquations) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
addAdditionalEquations(FieldAdditionalEquations<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
addAdditionalState(String, T...) - Method in class org.orekit.propagation.FieldSpacecraftState
Add an additional state.
addAdditionalState(String, double...) - Method in class org.orekit.propagation.SpacecraftState
Add an additional state.
addAdditionalStateDerivative(String, T...) - Method in class org.orekit.propagation.FieldSpacecraftState
Add an additional state derivative.
addAdditionalStateDerivative(String, double...) - Method in class org.orekit.propagation.SpacecraftState
Add an additional state derivative.
addAdditionalStateProvider(AdditionalStateProvider) - Method in class org.orekit.propagation.AbstractPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in interface org.orekit.propagation.FieldPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(AdditionalStateProvider) - Method in interface org.orekit.propagation.Propagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAnglesData(CRD.AnglesMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of angles data.
addAppliedDCBS(AppliedDCBS) - Method in class org.orekit.gnss.clock.RinexClock
Add an applied differencial code bias corrections.
addAppliedPCVS(AppliedPCVS) - Method in class org.orekit.gnss.clock.RinexClock
Add an applied phase center variations.
addBeidouNavigationMessage(BeidouNavigationMessage) - Method in class org.orekit.gnss.navigation.RinexNavigation
Add a Beidou navigation message to the list.
addCelestialBodyLoader(String, CelestialBodyLoader) - Static method in class org.orekit.bodies.CelestialBodyFactory
Add a loader for celestial bodies.
addCelestialBodyLoader(String, CelestialBodyLoader) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Add a loader for celestial bodies.
addChild(OrphanFrame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame
Add a child.
addChild(OrphanFrame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame
Add a child.
addClockData(String, RinexClock.ClockDataLine) - Method in class org.orekit.gnss.clock.RinexClock
Add a clock data line to a specified receiver/satellite.
addClockDataType(RinexClock.ClockDataType) - Method in class org.orekit.gnss.clock.RinexClock
Add a clock data types.
addCodeBias(CodeBias) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
Add a code bias value for the current satellite.
addComment(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set comment for relative metadata.
addComment(String) - Method in class org.orekit.files.ccsds.ndm.NdmParser
Add comment.
addComment(String) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Add comment.
addComment(String) - Method in class org.orekit.gnss.clock.RinexClock
Add a comment line.
addComment(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Add a comment line.
addConstraint(int, int, double) - Method in class org.orekit.utils.AbstractMultipleShooting
Add a constraint on one component of one patch point.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in interface org.orekit.forces.ForceModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in interface org.orekit.forces.ForceModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute the contribution of the force model to the perturbing acceleration.
addContribution(BodiesElements, double[][], double[][]) - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Add the contribution of the wave to Stokes coefficients.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.maneuvers.Maneuver
Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.maneuvers.Maneuver
Compute the contribution of the force model to the perturbing acceleration.
addCovarianceMatrix(CartesianCovariance) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
Add a covariance matrix.
addData(TimeStampedAngularCoordinates) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemData
Add a data point.
addData(TimeStampedPVCoordinates, boolean) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
Add a data point.
addDataBlock(CRD.CRDDataBlock) - Method in class org.orekit.files.ilrs.CRD
Add a data block to the current list of data blocks.
addDefaultCelestialBodyLoader(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Add the default loaders for all predefined celestial bodies.
addDefaultCelestialBodyLoader(String, String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Add the default loaders for celestial bodies.
addDefaultCelestialBodyLoader(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Add the default loaders for all predefined celestial bodies.
addDefaultCelestialBodyLoader(String, String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Add the default loaders for celestial bodies.
addDefaultEOP1980HistoryLoaders(String, String, String, String, String) - Static method in class org.orekit.frames.FramesFactory
Add the default loaders EOP history (IAU 1980 precession/nutation).
addDefaultEOP1980HistoryLoaders(String, String, String, String, String, Supplier<TimeScale>) - Method in class org.orekit.frames.LazyLoadedEop
Add the default loaders EOP history (IAU 1980 precession/nutation).
addDefaultEOP1980HistoryLoaders(String, String, String, String, String) - Method in class org.orekit.frames.LazyLoadedFrames
Add the default loaders EOP history (IAU 1980 precession/nutation).
addDefaultEOP2000HistoryLoaders(String, String, String, String, String) - Static method in class org.orekit.frames.FramesFactory
Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).
addDefaultEOP2000HistoryLoaders(String, String, String, String, String, Supplier<TimeScale>) - Method in class org.orekit.frames.LazyLoadedEop
Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).
addDefaultEOP2000HistoryLoaders(String, String, String, String, String) - Method in class org.orekit.frames.LazyLoadedFrames
Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).
addDefaultOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add the default READERS for ocean tides.
addDefaultOceanTidesReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Add the default readers for ocean tides.
addDefaultPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add the default readers for gravity fields.
addDefaultPotentialCoefficientsReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Add the default readers for gravity fields.
addDefaultProviders() - Method in class org.orekit.data.DataProvidersManager
Add the default providers configuration.
addDefaultUTCTAIOffsetsLoaders() - Method in class org.orekit.time.LazyLoadedTimeScales
Add the default loaders for UTC-TAI offsets history files (both IERS and USNO).
addDefaultUTCTAIOffsetsLoaders() - Static method in class org.orekit.time.TimeScalesFactory
Add the default loaders for UTC-TAI offsets history files (both IERS and USNO).
addDragSensitiveValidAfter(DragSensitive, AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Add a DragSensitive entry valid after a limit date.
Using addDragSensitiveValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addDragSensitiveValidBefore(DragSensitive, AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Add a DragSensitive entry valid before a limit date.
Using addDragSensitiveValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
addEffect(AdapterPropagator.DifferentialEffect) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Add a differential effect.
addEntry(String, String) - Method in class org.orekit.files.ccsds.ndm.odm.UserDefined
Add a key/value entry.
addEOPHistoryLoader(IERSConventions, EOPHistoryLoader) - Static method in class org.orekit.frames.FramesFactory
Add a loader for Earth Orientation Parameters history.
addEOPHistoryLoader(IERSConventions, EOPHistoryLoader) - Method in class org.orekit.frames.LazyLoadedEop
Add a loader for Earth Orientation Parameters history.
addEOPHistoryLoader(IERSConventions, EOPHistoryLoader) - Method in class org.orekit.frames.LazyLoadedFrames
Add a loader for Earth Orientation Parameters history.
addEphemerisName(int, String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Adds an ephemeris name to the list.
addEventDate(AbsoluteDate) - Method in class org.orekit.propagation.events.DateDetector
Add an event date.
addEventDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldDateDetector
Add an event date.
addEventDetector(T) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Add an event detector.
addEventDetector(D) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Add an event detector.
addEventDetector(D) - Method in interface org.orekit.propagation.FieldPropagator
Add an event detector.
addEventDetector(EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Add an event detector.
addEventDetector(D) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Add an event detector.
addEventDetector(T) - Method in interface org.orekit.propagation.Propagator
Add an event detector.
addFilter(DataFilter) - Method in class org.orekit.data.FiltersManager
Add a data filter.
addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Add a force model to the global perturbation model.
addForceModel(ForceModel) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Add a force model to the global perturbation model.
addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Add a force model to the global perturbation model.
addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Add a force model.
addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Add a force model to the global perturbation model.
addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Add a force model to the global perturbation model.
addGalileoNavigationMessage(GalileoNavigationMessage) - Method in class org.orekit.gnss.navigation.RinexNavigation
Add a Galileo navigation message to the list.
addGlonassNavigationMessage(GLONASSNavigationMessage) - Method in class org.orekit.gnss.navigation.RinexNavigation
Add a Glonass navigation message to the list.
addGPSNavigationMessage(GPSNavigationMessage) - Method in class org.orekit.gnss.navigation.RinexNavigation
Add a GPS navigation message to the list.
addGridPoint(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient
Add a point to the interpolation grid.
addGridPoint(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Add a point to the interpolation grid.
addHandler(EventHandler<D>) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Add one handler to the managed handlers list.
addHandlers(EventHandler<D>...) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Add several handlers to the managed handlers list.
addInput(T) - Method in class org.orekit.data.AbstractListCrawler
Add an input to the supported list.
addIRNSSNavigationMessage(IRNSSNavigationMessage) - Method in class org.orekit.gnss.navigation.RinexNavigation
Add a IRNSS navigation message to the list.
AdditionalDerivativesProvider - Interface in org.orekit.propagation.integration
Provider for additional derivatives.
AdditionalEquations - Interface in org.orekit.propagation.integration
Deprecated.
as of 11.1, replaced by AdditionalDerivativesProvider
AdditionalEquationsAdapter - Class in org.orekit.propagation.integration
Deprecated.
must be removed in 12.0 when AdditionalEquations is removed
AdditionalEquationsAdapter(AdditionalEquations, Supplier<SpacecraftState>) - Constructor for class org.orekit.propagation.integration.AdditionalEquationsAdapter
Deprecated.
Simple constructor.
AdditionalParameters - Class in org.orekit.files.ccsds.ndm.cdm
Container for additional parameters data block.
AdditionalParameters() - Constructor for class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Simple constructor.
AdditionalParametersKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM additional parameters entries.
AdditionalParametersWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for additional parameters data block for CCSDS Conjunction Data Messages.
AdditionalStateProvider - Interface in org.orekit.propagation
This interface represents providers for additional state data beyond SpacecraftState.
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CartesianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CircularOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.EquinoctialOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, T, T[]) - Method in class org.orekit.orbits.FieldCartesianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, T, T[]) - Method in class org.orekit.orbits.FieldCircularOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, T, T[]) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, T, T[]) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, T, T[]) - Method in class org.orekit.orbits.FieldOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.KeplerianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.Orbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(T) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations
Add the contribution of the Kepler evolution.
addKeplerContribution(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of the Kepler evolution.
addManeuver(Maneuver) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Add a maneuver.
addMassDerivative(T) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations
Add the contribution of the flow rate (dm/dt).
addMassDerivative(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of the flow rate (dm/dt).
addMeasurement(ObservedMeasurement<?>) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Add a measurement.
addMeteoData(CRD.MeteorologicalMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of meteorological data.
addModifier(EstimationModifier<T>) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Add a modifier.
addModifier(EstimationModifier<T>) - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Add a modifier.
addModifier(EstimationModifier<T>) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Add a modifier.
addModifier(EstimationModifier<T>) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Add a modifier.
addNewSegment(List<SpacecraftState>, String, int, AngularDerivativesFilter) - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Injects pre-computed satellite states into this attitude ephemeris file object, returning the generated OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment that has been stored internally.
addNewSegment(List<SpacecraftState>) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
addNewSegment(List<SpacecraftState>, int) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
addNewSegment(List<SpacecraftState>, CelestialBody, int) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
addNewSegment(List<SpacecraftState>, CelestialBody, int, TimeScale) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
addNonKeplerianAcceleration(FieldVector3D<T>) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations
Add the contribution of an acceleration expressed in some inertial frame.
addNonKeplerianAcceleration(Vector3D) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of a non-Keplerian acceleration.
addObservation(Observation) - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock
Adds an observation data line.
addObservation(ObservationType, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock
Adds an observation data line.
addObserver(int, String, MessageObserver) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Add an observer for an encoded messages.
addObserver(int, MessageObserver) - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor
Add an observer for encoded messages.
addObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver
Add an observer for this driver.
addOccultingBody(ExtendedPVCoordinatesProvider, double) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Add a new occulting body.
addOceanTidesReader(OceanTidesReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add a reader for ocean tides.
addOceanTidesReader(OceanTidesReader) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Add a reader for ocean tides.
addOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Add an offset from the instance.
addOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Add an offset from the instance.
addParameterDriver(ParameterDriver) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Add a parameter driver.
addParticipant(int, String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Adds a participant to the list.
addPhaseBias(PhaseBias) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Add a phase bias value for the current satellite.
addPoint(AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic
Add a fitting point.
addPotentialCoefficientsReader(PotentialCoefficientsReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add a reader for gravity fields.
addPotentialCoefficientsReader(PotentialCoefficientsReader) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Add a reader for gravity fields.
addPropagationConfiguration(OrbitDeterminationPropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Add a propagation configuration.
addPropagationConfiguration(DSSTPropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder
Add a propagation configuration.
addPropagator(Propagator) - Method in class org.orekit.estimation.measurements.generation.Generator
Add a propagator.
addProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager
Add a data provider to the supported list.
addQZSSNavigationMessage(QZSSNavigationMessage) - Method in class org.orekit.gnss.navigation.RinexNavigation
Add a QZSS navigation message to the list.
addRangeData(CRD.RangeMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of range data.
addReceiveDelay(int, double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Adds a receive delay to the list.
addReceiver(RinexClock.Receiver) - Method in class org.orekit.gnss.clock.RinexClock
Add a new receiver to the list of stored receivers.
addReferenceClockList(List<RinexClock.ReferenceClock>, AbsoluteDate) - Method in class org.orekit.gnss.clock.RinexClock
Add a list of reference clocks wich will be used after a specified date.
addResetter(ManeuverTriggersResetter) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Add a resetter.
addResetter(Field<T>, FieldManeuverTriggersResetter<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Add a resetter.
addSatellite(String) - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile
Adds a new satellite to this object.
addSatellite(String) - Method in class org.orekit.files.general.OrekitEphemerisFile
Adds a new satellite to this object.
addSatellite(String) - Method in class org.orekit.files.sp3.SP3
Add a new satellite with a given identifier to the list of stored satellites.
addSatellite(String) - Method in class org.orekit.gnss.clock.RinexClock
Add a new satellite with a given identifier to the list of stored satellites.
addSatelliteCoordinate(CPF.CPFCoordinate) - Method in class org.orekit.files.ilrs.CPF
Deprecated.
addSatelliteCoordinate(String, CPF.CPFCoordinate) - Method in class org.orekit.files.ilrs.CPF
Add a new P/V coordinates to the satellite.
addSatelliteCoordinate(String, SP3.SP3Coordinate) - Method in class org.orekit.files.sp3.SP3
Adds a new P/V coordinate for a given satellite.
addSatelliteCoordinates(String, List<CPF.CPFCoordinate>) - Method in class org.orekit.files.ilrs.CPF
Adds a set of P/V coordinates to the satellite.
addSatelliteVelocityToCPFCoordinate(String, Vector3D) - Method in class org.orekit.files.ilrs.CPF
Add the velocity to the last CPF coordinate entry.
addSBASNavigationMessage(SBASNavigationMessage) - Method in class org.orekit.gnss.navigation.RinexNavigation
Add a SBAS navigation message to the list.
addScheduler(Scheduler<T>) - Method in class org.orekit.estimation.measurements.generation.Generator
Add a sequences generator for a specific measurement type.
addSolution(long[], double) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Add a new solution.
addStationEccentricitiesValidAfter(Vector3D, AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Add a station eccentricity vector entry valid after a limit date.
Using addStationEccentricitiesValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addStationEccentricitiesValidBefore(Vector3D, AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Add a station eccentricity vector entry valid before a limit date.
Using addStationEccentricitiesValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
addSupportedParameter(ParameterDriver) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Add a supported parameter.
addSwitchingCondition(AttitudeProvider, AttitudeProvider, T, boolean, boolean, double, AngularDerivativesFilter, AttitudesSequence.SwitchHandler) - Method in class org.orekit.attitudes.AttitudesSequence
Add a switching condition between two attitude providers.
addSystemObservationType(SatelliteSystem, ObservationType) - Method in class org.orekit.gnss.clock.RinexClock
Add an observation type for a specified satellite system.
addTimeSystemCorrections(RinexNavigation.TimeSystemCorrection) - Method in class org.orekit.gnss.navigation.RinexNavigation
Add a time system correction to the list.
addTransmitDelay(int, double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Adds a transmit delay to the list.
addTroposphericModelValidAfter(EstimatedTroposphericModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Add a EstimatedTroposphericModel entry valid after a limit date.
Using addTroposphericModelValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addTroposphericModelValidBefore(EstimatedTroposphericModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Add an EstimatedTroposphericModel entry valid before a limit date.
Using addTroposphericValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
addUTCTAIOffsetsLoader(UTCTAIOffsetsLoader) - Method in class org.orekit.time.LazyLoadedTimeScales
Add a loader for UTC-TAI offsets history files.
addUTCTAIOffsetsLoader(UTCTAIOffsetsLoader) - Static method in class org.orekit.time.TimeScalesFactory
Add a loader for UTC-TAI offsets history files.
addValidAfter(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Add an entry valid after a limit date.
addValidAfter(T, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
addValidAfter(T, AbsoluteDate, boolean) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid after a limit date.
addValidBefore(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Add an entry valid before a limit date.
addValidBefore(T, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
addValidBefore(T, AbsoluteDate, boolean) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid before a limit date.
addValidBetween(T, AbsoluteDate, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid between two limit dates.
addWaveCoefficients(int, int, int, double, double, double, double, int, String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Add parsed coefficients.
AdmMetadata - Class in org.orekit.files.ccsds.ndm.adm
This class gathers the meta-data present in the Attitude Data Message (ADM).
AdmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Simple constructor.
AdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm
Keys for ADM container entries.
AdmMetadataWriter - Class in org.orekit.files.ccsds.ndm.adm
Writer for Common metadata for CCSDS Attitude Parameter/Ephemeris Messages.
AdmMetadataWriter(AdmMetadata) - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmMetadataWriter
Simple constructor.
AdmParser<T extends NdmConstituent<?,?>,P extends AbstractConstituentParser<T,?>> - Class in org.orekit.files.ccsds.ndm.adm
Base class for Attitude Data Message parsers.
AdmParser(String, String, IERSConventions, boolean, DataContext, AbsoluteDate, ParsedUnitsBehavior) - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmParser
Complete constructor.
AdmParser.RotationOrderConsumer - Interface in org.orekit.files.ccsds.ndm.adm
Interface representing instance methods that consume otation order values.
Aem - Class in org.orekit.files.ccsds.ndm.adm.aem
This class stores all the information of the Attitude Ephemeris Message (AEM) File parsed by AEMParser.
Aem(Header, List<AemSegment>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.Aem
Simple constructor.
AemData - Class in org.orekit.files.ccsds.ndm.adm.aem
The Attitude Ephemerides data blocks class contain list of attitude data points.
AemData() - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemData
Constructor.
AemMetadata - Class in org.orekit.files.ccsds.ndm.adm.aem
This class gathers the meta-data present in the Attitude Data Message (ADM).
AemMetadata(int) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Simple constructor.
AemMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.aem
Keys for AEM container entries.
AemParser - Class in org.orekit.files.ccsds.ndm.adm.aem
A parser for the CCSDS AEM (Attitude Ephemeris Message).
AemParser(IERSConventions, boolean, DataContext, AbsoluteDate, int, ParsedUnitsBehavior) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Complete constructor.
AemSatelliteEphemeris - Class in org.orekit.files.ccsds.ndm.adm.aem
AEM ephemeris blocks for a single satellite.
AemSatelliteEphemeris(String, List<AemSegment>) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.
AemSegment - Class in org.orekit.files.ccsds.ndm.adm.aem
This class stores the metadata and data for one attitude segment.
AemSegment(AemMetadata, AemData) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Simple constructor.
AemWriter - Class in org.orekit.files.ccsds.ndm.adm.aem
A writer for Attitude Ephemeris Messsage (AEM) files.
AemWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemWriter
Constructor used to create a new AEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
afterIntegration() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Method called just after integration.
afterIntegration() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Method called just after integration.
afterIntegration() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Method called just after integration.
afterIntegration() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Method called just after integration.
AggregateBoundedAttitudeProvider - Class in org.orekit.attitudes
A BoundedAttitudeProvider that covers a larger time span from several constituent attitude providers that cover shorter time spans.
AggregateBoundedAttitudeProvider(Collection<? extends BoundedAttitudeProvider>) - Constructor for class org.orekit.attitudes.AggregateBoundedAttitudeProvider
Constructor.
AggregateBoundedPropagator - Class in org.orekit.propagation.analytical
A BoundedPropagator that covers a larger time span from several constituent propagators that cover shorter time spans.
AggregateBoundedPropagator(Collection<? extends BoundedPropagator>) - Constructor for class org.orekit.propagation.analytical.AggregateBoundedPropagator
Create a propagator by concatenating several BoundedPropagators.
AGILeapSecondFilesLoader - Class in org.orekit.time
Loader for UTC-TAI extracted from LeapSecond file from AGI.
AGILeapSecondFilesLoader(String) - Constructor for class org.orekit.time.AGILeapSecondFilesLoader
Build a loader for LeapSecond.dat file from AGI.
AGILeapSecondFilesLoader(String, DataProvidersManager) - Constructor for class org.orekit.time.AGILeapSecondFilesLoader
Build a loader for LeapSecond.dat file from AGI.
AGILeapSecondFilesLoader.Parser - Class in org.orekit.time
Internal class performing the parsing.
alias(String) - Method in class org.orekit.utils.units.Unit
Create an alias for a unit.
AlignmentDetector - Class in org.orekit.propagation.events
Finder for satellite/body alignment events in orbital plane.
AlignmentDetector(Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
AlignmentDetector(double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
AlignmentDetector(double, Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.AlongTrackAiming
Find the along tile direction for tessellation at specified point.
alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.ConstantAzimuthAiming
Find the along tile direction for tessellation at specified point.
alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.DivertedSingularityAiming
Find the along tile direction for tessellation at specified point.
alongTileDirection(Vector3D, GeodeticPoint) - Method in interface org.orekit.models.earth.tessellation.TileAiming
Find the along tile direction for tessellation at specified point.
AlongTrackAiming - Class in org.orekit.models.earth.tessellation
Class used to orient tiles along an orbit track.
AlongTrackAiming(OneAxisEllipsoid, Orbit, boolean) - Constructor for class org.orekit.models.earth.tessellation.AlongTrackAiming
Simple constructor.
AltitudeDetector - Class in org.orekit.propagation.events
Finder for satellite altitude crossing events.
AltitudeDetector(double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AltitudeDetector(double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AltitudeDetector(double, double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
Name for ambiguity driver.
AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
Name for ambiguity driver.
AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.Phase
Name for ambiguity driver.
AmbiguityAcceptance - Interface in org.orekit.estimation.measurements.gnss
Interface defining ambiguity acceptance tests.
AmbiguitySolver - Class in org.orekit.estimation.measurements.gnss
Class for solving integer ambiguity problems.
AmbiguitySolver(List<ParameterDriver>, IntegerLeastSquareSolver, AmbiguityAcceptance) - Constructor for class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Simple constructor.
AMPERE - Static variable in class org.orekit.utils.units.Unit
Ampere unit.
analyticalDerivativeComputations(AbstractJacobiansMapper, SpacecraftState) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Deprecated.
as of 11.1, not used anymore
analyticalDerivatives(SpacecraftState) - Method in class org.orekit.propagation.analytical.tle.TLEJacobiansMapper
Deprecated.
as of 11.1, not used anymore
analyticalDerivatives(SpacecraftState) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Deprecated.
as of 11.1, not used anymore
andCombine(EventDetector...) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical AND of the given event detectors.
andCombine(Collection<? extends EventDetector>) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical AND of the given event detectors.
AnglesMeasurement(AbsoluteDate, double, double, int, int, boolean, double, double) - Constructor for class org.orekit.files.ilrs.CRD.AnglesMeasurement
Constructor.
AngleType - Enum in org.orekit.files.ccsds.ndm.tdm
Antenna geometry represented in the angle date.
AngularAzEl - Class in org.orekit.estimation.measurements
Class modeling an Azimuth-Elevation measurement from a ground station.
AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.AngularAzEl
Simple constructor.
AngularAzElBuilder - Class in org.orekit.estimation.measurements.generation
Builder for AngularAzEl measurements.
AngularAzElBuilder(CorrelatedRandomVectorGenerator, GroundStation, double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.AngularAzElBuilder
Simple constructor.
AngularCoordinates - Class in org.orekit.utils
Simple container for rotation/rotation rate/rotation acceleration triplets.
AngularCoordinates() - Constructor for class org.orekit.utils.AngularCoordinates
Simple constructor.
AngularCoordinates(Rotation, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a rotation/rotation rate pair.
AngularCoordinates(Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a rotation/rotation rate/rotation acceleration triplet.
AngularCoordinates(Rotation) - Constructor for class org.orekit.utils.AngularCoordinates
Builds angular coordinates with the given rotation, zero angular velocity, and zero angular acceleration.
AngularCoordinates(PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.AngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another one.
AngularCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.AngularCoordinates
Build one of the rotations that transform one pv coordinates into another one.
AngularCoordinates(FieldRotation<U>) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a AngularCoordinates from a FieldRotation<Derivative>.
AngularDerivativesFilter - Enum in org.orekit.utils
Enumerate for selecting which derivatives to use in TimeStampedAngularCoordinates and TimeStampedFieldAngularCoordinates interpolation.
AngularIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical angular measurement with ionospheric delay.
AngularIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier
Constructor.
AngularRaDec - Class in org.orekit.estimation.measurements
Class modeling an Right Ascension - Declination measurement from a ground point (station, telescope).
AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.AngularRaDec
Simple constructor.
AngularRaDecBuilder - Class in org.orekit.estimation.measurements.generation
Builder for AngularRaDec measurements.
AngularRaDecBuilder(CorrelatedRandomVectorGenerator, GroundStation, Frame, double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.AngularRaDecBuilder
Simple constructor.
AngularRadioRefractionModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical angular measurement with ionospheric radio refractive index.
AngularRadioRefractionModifier(AtmosphericRefractionModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier
Constructor.
AngularSeparationDetector - Class in org.orekit.propagation.events
Detects when spacecraft comes close to a moving beacon, as seen from a moving observer.
AngularSeparationDetector(PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationDetector
Build a new angular separation detector.
AngularSeparationFromSatelliteDetector - Class in org.orekit.propagation.events
Detects when two moving objects come close to each other, as seen from spacecraft.
AngularSeparationFromSatelliteDetector(PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Build a new angular detachment detector.
AngularTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical angular measurement with tropospheric delay.
AngularTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
Constructor.
Antenna - Class in org.orekit.gnss.antenna
GNSS antenna model.
Antenna(String, String, Map<Frequency, FrequencyPattern>) - Constructor for class org.orekit.gnss.antenna.Antenna
Simple constructor.
AntexLoader - Class in org.orekit.gnss.antenna
Factory for GNSS antennas (both receiver and satellite).
AntexLoader(String) - Constructor for class org.orekit.gnss.antenna.AntexLoader
Simple constructor.
AntexLoader(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.gnss.antenna.AntexLoader
Construct a loader by specifying the source of ANTEX auxiliary data files.
anticipateNext(ProcessingState) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Anticipate what next processing state should be.
Apm - Class in org.orekit.files.ccsds.ndm.adm.apm
This class stores all the information of the Attitude Parameter Message (APM) File parsed by APMParser.
Apm(Header, List<Segment<AdmMetadata, ApmData>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.Apm
Simple constructor.
ApmData - Class in org.orekit.files.ccsds.ndm.adm.apm
Container for Attitude Parameter Message data.
ApmData(CommentsContainer, ApmQuaternion, Euler, SpinStabilized, SpacecraftParameters) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Simple constructor.
ApmParser - Class in org.orekit.files.ccsds.ndm.adm.apm
A parser for the CCSDS APM (Attitude Parameter Message).
ApmParser(IERSConventions, boolean, DataContext, AbsoluteDate, ParsedUnitsBehavior) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Complete constructor.
ApmQuaternion - Class in org.orekit.files.ccsds.ndm.adm.apm
Container for Attitude Parameter Message quaternion logical block.
ApmQuaternion() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Simple constructor.
ApmQuaternionKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
Keys for APM quaternion entries.
ApmWriter - Class in org.orekit.files.ccsds.ndm.adm.apm
Writer for CCSDS Orbit Parameter Message.
ApmWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter
Complete constructor.
AppliedDCBS - Class in org.orekit.gnss
Corrections of Differential Code Biases (DCBs) applied.
AppliedDCBS(SatelliteSystem, String, String) - Constructor for class org.orekit.gnss.AppliedDCBS
Simple constructor.
AppliedPCVS - Class in org.orekit.gnss
Corrections of antenna phase center variations (PCVs) applied.
AppliedPCVS(SatelliteSystem, String, String) - Constructor for class org.orekit.gnss.AppliedPCVS
Simple constructor.
appliesTo(String) - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration
Check if this entry applies to a file name.
apply(Orbit) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the effect of the maneuver on an orbit.
apply(SpacecraftState) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the effect of the maneuver on a spacecraft state.
apply(SpacecraftState) - Method in interface org.orekit.propagation.analytical.AdapterPropagator.DifferentialEffect
Apply the effect to a spacecraft state.
apply(Orbit) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect
Compute the effect of the maneuver on an orbit.
apply(SpacecraftState) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect
Apply the effect to a spacecraft state.
applyCorrectionOnPV(CR3BPDifferentialCorrection) - Method in class org.orekit.orbits.HaloOrbit
Apply the differential correction to compute more accurate initial PV.
applyCorrectionOnPV(CR3BPDifferentialCorrection) - Method in class org.orekit.orbits.LibrationOrbit
Apply the differential correction to compute more accurate initial PV.
applyCorrectionOnPV(CR3BPDifferentialCorrection) - Method in class org.orekit.orbits.LyapunovOrbit
Apply the differential correction to compute more accurate initial PV.
applyDifferentialCorrection() - Method in class org.orekit.orbits.LibrationOrbit
Apply differential correction.
applyDifferentialCorrection(AttitudeProvider, TimeScale) - Method in class org.orekit.orbits.LibrationOrbit
Deprecated.
applyRelevantFilters(DataSource) - Method in class org.orekit.data.FiltersManager
Apply all the relevant data filters, taking care of layers.
applyResetters(SpacecraftState) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Apply resetters.
applyResetters(FieldSpacecraftState<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Apply resetters.
applyTo(PVCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(PVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
approximateAsPolynomialOnly(int, AbsoluteDate, int, int, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic
Approximate an already fitted model to polynomial only terms.
ApsideDetector - Class in org.orekit.propagation.events
Finder for apside crossing events.
ApsideDetector(Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector
Build a new instance.
ApsideDetector(double, Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector
Build a new instance.
ARBITRARY_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
An arbitrary finite date.
ARC_MINUTE - Static variable in class org.orekit.utils.units.Unit
Arc minute unit.
ARC_SECOND - Static variable in class org.orekit.utils.units.Unit
Arc second unit.
ARC_SECONDS_TO_RADIANS - Static variable in interface org.orekit.utils.Constants
Conversion factor from arc seconds to radians: 2*PI/(360*60*60).
ARC_SECONDS_TO_RADIANS - Static variable in class org.orekit.utils.units.UnitsConverter
Arcseconds to radians converter.
areAdditionalDataAvailable() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the flag indicating if additional parameters are in the message.
areFeesRequired() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Check if fees are required.
areFeesRequired() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Check if fees are required.
asCelestialBodyFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the associated celestial body frame.
asFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the associated frame tree node.
asOrbitRelativeFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the associated orbit relative frame.
asSpacecraftBodyFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the associated spacecraft body frame.
ASTRONOMICAL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector
Sun elevation at astronomical dawn/dusk (18° below horizon).
AstronomicalAmplitudeReader - Class in org.orekit.forces.gravity.potential
Parser for tides astronomical amplitude Hf.
AstronomicalAmplitudeReader(String, int, int, int, double) - Constructor for class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Simple constructor.
Atmosphere - Interface in org.orekit.models.earth.atmosphere
Interface for atmospheric models.
AtmosphericRefractionModel - Interface in org.orekit.models
Defines an refraction model that can be used to correct for the apparent position of an object due to atmospheric effects.
ATOMIC_NITROGEN - Static variable in class org.orekit.models.earth.atmosphere.DTM2000
Identifier for atomic nitrogen.
ATOMIC_OXYGEN - Static variable in class org.orekit.models.earth.atmosphere.DTM2000
Identifier for atomic oxygen.
attachTo(Frame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame
Attach the instance (and all its children down to leafs) to the main tree.
attachTo(Frame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame
Attach the instance (and all its children down to leafs) to the main tree.
Attitude - Class in org.orekit.attitudes
This class handles attitude definition at a given date.
Attitude(Frame, TimeStampedAngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
Attitude(AbsoluteDate, Frame, AngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
Attitude(AbsoluteDate, Frame, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
AttitudeBuilder - Interface in org.orekit.attitudes
This interface represents a builder for attitude.
AttitudeEndoints - Class in org.orekit.files.ccsds.ndm.adm
Endpoints for attitude definition.
AttitudeEndoints() - Constructor for class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
 
AttitudeEntryKey - Enum in org.orekit.files.ccsds.ndm.adm.aem
Keys for attitude entries in XML messages.
AttitudeEphemerisFile<C extends TimeStampedAngularCoordinates,S extends AttitudeEphemerisFile.AttitudeEphemerisSegment<C>> - Interface in org.orekit.files.general
An interface for accessing the data stored in an attitude ephemeris file.
AttitudeEphemerisFile.AttitudeEphemerisSegment<C extends TimeStampedAngularCoordinates> - Interface in org.orekit.files.general
A segment of an attitude ephemeris for a satellite.
AttitudeEphemerisFile.SatelliteAttitudeEphemeris<C extends TimeStampedAngularCoordinates,S extends AttitudeEphemerisFile.AttitudeEphemerisSegment<C>> - Interface in org.orekit.files.general
Contains the information about a single satellite from an AttitudeEphemerisFile.
AttitudeEphemerisFileParser<T extends AttitudeEphemerisFile<?,?>> - Interface in org.orekit.files.general
Parse an ephemeris file.
AttitudeEphemerisFileWriter - Interface in org.orekit.files.general
An interface for writing out ephemeris files to disk.
AttitudeProvider - Interface in org.orekit.attitudes
This interface represents an attitude provider model set.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
Sets the attitude provider.
AttitudeProviderModifier - Interface in org.orekit.attitudes
This interface represents an attitude provider that modifies/wraps another underlying provider.
AttitudesSequence - Class in org.orekit.attitudes
This classes manages a sequence of different attitude providers that are activated in turn according to switching events.
AttitudesSequence() - Constructor for class org.orekit.attitudes.AttitudesSequence
Constructor for an initially empty sequence.
AttitudesSequence.SwitchHandler - Interface in org.orekit.attitudes
Interface for attitude switch notifications.
AttitudeType - Enum in org.orekit.files.ccsds.ndm.adm
Enumerate for ADM attitude type.
AttitudeWriter - Class in org.orekit.files.ccsds.ndm.adm.aem
An AttitudeEphemerisFileWriter generating AEM files.
AttitudeWriter(AemWriter, Header, AemMetadata, FileFormat, String, int) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AttitudeWriter
Constructor used to create a new AEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
ATTRACTION_COEFFICIENT - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Name of the single parameter of this model: the attraction coefficient.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.DeSitterRelativity
Suffix for parameter name for attraction coefficient enabling Jacobian processing.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Suffix for parameter name for attraction coefficient enabling Jacobian processing.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Suffix for parameter name for attraction coefficient enabling Jacobian processing.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.ThirdBodyAttraction
Suffix for parameter name for attraction coefficient enabling Jacobian processing.
Authentication - Enum in org.orekit.gnss.metric.ntrip
Enumerate for authentication method in DataStreamRecord.
AuxiliaryElements - Class in org.orekit.propagation.semianalytical.dsst.utilities
Container class for common parameters used by all DSST forces.
AuxiliaryElements(Orbit, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Simple constructor.

B

B2A - Static variable in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Constant for A ← B direction.
B_STAR - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Parameter name for B* coefficient.
B_STAR - Static variable in class org.orekit.propagation.analytical.tle.TLE
Parameter name for B* coefficient.
BAR - Static variable in class org.orekit.utils.units.Unit
Bar unit.
BaseRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Base class modifying theoretical range measurement with ionospheric delay.
BaseRangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier
Constructor.
BaseRangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Base class modifying theoretical range-rate measurement with ionospheric delay.
BaseRangeRateIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier
Constructor.
BaseRangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Baselass modifying theoretical range-rate measurements with tropospheric delay.
BaseRangeRateTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier
Constructor.
BaseRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Base class modifying theoretical range measurements with tropospheric delay.
BaseRangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier
Constructor.
BasicConstantThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion
Constant thrust propulsion model with: - Constant thrust direction in spacecraft frame - Parameter drivers (for estimation) for the thrust norm or the flow rate.
BasicConstantThrustPropulsionModel(double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Simple constructor.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
 
basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Propagate an orbit without any fancy features.
basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Propagate an orbit without any fancy features.
BatchLSEstimator - Class in org.orekit.estimation.leastsquares
Least squares estimator for orbit determination.
BatchLSEstimator(LeastSquaresOptimizer, OrbitDeterminationPropagatorBuilder...) - Constructor for class org.orekit.estimation.leastsquares.BatchLSEstimator
Simple constructor.
BatchLSModel - Class in org.orekit.estimation.leastsquares
BatchLSModel(OrbitDeterminationPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Constructor for class org.orekit.estimation.leastsquares.BatchLSModel
Simple constructor.
BatchLSObserver - Interface in org.orekit.estimation.leastsquares
Observer for batch least squares estimator iterations.
BDTScale - Class in org.orekit.time
Beidou system time scale.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Method called just before integration.
beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Method called just before integration.
beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Method called just before integration.
BEIDOU_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of the earth's rotation rate in rad/s for Beidou user.
BEIDOU_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for BeiDou weeks: 2006-01-01T00:00:00 UTC.
BEIDOU_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for BeiDou weeks: 2006-01-01.
BEIDOU_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Earth's universal gravitational parameter for Beidou user in m³/s².
BEIDOU_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Number of weeks in the Beidou cycle.
BeidouAlmanac - Class in org.orekit.propagation.analytical.gnss.data
Class for BeiDou almanac.
BeidouAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
Build a new almanac.
BeidouGeo - Class in org.orekit.gnss.attitude
Attitude providers for Beidou geostationary orbit navigation satellites.
BeidouGeo(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouGeo
Simple constructor.
BeidouIGSO - Class in org.orekit.gnss.attitude
Attitude providers for Beidou inclined geosynchronous orbit navigation satellites.
BeidouIGSO(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouIGSO
Simple constructor.
BeidouMeo - Class in org.orekit.gnss.attitude
Attitude providers for Beidou Medium Earth Orbit navigation satellites.
BeidouMeo(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouMeo
Simple constructor.
BeidouNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a BeiDou navigation message.
BeidouNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
Constructor.
BESSELIAN_YEAR - Static variable in interface org.orekit.utils.Constants
Duration of a Besselian year: 365.242198781 Constants.JULIAN_DAY.
beta0 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
sqrt (1 - e2).
beta0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
sqrt (1 - e2).
beta02 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
1 - e2.
beta02 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
1 - e2.
Bias<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
Class modeling a measurement bias.
Bias(String[], double[], double[], double[], double[]) - Constructor for class org.orekit.estimation.measurements.modifiers.Bias
Simple constructor.
BistaticRange - Class in org.orekit.estimation.measurements
Class modeling a bistatic range measurement using an emitter ground station and a receiver ground station.
BistaticRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.BistaticRange
Simple constructor.
BistaticRangeBuilder - Class in org.orekit.estimation.measurements.generation
Builder for BistaticRange measurements.
BistaticRangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.BistaticRangeBuilder
Simple constructor.
BistaticRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical bistatic range measurement with ionospheric delay.
BistaticRangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeIonosphericDelayModifier
Constructor.
BistaticRangeRate - Class in org.orekit.estimation.measurements
Class modeling a bistatic range rate measurement using an emitter ground station and a receiver ground station.
BistaticRangeRate(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.BistaticRangeRate
Simple constructor.
BistaticRangeRateBuilder - Class in org.orekit.estimation.measurements.generation
Builder for BistaticRangeRate measurements.
BistaticRangeRateBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.BistaticRangeRateBuilder
Simple constructor.
BistaticRangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical bistatic range-rate measurement with ionospheric delay.
BistaticRangeRateIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeRateIonosphericDelayModifier
Constructor.
BistaticRangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical bistatic range-rate measurements with tropospheric delay.
BistaticRangeRateTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeRateTroposphericDelayModifier
Constructor.
BistaticRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical bistatic range measurement with tropospheric delay.
BistaticRangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeTroposphericDelayModifier
Constructor.
BodiesElements - Class in org.orekit.data
Elements of the bodies having an effect on nutation.
BodiesElements(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.BodiesElements
Simple constructor.
BodyCenterPointing - Class in org.orekit.attitudes
This class handles body center pointing attitude provider.
BodyCenterPointing(Frame, Ellipsoid) - Constructor for class org.orekit.attitudes.BodyCenterPointing
Creates new instance.
BodyFacade - Class in org.orekit.files.ccsds.definitions
Facade in front of several center bodies in CCSDS messages.
BodyFacade(String, CelestialBody) - Constructor for class org.orekit.files.ccsds.definitions.BodyFacade
Simple constructor.
BodyShape - Interface in org.orekit.bodies
Interface representing the rigid surface shape of a natural body.
BooleanDetector - Class in org.orekit.propagation.events
This class provides AND and OR operations for event detectors.
booleanValue(EncodedMessage) - Method in interface org.orekit.gnss.metric.parser.DataField
Get the value of the field as a boolean.
BoundedAttitudeProvider - Interface in org.orekit.attitudes
This interface is intended for attitude ephemerides valid only during a time range.
BoundedPropagator - Interface in org.orekit.propagation
This interface is intended for ephemerides valid only during a time range.
BoxAndSolarArraySpacecraft - Class in org.orekit.forces
Class representing the features of a classical satellite with a convex body shape and rotating flat solar arrays.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft.Facet - Class in org.orekit.forces
Class representing a single facet of a convex spacecraft body.
BrouwerLyddanePropagator - Class in org.orekit.propagation.analytical
This class propagates a SpacecraftState using the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).
BrouwerLyddanePropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit and potential provider.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Private helper constructor.
BrouwerLyddanePropagator(Orbit, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit and potential.
BrouwerLyddanePropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, mass and potential provider.
BrouwerLyddanePropagator(Orbit, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, mass and potential.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider and potential provider.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider and potential.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
BrouwerLyddanePropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit and potential provider.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Private helper constructor.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, PropagationType, double, double, int) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
BrouwerLyddanePropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for Brouwer-Lyddane propagator.
BrouwerLyddanePropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngle, double, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a new instance.
BrouwerLyddanePropagatorBuilder(Orbit, double, double, TideSystem, double, double, double, double, OrbitType, PositionAngle, double, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a new instance.
BrouwerLyddanePropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngle, double, AttitudeProvider, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a new instance.
build(Frame, PVCoordinatesProvider, TimeStampedAngularCoordinates) - Method in interface org.orekit.attitudes.AttitudeBuilder
Build a filtered attitude.
build(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in interface org.orekit.attitudes.AttitudeBuilder
Build a filtered attitude.
build(Frame, PVCoordinatesProvider, TimeStampedAngularCoordinates) - Method in class org.orekit.attitudes.FixedFrameBuilder
Build a filtered attitude.
build(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in class org.orekit.attitudes.FixedFrameBuilder
Build a filtered attitude.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.AngularAzElBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.AngularRaDecBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.BistaticRangeBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.BistaticRangeRateBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesPhaseBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesRangeBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.PositionBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.PVBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.RangeBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.RangeRateBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.TDOABuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.TurnAroundRangeBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.PhaseBuilder
Generate a single measurement.
build() - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Construct a KalmanEstimator from the data in this builder.
build() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder
Construct a KalmanEstimator from the data in this builder.
build() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Build the file from parsed entries.
build(Frame, PVCoordinatesProvider, TimeStampedAngularCoordinates) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Build a filtered attitude.
build(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Build a filtered attitude.
build(boolean, boolean, RotationOrder, boolean, AbsoluteDate, double...) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Get the angular coordinates corresponding to the attitude data.
build() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.NdmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Build the file from parsed entries.
build() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
Build the file from parsed entries.
build() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Finalizes the build.
build() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Finalizes the build.
build() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Finalizes the build.
build() - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
Finalizes the build.
buildAemParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Attitude Ephemeris Messages.
buildAemWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Attitude Ephemeris Messages.
buildApmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Attitude Parameters Messages.
buildApmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Attitude Parameters Messages.
buildAttitudeProvider(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame, int) - Method in enum org.orekit.gnss.antenna.SatelliteType
Build an attitude provider suitable for this satellite type.
buildCdmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Conjunction Data Messages.
buildCdmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Conjunction Data Messages.
buildFlatArray(Flattener, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Build a coefficients array in flat form.
buildFromCustomAttitude(AttitudeProvider, Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Build a ThrustDirectionAndAttitudeProvider where the attitude is provided by an external.
buildFromDirectionInFrame(Frame, ThrustDirectionProvider, Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Build a ThrustDirectionAndAttitudeProvider by a variable direction in a custom frame.
buildFromDirectionInLOF(LOFType, ThrustDirectionProvider, Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Build a ThrustDirectionAndAttitudeProvider by a variable direction in a Local Orbital Frame.
buildFromFixedDirectionInSatelliteFrame(Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Build a ThrustDirectionAndAttitudeProvider from a fixed direction in the satellite frame.
buildIdentityMatrix2() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Build the identity matrix of order 2.
buildIdentityMatrix4() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Build the identity matrix of order 4.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.EulerIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GillIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.LutherIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.MidpointIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in interface org.orekit.propagation.conversion.ODEIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder
Build a first order integrator.
buildKalmanModel(List<OrbitDeterminationPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a new Kalman model.
buildKalmanModel(List<OrbitDeterminationPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a new Kalman model.
buildKalmanModel(List<OrbitDeterminationPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new Kalman model.
buildKalmanModel(List<OrbitDeterminationPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a new Kalman model.
buildKalmanModel(List<OrbitDeterminationPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a new Kalman model.
buildKalmanModel(List<OrbitDeterminationPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider) - Method in interface org.orekit.propagation.conversion.OrbitDeterminationPropagatorBuilder
Build a new Kalman model.
buildKalmanModel(List<OrbitDeterminationPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
 
buildLSModel(OrbitDeterminationPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a new batch least squares model.
buildLSModel(OrbitDeterminationPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a new batch least squares model.
buildLSModel(OrbitDeterminationPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new batch least squares model.
buildLSModel(OrbitDeterminationPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a new batch least squares model.
buildLSModel(OrbitDeterminationPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a new batch least squares model.
buildLSModel(OrbitDeterminationPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in interface org.orekit.propagation.conversion.OrbitDeterminationPropagatorBuilder
Build a new batch least squares model.
buildLSModel(OrbitDeterminationPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
Build a new batch least squares model.
buildNdmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Navigation Data Messages.
buildNdmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Navigation Data Messages.
buildOcmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Orbit Comprehensive Messages.
buildOcmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Orbit Comprehensive Messages.
buildOemParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Orbit Ephemeris Messages.
buildOemWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Orbit Ephemeris Messages.
buildOmmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Orbit Mean elements Messages.
buildOmmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Orbit Mean elements Messages.
buildOpmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Orbit Parameters Messages.
buildOpmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Orbit Parameters Messages.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
Build a propagator.
buildRow(int, int, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Build a coefficients row.
buildSimpleZone(double, double[]...) - Static method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Build a simple zone (connected zone without holes).
buildSimpleZone(double, GeodeticPoint...) - Static method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Build a simple zone (connected zone without holes).
buildTdmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Tracking Data Messages.
buildTdmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Tracking Data Messages.
buildTermsList(String) - Static method in class org.orekit.utils.units.Parser
Build the list of terms corresponding to a units specification.
buildTokens(boolean, String, String, Attributes, int, String) - Method in class org.orekit.files.ccsds.ndm.adm.RotationXmlTokenBuilder
Create a list of parse tokens.
buildTokens(boolean, String, String, Attributes, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.MessageVersionXmlTokenBuilder
Create a list of parse tokens.
buildTokens(boolean, String, String, Attributes, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.RegularXmlTokenBuilder
Create a list of parse tokens.
buildTokens(boolean, String, String, Attributes, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.UserDefinedXmlTokenBuilder
Create a list of parse tokens.
buildTokens(boolean, String, String, Attributes, int, String) - Method in interface org.orekit.files.ccsds.utils.lexical.XmlTokenBuilder
Create a list of parse tokens.
buildTriangularArray(int, int, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
buildZeroMatrix2() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Build the empty matrix of order 2.
buildZeroMatrix4() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
Build the empty matrix of order 4.
BULLETINA_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the BulletinA files (IAU1980 and IAU2000 compatibles).
BULLETINB_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the BulletinB files (IAU1980 compatibles).
BULLETINB_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the BulletinB files (IAU2000 compatibles).
BurstSelector - Class in org.orekit.time
Selector generating high rate bursts of dates separated by some rest period.
BurstSelector(int, double, double, TimeScale) - Constructor for class org.orekit.time.BurstSelector
Simple constructor.
ByteArrayEncodedMessages - Class in org.orekit.gnss.metric.parser
Encoded messages as a byte array.
ByteArrayEncodedMessages(byte[]) - Constructor for class org.orekit.gnss.metric.parser.ByteArrayEncodedMessages
Simple constructor.

C

c1 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
C1 from SPTRCK #3.
c1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C1 from SPTRCK #3.
C1L - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
C1SS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
c2 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
C2 from SPTRCK #3.
c2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C2 from SPTRCK #3.
c4 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
C4 from SPTRCK #3.
c4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C4 from SPTRCK #3.
C_2FASX4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
C_3FASX6 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
C_FASX2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
C_G22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
C_G32 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
C_G44 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
C_G52 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
C_G54 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
CachedNormalizedSphericalHarmonicsProvider - Class in org.orekit.forces.gravity.potential
CachedNormalizedSphericalHarmonicsProvider(NormalizedSphericalHarmonicsProvider, double, int, int, double, double) - Constructor for class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Simple constructor.
calculateField(double, double, double) - Method in class org.orekit.models.earth.GeoMagneticField
Calculate the magnetic field at the specified geodetic point identified by latitude, longitude and altitude.
canAdd(int, int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Check if coefficients can be added.
canReceiveNMEA() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Check if caster can receive NMEA messages.
CarrierPhase - Enum in org.orekit.gnss.metric.ntrip
Enumerate for carrier phase in DataStreamRecord.
CartesianCovariance - Class in org.orekit.files.ccsds.ndm.odm
Container for OPM/OMM/OCM Cartesian covariance matrix.
CartesianCovariance(Supplier<FrameFacade>) - Constructor for class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Create an empty data set.
CartesianCovarianceKey - Enum in org.orekit.files.ccsds.ndm.odm
CartesianCovarianceWriter - Class in org.orekit.files.ccsds.ndm.odm
Writer for covariance matrix data.
CartesianCovarianceWriter(String, String, CartesianCovariance) - Constructor for class org.orekit.files.ccsds.ndm.odm.CartesianCovarianceWriter
Create a writer.
CartesianDerivativesFilter - Enum in org.orekit.utils
Enumerate for selecting which derivatives to use in TimeStampedPVCoordinates and TimeStampedFieldPVCoordinates interpolation.
CartesianOrbit - Class in org.orekit.orbits
This class holds Cartesian orbital parameters.
CartesianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from Cartesian parameters.
CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from Cartesian parameters.
CartesianOrbit(Orbit) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from any kind of orbital parameters.
CasterRecord - Class in org.orekit.gnss.metric.ntrip
Caster record in source table.
CasterRecord(String) - Constructor for class org.orekit.gnss.metric.ntrip.CasterRecord
Build a caster record by parsing a source table line.
CCSDS_AEM_VERS - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.AemWriter
Version number implemented.
CCSDS_APM_VERS - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter
Version number implemented.
CCSDS_CDM_VERS - Static variable in class org.orekit.files.ccsds.ndm.cdm.CdmWriter
Version number implemented.
CCSDS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).
CCSDS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01.
CCSDS_OCM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter
Version number implemented.
CCSDS_OEM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.OemWriter
Version number implemented.
CCSDS_OMM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmWriter
Version number implemented.
CCSDS_OPM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.OpmWriter
Version number implemented.
CCSDS_TDM_VERS - Static variable in class org.orekit.files.ccsds.ndm.tdm.TdmWriter
Version number implemented.
Cdm - Class in org.orekit.files.ccsds.ndm.cdm
This class stores all the information of the Conjunction Data Message (CDM) File parsed by CdmParser.
Cdm(CdmHeader, List<CdmSegment>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.cdm.Cdm
Simple constructor.
CdmData - Class in org.orekit.files.ccsds.ndm.cdm
Container for Conjunction Data Message data.
CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData
Simple constructor.
CdmHeader - Class in org.orekit.files.ccsds.ndm.cdm
Header of a CCSDS Conjunction Data Message.
CdmHeader(double) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmHeader
Constructor.
CdmHeaderKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keywords allowed in CdmHeader.
CdmHeaderProcessingState - Class in org.orekit.files.ccsds.ndm.cdm
CdmHeaderProcessingState(CdmParser) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmHeaderProcessingState
Simple constructor.
CdmMessageWriter - Class in org.orekit.files.ccsds.ndm.cdm
Cdm message writer.
CdmMessageWriter(String, String, double, ContextBinding) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Constructor used to create a new NDM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
CdmMetadata - Class in org.orekit.files.ccsds.ndm.cdm
This class gathers the meta-data present in the Conjunction Data Message (CDM).
CdmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Simple constructor.
CdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM container entries.
CdmMetadataWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for Metadata for CCSDS Conjunction Data Messages.
CdmMetadataWriter(CdmMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMetadataWriter
Simple constructor.
CdmParser - Class in org.orekit.files.ccsds.ndm.cdm
Base class for Conjunction Data Message parsers.
CdmParser(IERSConventions, boolean, DataContext, ParsedUnitsBehavior) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmParser
Complete constructor.
CdmRelativeMetadata - Class in org.orekit.files.ccsds.ndm.cdm
This class gathers the relative meta-data present in the Conjunction Data Message (CDM).
CdmRelativeMetadata() - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Simple constructor.
CdmRelativeMetadataKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM container entries.
CdmSegment - Class in org.orekit.files.ccsds.ndm.cdm
This class stores the metadata and data for one object.
CdmSegment(CdmMetadata, CdmData) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmSegment
Simple constructor.
CdmWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for CCSDS Conjunction Data Message.
CdmWriter(IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmWriter
Complete constructor.
CelestialBodies - Interface in org.orekit.bodies
Commonly used celestial bodies.
CelestialBody - Interface in org.orekit.bodies
Interface for celestial bodies like Sun, Moon or solar system planets.
CelestialBodyFactory - Class in org.orekit.bodies
Factory class for bodies of the solar system.
CelestialBodyFrame - Enum in org.orekit.files.ccsds.definitions
Frames used in CCSDS Orbit Data Messages.
CelestialBodyLoader - Interface in org.orekit.bodies
Interface for loading celestial bodies.
CelestialBodyPointed - Class in org.orekit.attitudes
This class handles a celestial body pointed attitude provider.
CelestialBodyPointed(Frame, PVCoordinatesProvider, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.CelestialBodyPointed
Creates new instance.
CenterName - Enum in org.orekit.files.ccsds.definitions
Orbit central bodies for which a Celestial body can be created.
CENTRAL_ATTRACTION_COEFFICIENT - Static variable in class org.orekit.forces.gravity.NewtonianAttraction
Name of the single parameter of this model: the central attraction coefficient.
CENTRAL_ATTRACTION_COEFFICIENT - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Name of the single parameter of this model: the central attraction coefficient.
checkAllowed(double, Object, Enum<?>, double, double) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Complain if a key is not allowed.
checkEOPContinuity(double) - Method in class org.orekit.frames.EOPHistory
Check Earth orientation parameters continuity.
checkException() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Check if any of the streaming thread has thrown an exception.
checkExternalFrame(Enum<?>, Enum<?>) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Check external frame is properly initialized.
checkInitialFiringState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Method to set the firing state on initialization.
checkMandatoryEntriesExceptExternalFrame(Enum<?>, Enum<?>, Enum<?>) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Check is mandatory entries except external frame have been initialized.
checkNotNaN(double, Enum<?>) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Complain if a field is NaN.
checkNotNegative(int, Enum<?>) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Complain if a field is negative.
checkNotNull(Object, Enum<?>) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Complain if a field is null.
checkNotNull(Object, Enum<?>) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Complain if a field is null.
checkTimeSystems() - Method in class org.orekit.files.ccsds.ndm.adm.aem.Aem
Check that, according to the CCSDS standard, every AEMBlock has the same time system.
checkTimeSystems() - Method in class org.orekit.files.ccsds.ndm.odm.oem.Oem
Check that, according to the CCSDS standard, every OEMBlock has the same time system.
checkUnit(Unit) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Check if parsed unit is compatible with field type.
checkUnits(List<Unit>) - Method in enum org.orekit.files.ccsds.definitions.ElementsType
Check if parsed units are compatible with elements types.
ChronologicalComparator - Class in org.orekit.time
Comparator for TimeStamped instance.
ChronologicalComparator() - Constructor for class org.orekit.time.ChronologicalComparator
Simple constructor.
CircularFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with circular shape.
CircularFieldOfView(Vector3D, double, double) - Constructor for class org.orekit.geometry.fov.CircularFieldOfView
Build a new instance.
CircularOrbit - Class in org.orekit.orbits
This class handles circular orbital parameters.
CircularOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance.
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance.
CircularOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from Cartesian parameters.
CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from Cartesian parameters.
CircularOrbit(Orbit) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from any kind of orbital parameters.
CIVIL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector
Sun elevation at civil dawn/dusk (6° below horizon).
CjSjCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Sj(k, h) and the Cj(k, h) series and their partial derivatives with respect to k and h.
CjSjCoefficient(double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Cj(k, h) and Sj(k, h) constructor.
CK2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
CK4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
ClassicalRungeKuttaIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for ClassicalRungeKuttaIntegrator.
ClassicalRungeKuttaIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder
Build a new instance.
ClasspathCrawler - Class in org.orekit.data
Provider for data files stored as resources in the classpath.
ClasspathCrawler(String...) - Constructor for class org.orekit.data.ClasspathCrawler
Build a data classpath crawler.
ClasspathCrawler(ClassLoader, String...) - Constructor for class org.orekit.data.ClasspathCrawler
Build a data classpath crawler.
clear() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue
Clear all stored events.
clear() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
Clear all stored events.
clear() - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Remove all handlers managed by this multiplexer.
clear() - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Remove all handlers managed by this multiplexer.
clear() - Method in class org.orekit.utils.DoubleArrayDictionary
Remove all entries.
clear() - Method in class org.orekit.utils.FieldArrayDictionary
Remove all entries.
clearCelestialBodyCache(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear the specified celestial body from the internal cache.
clearCelestialBodyCache() - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear all loaded celestial bodies.
clearCelestialBodyCache(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear the specified celestial body from the internal cache.
clearCelestialBodyCache() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear all loaded celestial bodies.
clearCelestialBodyLoaders(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear loaders for one celestial body.
clearCelestialBodyLoaders() - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear loaders for all celestial bodies.
clearCelestialBodyLoaders(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear loaders for one celestial body.
clearCelestialBodyLoaders() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear loaders for all celestial bodies.
clearEOPHistoryLoaders() - Static method in class org.orekit.frames.FramesFactory
Clear loaders for Earth Orientation Parameters history.
clearEOPHistoryLoaders() - Method in class org.orekit.frames.LazyLoadedEop
Clear loaders for Earth Orientation Parameters history.
clearEOPHistoryLoaders() - Method in class org.orekit.frames.LazyLoadedFrames
Clear loaders for Earth Orientation Parameters history.
clearEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Remove all events detectors.
clearEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator
Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Remove all events detectors.
clearEventsDetectors() - Method in interface org.orekit.propagation.Propagator
Remove all events detectors.
clearFilters() - Method in class org.orekit.data.FiltersManager
Remove all data filters.
clearHistory() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient
Clear the recorded values from the interpolation grid.
clearHistory() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Clear the recorded values from the interpolation grid.
clearLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager
Clear the set of data file names that have been loaded.
clearLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger
Clear the logged events.
clearLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger
Clear the logged events.
clearOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Clear ocean tides readers.
clearOceanTidesReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Clear ocean tides readers.
clearPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Clear gravity field readers.
clearPotentialCoefficientsReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Clear gravity field readers.
clearProviders() - Method in class org.orekit.data.DataProvidersManager
Remove all data providers.
clearStepHandlers() - Method in interface org.orekit.propagation.FieldPropagator
Remove all step handlers.
clearStepHandlers() - Method in interface org.orekit.propagation.Propagator
Remove all step handlers.
clearUTCTAIOffsetsLoaders() - Method in class org.orekit.time.LazyLoadedTimeScales
Clear loaders for UTC-TAI offsets history files.
clearUTCTAIOffsetsLoaders() - Static method in class org.orekit.time.TimeScalesFactory
Clear loaders for UTC-TAI offsets history files.
CLOCK_CORRECTIONS - Static variable in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Name of the additional state for satellite clock corrections.
CLOCK_DRIFT_PREFIX - Static variable in class org.orekit.estimation.measurements.ObservableSatellite
Prefix for clock drift parameter driver, the propagator index will be appended to it.
CLOCK_OFFSET_PREFIX - Static variable in class org.orekit.estimation.measurements.ObservableSatellite
Prefix for clock offset parameter driver, the propagator index will be appended to it.
ClockCorrection - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR clock correction data.
ClockCorrection(double, double, double) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.ClockCorrection
Constructor.
ClockCorrectionsProvider - Class in org.orekit.propagation.analytical.gnss
Provider for clock corrections as additional states.
ClockCorrectionsProvider(GNSSClockElements) - Constructor for class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Simple constructor.
ClockDataLine(RinexClock.ClockDataType, String, DateComponents, TimeComponents, int, double, double, double, double, double, double) - Constructor for class org.orekit.gnss.clock.RinexClock.ClockDataLine
Constructor.
close() - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter
close() - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter
close() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Close the generator.
close() - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Close the generator.
CM_COEFFICIENTS - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Identifier for cMm coefficients.
co2AB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
C / (2 * A * B) .
co2AB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
C / (2 * A * B) .
CodeBias - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for code bias data.
CodeBias(int, double) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.CodeBias
Constructor.
coef - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
coef for SGP C3 computation.
coef - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
coef for SGP C3 computation.
coef1 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
coef for SGP C5 computation.
coef1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
coef for SGP C5 computation.
CoefficientsFactory - Class in org.orekit.propagation.semianalytical.dsst.utilities
This class is designed to provide coefficient from the DSST theory.
CoefficientsFactory.NSKey - Class in org.orekit.propagation.semianalytical.dsst.utilities
Key formed by two integer values.
CombinationType - Enum in org.orekit.estimation.measurements.gnss
Enumerate for combination of measurements types.
combine(ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Combines observation data using a dual frequency combination of measurements.
combine(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Combines observation data using a combination of measurements.
combine(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Combines observation data using a combination of measurements.
combine(ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Combines observation data using a single frequency combination of measurements.
combine(ObservationDataSet) - Method in interface org.orekit.estimation.measurements.gnss.MeasurementCombination
Combines observation data using a combination of measurements.
combine(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.MelbourneWubbenaCombination
Combines observation data using a combination of measurements.
combinedDerivatives(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.propagation.integration.AdditionalEquationsAdapter
Deprecated.
Compute the derivatives related to the additional state (and optionally main state increments).
CombinedDerivatives - Class in org.orekit.propagation.integration
Container for additional derivatives.
CombinedDerivatives(double[], double[]) - Constructor for class org.orekit.propagation.integration.CombinedDerivatives
Simple constructor.
combinedDerivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.integration.FieldAdditionalEquationsAdapter
Deprecated.
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Deprecated.
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Deprecated.
Compute the derivatives related to the additional state (and optionally main state increments).
CombinedObservationData - Class in org.orekit.gnss
Combined observation data.
CombinedObservationData(CombinationType, MeasurementType, double, double, List<ObservationData>) - Constructor for class org.orekit.gnss.CombinedObservationData
Constructor.
CombinedObservationDataSet - Class in org.orekit.gnss
Combined observation data set.
CombinedObservationDataSet(RinexObservationHeader, SatelliteSystem, int, AbsoluteDate, double, List<CombinedObservationData>) - Constructor for class org.orekit.gnss.CombinedObservationDataSet
Simple constructor.
CommentsContainer - Class in org.orekit.files.ccsds.section
Container for comments in various CCSDS messages.
CommentsContainer() - Constructor for class org.orekit.files.ccsds.section.CommentsContainer
Create a new meta-data.
CommonGnssData - Class in org.orekit.propagation.analytical.gnss.data
Container for common GNSS data contained in almanac and navigation messages.
CommonGnssData(double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Constructor.
CommonMetadata - Class in org.orekit.files.ccsds.ndm.odm
Common metadata for Orbit Parameter/Ephemeris/Mean Messages.
CommonMetadata() - Constructor for class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Simple constructor.
CommonMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm
Keys for common ODM container entries.
CommonMetadataWriter - Class in org.orekit.files.ccsds.ndm.odm
Writer for Common metadata for CCSDS Orbit Parameter/Ephemeris/Mean Messages.
CommonMetadataWriter(CommonMetadata, TimeConverter) - Constructor for class org.orekit.files.ccsds.ndm.odm.CommonMetadataWriter
Simple constructor.
ComparableMeasurement - Interface in org.orekit.estimation.measurements
Base interface for comparing measurements regardless of their type.
compare(IntegerLeastSquareSolution, IntegerLeastSquareSolution) - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareComparator
The comparison is based on the squared distance to the float solution.
compare(TimeStamped, TimeStamped) - Method in class org.orekit.time.ChronologicalComparator
Compare two time-stamped instances.
compareTo(ComparableMeasurement) - Method in interface org.orekit.estimation.measurements.ComparableMeasurement
compareTo(CoefficientsFactory.NSKey) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
compareTo(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate
Compare the instance with another date.
compareTo(DateComponents) - Method in class org.orekit.time.DateComponents
compareTo(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents
compareTo(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Compare the instance with another date.
compareTo(TimeComponents) - Method in class org.orekit.time.TimeComponents
compile(PoissonSeries...) - Static method in class org.orekit.data.PoissonSeries
Join several nutation series, for fast simultaneous evaluation.
complain(String, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Complain about a missing value.
complainIfNotSupported(String) - Method in class org.orekit.forces.AbstractForceModel
Complain if a parameter is not supported.
completed() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Check if maneuver has been completed.
completed() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Check if maneuver has been completed.
components(AbsoluteDate) - Method in class org.orekit.files.ccsds.definitions.TimeConverter
Generate calendar components.
compose(AbsoluteDate, StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform
Build a transform by combining two existing ones.
CompositeDataContext - Class in org.orekit.data
A simple implementation of DataContext that composes the constituent factories into a data context.
CompositeDataContext(TimeScales, Frames, CelestialBodies, GravityFields, GeoMagneticFields) - Constructor for class org.orekit.data.CompositeDataContext
Simple constructor.
compositeRotation(StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform
Compute a composite rotation.
compositeTranslation(StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform
Compute a composite translation.
compute(AbsoluteDate, List<Propagator>) - Method in class org.orekit.gnss.DOPComputer
Compute the DOP at a given date for a set of GNSS spacecrafts.
compute(LibrationOrbitType) - Method in class org.orekit.orbits.CR3BPDifferentialCorrection
Return the real starting PVCoordinates on the Libration orbit type after differential correction from a first guess.
compute() - Method in class org.orekit.utils.AbstractMultipleShooting
Return the list of corrected patch points.
compute() - Method in interface org.orekit.utils.MultipleShooting
Return the list of corrected patch points.
computeAdditionalConstraints(List<SpacecraftState>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Compute the additional constraints.
computeAdditionalConstraints(List<SpacecraftState>) - Method in class org.orekit.utils.AbstractMultipleShooting
Compute the additional constraints.
computeAdditionalConstraints(List<SpacecraftState>) - Method in class org.orekit.utils.MultipleShooter
Compute the additional constraints.
computeAdditionalJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Compute a part of the Jacobian matrix from additional constraints.
computeAdditionalJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.utils.AbstractMultipleShooting
Compute a part of the Jacobian matrix from additional constraints.
computeAdditionalJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.utils.MultipleShooter
Compute a part of the Jacobian matrix from additional constraints.
computeDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations
Compute differential equations for main state.
computeDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.propagation.integration.AdditionalEquations
Deprecated.
Compute the derivatives related to the additional state parameters.
computeDerivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations
Compute differential equations for main state.
computeDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations
Deprecated.
Compute the derivatives related to the additional state parameters.
computeDerivatives(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Compute the derivatives related to the additional state parameters.
computeDerivatives(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Compute the derivatives related to the additional state parameters.
computeDerivatives(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Deprecated.
Compute the derivatives related to the additional state parameters.
computeDerivatives(SpacecraftState, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Deprecated.
Compute the derivatives related to the additional state parameters.
computeEpochJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Compute a part of the Jacobian matrix with derivatives from epoch.
computeEpochJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.utils.AbstractMultipleShooting
Compute a part of the Jacobian matrix with derivatives from epoch.
computeGsHs(double, double, double, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute recursively Gs and Hs polynomials from equation 3.1-(5).
computeGsHs(T, T, T, T, int, Field<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute recursively Gs and Hs polynomials from equation 3.1-(5).
computeHaloFirstGuess(double, LibrationOrbitFamily, double, double) - Method in class org.orekit.orbits.RichardsonExpansion
Calculate first Guess.
computeHeightCorrection(double, double) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils
This method computes the height correction for the hydrostatic component of the mapping function.
computeHeightCorrection(T, T, Field<T>) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils
This method computes the height correction for the hydrostatic component of the mapping function.
computeInitValues(T, T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear
Compute the values for the first four coefficients and their derivatives by means of series.
computeInitValues(T, T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear
Compute the initial values (see Collins, 4-255, 4-256 and 4.259)
computeInitValues(T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
Compute the roots for the Hansen coefficients and their derivatives.
computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Compute the values for the first four coefficients and their derivatives by means of series.
computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the initial values (see Collins, 4-255, 4-256 and 4.259)
computeInitValues(double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Compute the roots for the Hansen coefficients and their derivatives.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
 
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit
 
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
 
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit
 
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
 
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit
 
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeLimitVisibilityPoint(double, double, double) - Method in class org.orekit.frames.TopocentricFrame
Compute the limit visibility point for a satellite in a given direction.
computeLyapunov() - Method in class org.orekit.orbits.CR3BPDifferentialCorrection
Return the real starting PVCoordinates on the Lyapunov orbit after differential correction from a first guess.
computeLyapunovFirstGuess(double, double, double) - Method in class org.orekit.orbits.RichardsonExpansion
Calculate first Guess.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, double, int) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, int) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, int) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Conversion from osculating to mean orbit.
computeMeanState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Conversion from osculating to mean orbit.
computeMeanState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Conversion from osculating to mean orbit.
computeMeanState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Conversion from osculating to mean orbit.
computeOsculatingState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Conversion from mean to osculating orbit.
computeOsculatingState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Conversion from mean to osculating orbit.
computeQns(double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute the Qn,s coefficients evaluated at γ from the recurrence formula 2.8.3-(2).
computeQns(T, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute the Qn,s coefficients evaluated at γ from the recurrence formula 2.8.3-(2).
computeThrustDirection(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ConstantThrustDirectionProvider
 
computeThrustDirection(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustDirectionProvider
Compute the thrust direction corresponding to an orbital state.
computeVns(int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute the Vn,s coefficients from 2.8.2-(1)(2).
computeZenithDelay(GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
ConfigurableLowThrustManeuver - Class in org.orekit.forces.maneuvers
This class implements a configurable low thrust maneuver.
ConfigurableLowThrustManeuver(ThrustDirectionAndAttitudeProvider, AbstractDetector<? extends EventDetector>, AbstractDetector<? extends EventDetector>, double, double) - Constructor for class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Constructor.
ConfigurableLowThrustManeuver(ThrustDirectionAndAttitudeProvider, ManeuverTriggers, double, double) - Constructor for class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Constructor.
configureDerivatives(Propagator) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Deprecated.
configureDerivatives(Propagator) - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Deprecated.
configureDerivatives(Propagator) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Deprecated.
configureDerivatives(Propagator) - Method in class org.orekit.estimation.leastsquares.TLEBatchLSModel
Deprecated.
configureHarvester(Propagator) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Configure the propagator to compute derivatives.
configureHarvester(Propagator) - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Configure the propagator to compute derivatives.
configureHarvester(Propagator) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Configure the propagator to compute derivatives.
configureHarvester(Propagator) - Method in class org.orekit.estimation.leastsquares.TLEBatchLSModel
Deprecated.
Configure the propagator to compute derivatives.
configureOceanLoadDeformationCoefficients(OceanLoadDeformationCoefficients) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Configure ocean load deformation coefficients.
configureOceanLoadDeformationCoefficients(OceanLoadDeformationCoefficients) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Configure ocean load deformation coefficients.
configureOrbits(MatricesHarvester, Propagator) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Configure the current estimated orbits.
configureOrbits(MatricesHarvester, Propagator) - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Configure the current estimated orbits.
configureOrbits(MatricesHarvester, Propagator) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Configure the current estimated orbits.
configureOrbits(MatricesHarvester, Propagator) - Method in class org.orekit.estimation.leastsquares.TLEBatchLSModel
Deprecated.
Configure the current estimated orbits.
ConstantAzimuthAiming - Class in org.orekit.models.earth.tessellation
Class used to orient tiles with respect to a geographic azimuth.
ConstantAzimuthAiming(OneAxisEllipsoid, double) - Constructor for class org.orekit.models.earth.tessellation.ConstantAzimuthAiming
Simple constructor.
ConstantProcessNoise - Class in org.orekit.estimation.sequential
Provider for constant process noise matrices.
ConstantProcessNoise(RealMatrix) - Constructor for class org.orekit.estimation.sequential.ConstantProcessNoise
Simple constructor.
ConstantProcessNoise(RealMatrix, RealMatrix) - Constructor for class org.orekit.estimation.sequential.ConstantProcessNoise
Simple constructor.
Constants - Interface in org.orekit.utils
Set of useful physical constants.
ConstantThrustDirectionProvider - Class in org.orekit.forces.maneuvers.propulsion
Simple implementation of VariableThrustDirectionVector, providing a constant direction.
ConstantThrustDirectionProvider(Vector3D) - Constructor for class org.orekit.forces.maneuvers.propulsion.ConstantThrustDirectionProvider
Constructor.
ConstantThrustManeuver - Class in org.orekit.forces.maneuvers
This class implements a simple maneuver with constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, AttitudeProvider, AbstractConstantThrustPropulsionModel) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AttitudeProvider, DateBasedManeuverTriggers, AbstractConstantThrustPropulsionModel) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
containsSatellite(String) - Method in class org.orekit.files.sp3.SP3
Tests whether a satellite with the given id is contained in this orbit file.
ContextBinding - Class in org.orekit.files.ccsds.utils
Context for parsing/writing Navigation Data Message.
ContextBinding(Supplier<IERSConventions>, BooleanSupplier, Supplier<DataContext>, Supplier<ParsedUnitsBehavior>, Supplier<AbsoluteDate>, Supplier<TimeSystem>, DoubleSupplier, DoubleSupplier) - Constructor for class org.orekit.files.ccsds.utils.ContextBinding
Create a new context.
ContinueOnEvent<T extends EventDetector> - Class in org.orekit.propagation.events.handlers
Event handler which will always return continue as a state.
ContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.ContinueOnEvent
 
ContinuousScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation
Scheduler generating measurements sequences continuously.
ContinuousScheduler(MeasurementBuilder<T>, DatesSelector) - Constructor for class org.orekit.estimation.measurements.generation.ContinuousScheduler
Simple constructor.
convert(double[]) - Method in interface org.orekit.data.SimpleTimeStampedTableParser.RowConverter
Convert a row.
convert(Propagator, double, int, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Convert a propagator to another.
convert(Propagator, double, int, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Convert a propagator to another.
convert(List<SpacecraftState>, boolean, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert() - Method in class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter
Convert an osculating orbit into a mean orbit, in DSST sense.
convert(Propagator, double, int, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Convert a propagator into another one.
convert(Propagator, double, int, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Convert a propagator into another one.
convert(List<SpacecraftState>, boolean, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(double) - Method in class org.orekit.utils.units.UnitsConverter
Convert a value.
convertIntervalDetector(Field<S>, ParameterDrivenDateIntervalDetector) - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Convert a primitive firing intervals detector into a field firing intervals detector.
convertIntervalDetector(Field<S>, T) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Convert a primitive firing intervals detector into a field firing intervals detector.
convertStartDetector(Field<S>, A) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Convert a primitive firing start detector into a field firing start detector.
convertStopDetector(Field<S>, O) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Convert a primitive firing stop detector into a field firing stop detector.
convertType(Orbit) - Method in enum org.orekit.orbits.OrbitType
Convert an orbit to the instance type.
convertType(FieldOrbit<T>) - Method in enum org.orekit.orbits.OrbitType
Convert an orbit to the instance type.
copy() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Create a copy of a DSSTPropagatorBuilder object.
copy() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Create a copy of a NumericalPropagatorBuilder object.
copyObservationData(ObservationData) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother
Copy an ObservationData object.
copyObservationData(ObservationData) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother
Copy an ObservationData object.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.BeidouGeo
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.BeidouGeo
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.BeidouMeo
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.BeidouMeo
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Galileo
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.Galileo
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GenericGNSS
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GenericGNSS
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Glonass
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.Glonass
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIA
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIA
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIF
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIF
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIR
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIR
Compute GNSS attitude with midnight/noon yaw turn correction.
CorrectionApplied - Enum in org.orekit.files.ccsds.ndm.tdm
Indicator for corrections application.
cosi0 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
cosinus original inclination.
cosi0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
cosinus original inclination.
COULOMB - Static variable in class org.orekit.utils.units.Unit
Coulomb unit.
countAtDate(AbsoluteDate) - Method in class org.orekit.time.SatelliteClockScale
Compute clock count corresponding to some date.
COV_LINE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Covariance line element for XML messages.
Covariance - Class in org.orekit.files.ccsds.ndm.odm.ocm
Covariance entry.
Covariance(ElementsType, Ordering, AbsoluteDate, String[], int) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.Covariance
Simple constructor.
CovarianceHistory - Class in org.orekit.files.ccsds.ndm.odm.ocm
Covariance history.
CovarianceHistoryMetadata - Class in org.orekit.files.ccsds.ndm.odm.ocm
Metadata for covariance history.
CovarianceHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
CovarianceMatrixProvider - Interface in org.orekit.estimation.sequential
Provider for process noise matrices.
CovarianceMethod - Enum in org.orekit.files.ccsds.ndm.cdm
Maneuvrable possibilities used in CCSDS Conjunction Data Messages.
CPF - Class in org.orekit.files.ilrs
This class stores all the information of the Consolidated laser ranging Prediction File (CPF) parsed by CPFParser.
CPF() - Constructor for class org.orekit.files.ilrs.CPF
Constructor.
CPF.CPFCoordinate - Class in org.orekit.files.ilrs
A single record of position and possibility velocity in an SP3 file.
CPF.CPFEphemeris - Class in org.orekit.files.ilrs
An ephemeris entry for a single satellite contains in a CPF file.
CPFCoordinate(AbsoluteDate, Vector3D, int) - Constructor for class org.orekit.files.ilrs.CPF.CPFCoordinate
Constructor with null velocity vector.
CPFCoordinate(AbsoluteDate, Vector3D, Vector3D, int) - Constructor for class org.orekit.files.ilrs.CPF.CPFCoordinate
Constructor.
CPFEphemeris() - Constructor for class org.orekit.files.ilrs.CPF.CPFEphemeris
Deprecated.
as of 11.0.1, replaced by
CPFEphemeris(String) - Constructor for class org.orekit.files.ilrs.CPF.CPFEphemeris
Constructor.
CPFHeader - Class in org.orekit.files.ilrs
Container for Consolidated laser ranging Prediction File (CPF) header.
CPFHeader() - Constructor for class org.orekit.files.ilrs.CPFHeader
 
CPFParser - Class in org.orekit.files.ilrs
A parser for the CPF orbit file format.
CPFParser() - Constructor for class org.orekit.files.ilrs.CPFParser
Default constructor.
CPFParser(double, int, IERSConventions, TimeScale, Frames) - Constructor for class org.orekit.files.ilrs.CPFParser
Constructor.
CPFWriter - Class in org.orekit.files.ilrs
An CPF Writer class that can take in a general EphemerisFile object and export it as a valid CPF file.
CPFWriter(CPFHeader, TimeScale) - Constructor for class org.orekit.files.ilrs.CPFWriter
Constructor.
CPFWriter(CPFHeader, TimeScale, boolean) - Constructor for class org.orekit.files.ilrs.CPFWriter
Constructor.
CR3BPConstants - Class in org.orekit.propagation.numerical.cr3bp
Set of useful physical CR3BP constants using JPL data.
CR3BPDifferentialCorrection - Class in org.orekit.orbits
Class implementing the differential correction method for Halo or Lyapunov Orbits.
CR3BPDifferentialCorrection(PVCoordinates, CR3BPSystem, double) - Constructor for class org.orekit.orbits.CR3BPDifferentialCorrection
Simple Constructor.
CR3BPDifferentialCorrection(PVCoordinates, CR3BPSystem, double, AttitudeProvider, TimeScale) - Constructor for class org.orekit.orbits.CR3BPDifferentialCorrection
CR3BPFactory - Class in org.orekit.bodies
Factory class creating predefined CR3BP system using CR3BPSystem class.
CR3BPForceModel - Class in org.orekit.propagation.numerical.cr3bp
Class calculating the acceleration induced by CR3BP model.
CR3BPForceModel(CR3BPSystem) - Constructor for class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Simple constructor.
CR3BPMultipleShooter - Class in org.orekit.propagation.numerical.cr3bp
Multiple shooting method applicable for orbits, either propagation in CR3BP, or in an ephemeris model.
CR3BPMultipleShooter(List<SpacecraftState>, List<NumericalPropagator>, List<AdditionalEquations>, double, double) - Constructor for class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
CR3BPMultipleShooter(List<SpacecraftState>, List<NumericalPropagator>, List<STMEquations>, double, double, int) - Constructor for class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Simple Constructor.
CR3BPRotatingFrame - Class in org.orekit.frames
Class creating the rotating frame centered on the barycenter of the CR3BP System.
CR3BPRotatingFrame(double, CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.CR3BPRotatingFrame
Simple constructor.
CR3BPSystem - Class in org.orekit.bodies
Class creating, from two different celestial bodies, the corresponding system with respect to the Circular Restricted Three Body problem hypotheses.
CR3BPSystem(CelestialBody, CelestialBody, double) - Constructor for class org.orekit.bodies.CR3BPSystem
Simple constructor.
CR3BPSystem(CelestialBody, CelestialBody, double, double) - Constructor for class org.orekit.bodies.CR3BPSystem
Simple constructor.
CRD - Class in org.orekit.files.ilrs
This class stores all the information of the Consolidated laser ranging Data Format (CRD) parsed by CRDParser.
CRD() - Constructor for class org.orekit.files.ilrs.CRD
Constructor.
CRD.AnglesMeasurement - Class in org.orekit.files.ilrs
Pointing angles record.
CRD.CRDDataBlock - Class in org.orekit.files.ilrs
Data block containing a set of data contain in the CRD file.
CRD.Meteo - Class in org.orekit.files.ilrs
Meteorological data.
CRD.MeteorologicalMeasurement - Class in org.orekit.files.ilrs
This data record contains a minimal set of meteorological data.
CRD.RangeMeasurement - Class in org.orekit.files.ilrs
Range record.
CRDConfiguration - Class in org.orekit.files.ilrs
Container for Consolidated laser ranging Data Format (CDR) configuration records.
CRDConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration
 
CRDConfiguration.DetectorConfiguration - Class in org.orekit.files.ilrs
Container for detector configuration record.
CRDConfiguration.LaserConfiguration - Class in org.orekit.files.ilrs
Container for laser configuration record.
CRDConfiguration.MeteorologicalConfiguration - Class in org.orekit.files.ilrs
Container for meteorological configuration record.
CRDConfiguration.SoftwareConfiguration - Class in org.orekit.files.ilrs
Container for software configuration record.
CRDConfiguration.SystemConfiguration - Class in org.orekit.files.ilrs
Container for system configuration record.
CRDConfiguration.TimingSystemConfiguration - Class in org.orekit.files.ilrs
Container for timing system configuration record.
CRDConfiguration.TransponderConfiguration - Class in org.orekit.files.ilrs
Container for transponder configuration record.
CRDDataBlock() - Constructor for class org.orekit.files.ilrs.CRD.CRDDataBlock
Constructor.
CRDHeader - Class in org.orekit.files.ilrs
Container for Consolidated laser ranging Data Format (CDR) header.
CRDHeader() - Constructor for class org.orekit.files.ilrs.CRDHeader
 
CRDHeader.RangeType - Enum in org.orekit.files.ilrs
Range type for SLR data.
CRDParser - Class in org.orekit.files.ilrs
A parser for the CRD data file format.
CRDParser() - Constructor for class org.orekit.files.ilrs.CRDParser
Default constructor.
CRDParser(TimeScale) - Constructor for class org.orekit.files.ilrs.CRDParser
Constructor.
create(CenterName) - Static method in class org.orekit.files.ccsds.definitions.BodyFacade
Create a body facade from an input center name.
create(IERSConventions, DataContext, AbsoluteDate, RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Build an instance.
create(IERSConventions, DataContext, AbsoluteDate, RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build an instance.
create(IERSConventions, DataContext, AbsoluteDate, RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build an instance.
create(double, double, int, EventHandler<? super ImpulseManeuver<T>>) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
create(OneAxisEllipsoid, GeodeticPoint) - Static method in class org.orekit.gnss.DOPComputer
Creates a DOP computer for one location.
create(double, double, int, EventHandler<? super T>) - Method in class org.orekit.propagation.events.AbstractDetector
Build a new instance.
create(double, double, int, EventHandler<? super AlignmentDetector>) - Method in class org.orekit.propagation.events.AlignmentDetector
Build a new instance.
create(double, double, int, EventHandler<? super AltitudeDetector>) - Method in class org.orekit.propagation.events.AltitudeDetector
Build a new instance.
create(double, double, int, EventHandler<? super AngularSeparationDetector>) - Method in class org.orekit.propagation.events.AngularSeparationDetector
Build a new instance.
create(double, double, int, EventHandler<? super AngularSeparationFromSatelliteDetector>) - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Build a new instance.
create(double, double, int, EventHandler<? super ApsideDetector>) - Method in class org.orekit.propagation.events.ApsideDetector
Build a new instance.
create(double, double, int, EventHandler<? super BooleanDetector>) - Method in class org.orekit.propagation.events.BooleanDetector
 
create(double, double, int, EventHandler<? super DateDetector>) - Method in class org.orekit.propagation.events.DateDetector
Build a new instance.
create(double, double, int, EventHandler<? super EclipseDetector>) - Method in class org.orekit.propagation.events.EclipseDetector
Build a new instance.
create(double, double, int, EventHandler<? super ElevationDetector>) - Method in class org.orekit.propagation.events.ElevationDetector
Build a new instance.
create(double, double, int, EventHandler<? super ElevationExtremumDetector>) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Build a new instance.
create(double, double, int, EventHandler<? super EventEnablingPredicateFilter<T>>) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
Build a new instance.
create(double, double, int, EventHandler<? super EventShifter<T>>) - Method in class org.orekit.propagation.events.EventShifter
Build a new instance.
create(double, double, int, EventHandler<? super EventSlopeFilter<T>>) - Method in class org.orekit.propagation.events.EventSlopeFilter
Build a new instance.
create(T, T, int, FieldEventHandler<? super D, T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldAltitudeDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldApsideDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldApsideDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldDateDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldDateDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldEclipseDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldElevationDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldElevationDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldFunctionalDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector
 
create(T, T, int, FieldEventHandler<? super FieldLatitudeCrossingDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldNodeDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldNodeDetector
Build a new instance.
create(double, double, int, EventHandler<? super FieldOfViewDetector>) - Method in class org.orekit.propagation.events.FieldOfViewDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldParameterDrivenDateIntervalDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Build a new instance.
create(double, double, int, EventHandler<? super FootprintOverlapDetector>) - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Build a new instance.
create(double, double, int, EventHandler<? super FunctionalDetector>) - Method in class org.orekit.propagation.events.FunctionalDetector
 
create(double, double, int, EventHandler<? super GeographicZoneDetector>) - Method in class org.orekit.propagation.events.GeographicZoneDetector
Build a new instance.
create(double, double, int, EventHandler<? super GroundAtNightDetector>) - Method in class org.orekit.propagation.events.GroundAtNightDetector
Build a new instance.
create(double, double, int, EventHandler<? super GroundFieldOfViewDetector>) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Build a new instance.
create(double, double, int, EventHandler<? super HaloXZPlaneCrossingDetector>) - Method in class org.orekit.propagation.events.HaloXZPlaneCrossingDetector
Build a new instance.
create(double, double, int, EventHandler<? super InterSatDirectViewDetector>) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
Build a new instance.
create(double, double, int, EventHandler<? super LatitudeCrossingDetector>) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Build a new instance.
create(double, double, int, EventHandler<? super LatitudeExtremumDetector>) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
Build a new instance.
create(double, double, int, EventHandler<? super LongitudeCrossingDetector>) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Build a new instance.
create(double, double, int, EventHandler<? super LongitudeExtremumDetector>) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
Build a new instance.
create(double, double, int, EventHandler<? super MagneticFieldDetector>) - Method in class org.orekit.propagation.events.MagneticFieldDetector
Build a new instance.
create(double, double, int, EventHandler<? super NegateDetector>) - Method in class org.orekit.propagation.events.NegateDetector
 
create(double, double, int, EventHandler<? super NodeDetector>) - Method in class org.orekit.propagation.events.NodeDetector
Build a new instance.
create(double, double, int, EventHandler<? super ParameterDrivenDateIntervalDetector>) - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Build a new instance.
create(double, double, int, EventHandler<? super PositionAngleDetector>) - Method in class org.orekit.propagation.events.PositionAngleDetector
Build a new instance.
createBesselianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Besselian Epoch (BE).
createBesselianEpoch(double) - Method in class org.orekit.time.AbstractTimeScales
 
createBesselianEpoch(T) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Besselian Epoch (BE).
createBesselianEpoch(T, TimeScales) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Besselian Epoch (BE).
createBesselianEpoch(double) - Method in interface org.orekit.time.TimeScales
Build an instance corresponding to a Besselian Epoch (BE).
createDataFields(boolean, boolean, RotationOrder, boolean, TimeStampedAngularCoordinates) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Get the attitude data fields corresponding to the attitude type.
createFilter(ObservationData, ObservationData, ObservationData, SatelliteSystem) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother
Creates an Hatch filter given initial data.
createFilter(ObservationData, ObservationData, SatelliteSystem) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother
Creates an Hatch filter given initial data.
createFromModifiedRodrigues(double[][]) - Static method in class org.orekit.utils.AngularCoordinates
Convert a modified Rodrigues vector and derivatives to angular coordinates.
createFromModifiedRodrigues(T[][]) - Static method in class org.orekit.utils.FieldAngularCoordinates
Convert a modified Rodrigues vector and derivatives to angular coordinates.
createFromWeekComponents(int, int, int) - Static method in class org.orekit.time.DateComponents
Build a date from week components.
createGPSDate(int, T) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a GPS date.
createGPSDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a GPS date.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.AbstractPropagator
Create the harvester suitable for propagator.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Create the harvester suitable for propagator.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Create the harvester suitable for propagator.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Create the harvester suitable for propagator.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Create the harvester suitable for propagator.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Create the harvester suitable for propagator.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create the harvester suitable for propagator.
createInitialOrbit() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Build an initial orbit using the current selected parameters.
createJDDate(int, double, TimeScale) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Julian Day date.
createJDDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Julian Day date.
createJulianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Julian Epoch (JE).
createJulianEpoch(double) - Method in class org.orekit.time.AbstractTimeScales
 
createJulianEpoch(T) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Julian Epoch (JE).
createJulianEpoch(T, TimeScales) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Julian Epoch (JE).
createJulianEpoch(double) - Method in interface org.orekit.time.TimeScales
Build an instance corresponding to a Julian Epoch (JE).
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
 
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Create a mapper between raw double components and spacecraft state.
createMJDDate(int, double, TimeScale) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Modified Julian Day date.
createMJDDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Modified Julian Day date.
createPropagators(RealVector) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Create the propagators and parameters corresponding to an evaluation point.
createSlot(FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients
Get the slot valid for some date.
createSlot(SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients
Get the slot valid for some date.
createTransformedITRF(Frame, String) - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Create an ITRF frame by transforming another ITRF frame.
createTransformedITRF(Frame, String, TimeScale) - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Create an ITRF frame by transforming another ITRF frame.
createVertex(Vector3D, Vector3D, double, int) - Method in enum org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType
Create a vertex.
crossProduct(FieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldPVCoordinates
Compute the cross-product of two instances.
crossProduct(PVCoordinates, PVCoordinates) - Static method in class org.orekit.utils.PVCoordinates
Compute the cross-product of two instances.
CssiSpaceWeatherData - Class in org.orekit.models.earth.atmosphere.data
This class provides three-hourly and daily solar activity data needed by atmospheric models: F107 solar flux, Ap and Kp indexes.
CssiSpaceWeatherData(String) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Simple constructor.
CssiSpaceWeatherData(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Constructor that allows specifying the source of the CSSI space weather file.
CssiSpaceWeatherDataLoader - Class in org.orekit.models.earth.atmosphere.data
This class reads solar activity data from CSSI Space Weather files for the class CssiSpaceWeatherData.
CssiSpaceWeatherDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Constructor.
CssiSpaceWeatherDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data
Container class for Solar activity indexes.
CssiSpaceWeatherDataLoader.LineReader - Class in org.orekit.models.earth.atmosphere.data
Deprecated.
as of 11.2, replaced by CommonLineReader to remove duplicated code.
cycleSlipDataSet(String, AbsoluteDate, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Set the data: collect data at the current Date, at the current frequency, for a given satellite, add it within the attributes data and stuff.
CycleSlipDetectorResults - Class in org.orekit.estimation.measurements.gnss
This class is used to contains all the data computed within cycle-slip detector.
CycleSlipDetectors - Interface in org.orekit.estimation.measurements.gnss
Interface for phase measurement cycle-slip detection.

D

Data - Interface in org.orekit.files.ccsds.section
This marker interface represents segment data.
DataContext - Interface in org.orekit.data
Provides auxiliary data for portions of the application.
dataContext(DataContext) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Sets the data context used by the propagator.
DataField - Interface in org.orekit.gnss.metric.parser
Interface for data fields used to parsed encoded messages.
DataFilter - Interface in org.orekit.data
Interface for filtering data (typically uncompressing it) in data providers before passing it to data loaders.
DataFormat - Enum in org.orekit.gnss.metric.ntrip
Enumerate for data format in DataStreamRecord.
DataLoader - Interface in org.orekit.data
Interface for loading data files from data providers.
DataProvider - Interface in org.orekit.data
Interface for providing data files to file loaders.
DataProvidersManager - Class in org.orekit.data
This class manages supported data providers.
DataProvidersManager() - Constructor for class org.orekit.data.DataProvidersManager
Build an instance with default configuration.
DataQuality - Enum in org.orekit.files.ccsds.ndm.tdm
Quality of the data.
DataSource - Class in org.orekit.data
Container associating a name with a stream or reader that can be opened lazily.
DataSource(String, DataSource.StreamOpener) - Constructor for class org.orekit.data.DataSource
Complete constructor.
DataSource(String, DataSource.ReaderOpener) - Constructor for class org.orekit.data.DataSource
Complete constructor.
DataSource(String) - Constructor for class org.orekit.data.DataSource
Build an instance from file name only.
DataSource(File) - Constructor for class org.orekit.data.DataSource
Build an instance from a file on the local file system.
DataSource(URI) - Constructor for class org.orekit.data.DataSource
Build an instance from URI only.
DataSource.Opener - Interface in org.orekit.data
Interface for lazy-opening data streams one time.
DataSource.ReaderOpener - Interface in org.orekit.data
Interface for lazy-opening a characters stream one time.
DataSource.StreamOpener - Interface in org.orekit.data
Interface for lazy-opening a binary stream one time.
DataStreamRecord - Class in org.orekit.gnss.metric.ntrip
Data stream record in source table.
DataStreamRecord(String) - Constructor for class org.orekit.gnss.metric.ntrip.DataStreamRecord
Build a data stream record by parsing a source table line.
DATE_AFTER - Static variable in class org.orekit.forces.drag.TimeSpanDragForce
Prefix for dates after in the parameter drivers' name.
DATE_AFTER - Static variable in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Prefix for dates after in the parameter drivers' name.
DATE_AFTER - Static variable in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Prefix for dates after in the tropospheric parameter drivers' name.
DATE_BEFORE - Static variable in class org.orekit.forces.drag.TimeSpanDragForce
Prefix for dates before in the parameter drivers' name.
DATE_BEFORE - Static variable in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Prefix for dates before in the parameter drivers' name.
DATE_BEFORE - Static variable in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Prefix for dates before in the tropospheric parameter drivers' name.
dateAtCount(double) - Method in class org.orekit.time.SatelliteClockScale
Compute date corresponding to some clock count.
DateBasedManeuverTriggers - Class in org.orekit.forces.maneuvers.trigger
Maneuver triggers based on a start and end date.
DateBasedManeuverTriggers(AbsoluteDate, double) - Constructor for class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Simple constructor.
DateBasedManeuverTriggers(String, AbsoluteDate, double) - Constructor for class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Simple constructor.
DateComponents - Class in org.orekit.time
Class representing a date broken up as year, month and day components.
DateComponents(int, int, int) - Constructor for class org.orekit.time.DateComponents
Build a date from its components.
DateComponents(int, Month, int) - Constructor for class org.orekit.time.DateComponents
Build a date from its components.
DateComponents(int, int) - Constructor for class org.orekit.time.DateComponents
Build a date from a year and day number.
DateComponents(int) - Constructor for class org.orekit.time.DateComponents
Build a date from its offset with respect to a DateComponents.J2000_EPOCH.
DateComponents(DateComponents, int) - Constructor for class org.orekit.time.DateComponents
Build a date from its offset with respect to a reference epoch.
DateDetector - Class in org.orekit.propagation.events
Finder for date events.
DateDetector(double, double, TimeStamped...) - Constructor for class org.orekit.propagation.events.DateDetector
Build a new instance.
DateDetector(AbsoluteDate) - Constructor for class org.orekit.propagation.events.DateDetector
Build a new instance.
DateDriver - Class in org.orekit.utils
Parameter driver allowing to drive a date.
DateDriver(AbsoluteDate, String, boolean) - Constructor for class org.orekit.utils.DateDriver
Simple constructor.
DatesSelector - Interface in org.orekit.time
Interface for selecting dates within an interval.
DateTimeComponents - Class in org.orekit.time
Holder for date and time components.
DateTimeComponents(DateComponents, TimeComponents) - Constructor for class org.orekit.time.DateTimeComponents
Build a new instance from its components.
DateTimeComponents(int, int, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(int, Month, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(int, int, int) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(int, Month, int) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(DateTimeComponents, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from a seconds offset with respect to another one.
dateToString(TimeConverter, AbsoluteDate) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Convert a date to string value with high precision.
dateToString(int, int, int, int, int, double) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Convert a date to string value with high precision.
dateToString(TimeConverter, AbsoluteDate) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Convert a date to string value with high precision.
dateToString(int, int, int, int, int, double) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Convert a date to string value with high precision.
DAY - Static variable in class org.orekit.utils.units.Unit
Day unit.
DAYS_TO_SECONDS - Static variable in class org.orekit.utils.units.UnitsConverter
Days to seconds converter.
decomposer(MatrixDecomposer) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Configure the matrix decomposer.
decomposer(MatrixDecomposer) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder
Configure the matrix decomposer.
deepPeriodicEffects(double) - Method in class org.orekit.propagation.analytical.tle.DeepSDP4
Computes periodic terms from current coordinates and epoch.
deepPeriodicEffects(T) - Method in class org.orekit.propagation.analytical.tle.FieldDeepSDP4
Computes periodic terms from current coordinates and epoch.
DeepSDP4 - Class in org.orekit.propagation.analytical.tle
This class contains the methods that compute deep space perturbation terms.
DeepSDP4(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.DeepSDP4
Constructor for a unique initial TLE.
DeepSDP4(TLE, AttitudeProvider, double, Frame) - Constructor for class org.orekit.propagation.analytical.tle.DeepSDP4
Constructor for a unique initial TLE.
deepSecularEffects(double) - Method in class org.orekit.propagation.analytical.tle.DeepSDP4
Computes secular terms from current coordinates and epoch.
deepSecularEffects(T) - Method in class org.orekit.propagation.analytical.tle.FieldDeepSDP4
Computes secular terms from current coordinates and epoch.
DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Identifier for default type of ephemeris (SGP4/SDP4).
DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for default type of ephemeris (SGP4/SDP4).
DEFAULT_ANTEX_SUPPORTED_NAMES - Static variable in class org.orekit.gnss.antenna.AntexLoader
Default supported files name pattern for antex files.
DEFAULT_BLQ_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Default supported files name pattern for Onsala Space Observatory files in BLQ format.
DEFAULT_CACHED_SLOTS_NUMBER - Static variable in class org.orekit.utils.GenericTimeStampedCache
Default number of independent cached time slots.
DEFAULT_CLOCK_VALUE - Static variable in class org.orekit.files.sp3.SP3Parser
Bad or absent clock values are to be set to 999999.999999.
DEFAULT_CORRECTION_FACTOR - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Default correction factor value.
DEFAULT_CRD_SUPPORTED_NAMES - Static variable in class org.orekit.files.ilrs.CRDParser
Default supported files name pattern for CRD files.
DEFAULT_DE_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader
Default supported files name pattern for JPL DE files.
DEFAULT_EXTRAPOLATION_THRESHOLD_SEC - Static variable in class org.orekit.propagation.analytical.Ephemeris
Default extrapolation time threshold: 1ms.
DEFAULT_FILE_NAME - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.OemWriter
Default file name for error messages.
DEFAULT_ID - Static variable in class org.orekit.files.ilrs.CPF
Default satellite ID, used if header is null when initializing the ephemeris.
DEFAULT_INDENT - Static variable in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Default number of space for each indentation level.
DEFAULT_INPOP_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader
Default supported files name pattern for IMCCE INPOP files.
DEFAULT_INTERPOLATION_METHOD - Static variable in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Default interpolation sample size if it is not specified.
DEFAULT_INTERPOLATION_SIZE - Static variable in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Default interpolation sample size if it is not specified.
DEFAULT_INTERPOLATION_SIZE - Static variable in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Defines the default interpolation sample size if it is not specified on a segment.
DEFAULT_LOW_ELEVATION_THRESHOLD - Static variable in class org.orekit.models.earth.troposphere.SaastamoinenModel
Default lowest acceptable elevation angle [rad].
DEFAULT_MASS - Static variable in interface org.orekit.propagation.FieldPropagator
Default mass.
DEFAULT_MASS - Static variable in interface org.orekit.propagation.Propagator
Default mass.
DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.AbstractDetector
Default maximum number of iterations in the event time search.
DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.FieldAbstractDetector
Default cmaximum number of iterations in the event time search.
DEFAULT_MAX_RECONNECT - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient
Default maximum number of reconnect a attempts without readin any data.
DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.AbstractDetector
Default maximum checking interval (s).
DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.FieldAbstractDetector
Default maximum checking interval (s).
DEFAULT_NAME - Static variable in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Default name for trigger.
DEFAULT_ORIGINATOR - Static variable in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Default value for HeaderKey.ORIGINATOR.
DEFAULT_ORIGINATOR - Static variable in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Default value for HeaderKey.ORIGINATOR.
DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.OceanTides
Default number of points tides field sampling.
DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.SolidTides
Default number of points tides field sampling.
DEFAULT_PORT - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient
Default port for ntrip communication.
DEFAULT_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Default local pressure at viewpoint (Pa).
DEFAULT_RECONNECT_DELAY - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient
Default delay before we reconnect after connection close (s).
DEFAULT_RECONNECT_DELAY_FACTOR - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient
Default factor by which reconnection delay is multiplied after each attempt.
DEFAULT_RINEX_2_SUPPORTED_NAMES - Static variable in class org.orekit.gnss.RinexObservationLoader
Default supported files name pattern for rinex 2 observation files.
DEFAULT_RINEX_3_SUPPORTED_NAMES - Static variable in class org.orekit.gnss.RinexObservationLoader
Default supported files name pattern for rinex 3 observation files.
DEFAULT_STEP - Static variable in class org.orekit.forces.gravity.OceanTides
Default step for tides field sampling (seconds).
DEFAULT_STEP - Static variable in class org.orekit.forces.gravity.SolidTides
Default step for tides field sampling (seconds).
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Default regular expression for supported names that works with all officially published files.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Default regular expression for the supported name that work with all officially published files.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.time.AGILeapSecondFilesLoader
Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.time.TAIUTCDatFilesLoader
Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES_DTC - Static variable in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Default regular expression for supported names that works with test and published files for the DTCFILE file.
DEFAULT_SUPPORTED_NAMES_SOLFSMY - Static variable in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Default regular expression for supported names that works with test and published files for the SOLFSMY file.
DEFAULT_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Default local temperature at viewpoint (K).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.AbstractDetector
Default convergence threshold (s).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.FieldAbstractDetector
Default convergence threshold (s).
DEFAULT_TIMEOUT - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient
Default timeout for connections and reads (ms).
DEFAULT_YAW_BIAS - Static variable in class org.orekit.gnss.attitude.GPSBlockIIA
Default yaw bias (rad).
DEFAULT_YAW_BIAS - Static variable in class org.orekit.gnss.attitude.GPSBlockIIF
Default yaw bias (rad).
DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.Galileo
Default yaw rates for all spacecrafts in radians per seconds.
DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.Glonass
Default yaw rates for all spacecrafts in radians per seconds.
DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.GPSBlockIIF
Default yaw rates for all spacecrafts in radians per seconds.
DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.GPSBlockIIR
Default yaw rates for all spacecrafts in radians per seconds.
DefaultDataContext - Annotation Type in org.orekit.annotation
Indicates that the annotated method, field, or constructor uses the default data context.
DefaultDataContextPlugin - Class in org.orekit.compiler.plugin
Processes DefaultDataContext to issue warnings at compile time.
DefaultDataContextPlugin() - Constructor for class org.orekit.compiler.plugin.DefaultDataContextPlugin
 
DEG_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Degree per second unit.
DEGREE - Static variable in class org.orekit.utils.units.Unit
Degree unit.
DelaunayArguments - Class in org.orekit.data
Delaunay arguments used for nutation or tides.
DelaunayArguments(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.DelaunayArguments
Simple constructor.
DELTA_R_FILE_NAME - Static variable in class org.orekit.models.earth.troposphere.SaastamoinenModel
Default file name for δR correction term table.
dependsOnPositionOnly() - Method in class org.orekit.forces.drag.AbstractDragForceModel
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.empirical.ParametricAcceleration
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Check if force models depends on position only.
dependsOnPositionOnly() - Method in interface org.orekit.forces.ForceModel
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.DeSitterRelativity
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.LenseThirringRelativity
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.NewtonianAttraction
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.OceanTides
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.Relativity
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.SolidTides
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.inertia.InertialForces
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.maneuvers.Maneuver
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Check if force models depends on position only.
derivative(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate time derivative of a set of Poisson series.
derivative(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate time derivative of a set of Poisson series.
derivative(double) - Method in class org.orekit.data.PolynomialNutation
Evaluate the time derivative of the polynomial.
derivative(T) - Method in class org.orekit.data.PolynomialNutation
Evaluate the time derivative of the polynomial.
derivatives(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
Deprecated.
derivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
derivatives(SpacecraftState) - Method in class org.orekit.propagation.integration.AdditionalEquationsAdapter
Deprecated.
derivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
derivatives(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.integration.FieldAdditionalEquationsAdapter
Deprecated.
Compute the derivatives related to the additional state parameters.
derivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Deprecated.
derivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Deprecated.
derivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Deprecated.
derivatives(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Deprecated.
deselectDynamicParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Deselects orbital and propagation drivers.
DeSitterRelativity - Class in org.orekit.forces.gravity
De Sitter post-Newtonian correction force due to general relativity.
DeSitterRelativity() - Constructor for class org.orekit.forces.gravity.DeSitterRelativity
Constructor.
DeSitterRelativity(CelestialBody, CelestialBody) - Constructor for class org.orekit.forces.gravity.DeSitterRelativity
Simple constructor.
detect(List<ObservationDataSet>) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Detects if a cycle-slip occurs for a given list of observation data set.
detect(List<ObservationDataSet>) - Method in interface org.orekit.estimation.measurements.gnss.CycleSlipDetectors
Detects if a cycle-slip occurs for a given list of observation data set.
DetectorConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
 
differentiate(ParameterFunction, int, double) - Static method in class org.orekit.utils.Differentiation
Differentiate a scalar function using finite differences.
differentiate(StateFunction, int, AttitudeProvider, OrbitType, PositionAngle, double, int) - Static method in class org.orekit.utils.Differentiation
Differentiate a vector function using finite differences.
Differentiation - Class in org.orekit.utils
Utility class for differentiating various kinds of functions.
directionAt(double) - Method in class org.orekit.geometry.fov.CircularFieldOfView
Get boundary direction at angle.
directionAt(double) - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Get boundary direction at angle.
directionAt(double) - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get boundary direction at angle.
DirectoryCrawler - Class in org.orekit.data
Provider for data files stored in a directories tree on filesystem.
DirectoryCrawler(File) - Constructor for class org.orekit.data.DirectoryCrawler
Build a data files crawler.
discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Find the best solutions to the Integer Least Square problem.
discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.IntegerBootstrapping
Compute the solution by the bootstrap method from equation (13) in P.J.G.
discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod
Find the best solutions to the Integer Least Square problem.
discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Find the best solutions to the Integer Least Square problem.
DiscreteTroposphericModel - Interface in org.orekit.models.earth.troposphere
Defines a tropospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.
displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.OceanLoading
Compute displacement of a ground reference point.
displacement(BodiesElements, Frame, Vector3D) - Method in interface org.orekit.models.earth.displacement.StationDisplacement
Compute displacement of a ground reference point.
displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.TidalDisplacement
Compute displacement of a ground reference point.
DivertedSingularityAiming - Class in org.orekit.models.earth.tessellation
Class used to orient tiles such that there are no singularities within the zone of interest.
DivertedSingularityAiming(SphericalPolygonsSet) - Constructor for class org.orekit.models.earth.tessellation.DivertedSingularityAiming
Simple constructor.
divide(String, Unit) - Method in class org.orekit.utils.units.Unit
Create quotient of units.
doEvent(SpacecraftState) - Method in class org.orekit.propagation.events.EventState
Notify the user's listener of the event.
doEvent(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventState
Notify the user's listener of the event.
doModify(EstimatedMeasurement<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier
Modify measurement.
doModify(EstimatedMeasurement<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier
Modify measurement.
DOP - Class in org.orekit.gnss
This class is a container for the result of a single DOP computation.
DOP(GeodeticPoint, AbsoluteDate, int, double, double, double, double, double) - Constructor for class org.orekit.gnss.DOP
Constructor.
DOP_MIN_ELEVATION - Static variable in class org.orekit.gnss.DOPComputer
Minimum elevation : 0°.
DOPComputer - Class in org.orekit.gnss
This class aims at computing the dilution of precision.
DormandPrince54IntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for DormandPrince54Integrator.
DormandPrince54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder
Build a new instance.
DormandPrince853IntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for DormandPrince853Integrator.
DormandPrince853IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder
Build a new instance.
DoubleArrayDictionary - Class in org.orekit.utils
String → double[] mapping, for small number of keys.
DoubleArrayDictionary() - Constructor for class org.orekit.utils.DoubleArrayDictionary
Constructor with default initial capacity.
DoubleArrayDictionary(int) - Constructor for class org.orekit.utils.DoubleArrayDictionary
Constructor with specified capacity.
DoubleArrayDictionary(DoubleArrayDictionary) - Constructor for class org.orekit.utils.DoubleArrayDictionary
Constructor from another dictionary.
DoubleArrayDictionary(Map<String, double[]>) - Constructor for class org.orekit.utils.DoubleArrayDictionary
Constructor from a map.
DoubleArrayDictionary.Entry - Class in org.orekit.utils
Entry in a dictionary.
DoubleDihedraFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with dihedral shape (i.e.
DoubleDihedraFieldOfView(Vector3D, Vector3D, double, Vector3D, double, double) - Constructor for class org.orekit.geometry.fov.DoubleDihedraFieldOfView
Build a Field Of View with dihedral shape (i.e.
doubleToString(double) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Convert a double to string value with high precision.
doubleToString(double) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Convert a double to string value with high precision.
doubleValue(EncodedMessage) - Method in interface org.orekit.gnss.metric.parser.DataField
Get the value of the field as a double.
DRAG_COEFFICIENT - Static variable in interface org.orekit.forces.drag.DragSensitive
Parameter name for drag coefficient enabling Jacobian processing.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to drag.
dragAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[]) - Method in interface org.orekit.forces.drag.DragSensitive
Compute the acceleration due to drag.
dragAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in interface org.orekit.forces.drag.DragSensitive
Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[]) - Method in class org.orekit.forces.drag.IsotropicDrag
Compute the acceleration due to drag.
dragAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.drag.IsotropicDrag
Compute the acceleration due to drag.
DragForce - Class in org.orekit.forces.drag
Atmospheric drag force model.
DragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.DragForce
Simple constructor.
DragSensitive - Interface in org.orekit.forces.drag
Interface for spacecraft that are sensitive to atmospheric drag forces.
DRIFT_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation
Suffix for ground clock drift parameters name.
DSST_THEORY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
Constant for DSST mean elements theory.
DSSTAtmosphericDrag - Class in org.orekit.propagation.semianalytical.dsst.forces
Atmospheric drag contribution to the DSSTPropagator.
DSSTAtmosphericDrag(DragForce, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Simple constructor with custom force.
DSSTAtmosphericDrag(Atmosphere, double, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Simple constructor assuming spherical spacecraft.
DSSTAtmosphericDrag(Atmosphere, DragSensitive, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Simple constructor with custom spacecraft.
DSSTBatchLSModel - Class in org.orekit.estimation.leastsquares
DSSTBatchLSModel(OrbitDeterminationPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver, PropagationType, PropagationType) - Constructor for class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Simple constructor.
DSSTForceModel - Interface in org.orekit.propagation.semianalytical.dsst.forces
This interface represents a force modifying spacecraft motion for a DSSTPropagator.
DSSTHarvester - Class in org.orekit.propagation.semianalytical.dsst
Harvester between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
DSSTJacobiansMapper - Class in org.orekit.propagation.semianalytical.dsst
Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
DSSTKalmanModel - Class in org.orekit.estimation.sequential
Deprecated.
as of 11.1, replaced by SemiAnalyticalKalmanModel
DSSTKalmanModel(List<OrbitDeterminationPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider, PropagationType, PropagationType) - Constructor for class org.orekit.estimation.sequential.DSSTKalmanModel
Deprecated.
Kalman process model constructor.
DSSTNewtonianAttraction - Class in org.orekit.propagation.semianalytical.dsst.forces
Force model for Newtonian central body attraction for the DSST propagator.
DSSTNewtonianAttraction(double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Simple constructor.
DSSTNewtonianAttractionContext - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in DSSTNewtonianAttraction.
DSSTNewtonianAttractionContext(AuxiliaryElements, double[]) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttractionContext
Simple constructor.
DSSTPartialDerivativesEquations - Class in org.orekit.propagation.semianalytical.dsst
DSSTPartialDerivativesEquations(String, DSSTPropagator, PropagationType) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Deprecated.
Simple constructor.
DSSTPropagator - Class in org.orekit.propagation.semianalytical.dsst
This class propagates orbits using the DSST theory.
DSSTPropagator(ODEIntegrator, PropagationType) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a new instance of DSSTPropagator.
DSSTPropagator(ODEIntegrator, PropagationType, AttitudeProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a new instance of DSSTPropagator.
DSSTPropagator(ODEIntegrator) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a new instance of DSSTPropagator.
DSSTPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for DSST propagator.
DSSTPropagatorBuilder(Orbit, ODEIntegratorBuilder, double, PropagationType, PropagationType) - Constructor for class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a new instance.
DSSTPropagatorBuilder(Orbit, ODEIntegratorBuilder, double, PropagationType, PropagationType, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a new instance.
DSSTSolarRadiationPressure - Class in org.orekit.propagation.semianalytical.dsst.forces
Solar radiation pressure contribution to the DSSTPropagator.
DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Simple constructor with default reference values and spherical spacecraft.
DSSTSolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Simple constructor with default reference values, but custom spacecraft.
DSSTSolarRadiationPressure(double, double, double, double, ExtendedPVCoordinatesProvider, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Constructor with customizable reference values but spherical spacecraft.
DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Complete constructor.
DSSTTesseral - Class in org.orekit.propagation.semianalytical.dsst.forces
Tesseral contribution to the central body gravitational perturbation.
DSSTTesseral(Frame, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Simple constructor with default reference values.
DSSTTesseral(Frame, double, UnnormalizedSphericalHarmonicsProvider, int, int, int, int, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Simple constructor.
DSSTTesseralContext - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in DSSTTesseral.
DSSTThirdBody - Class in org.orekit.propagation.semianalytical.dsst.forces
Third body attraction perturbation to the DSSTPropagator.
DSSTThirdBody(CelestialBody, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Complete constructor.
DSSTThirdBodyContext - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in DSSTThirdBody.
DSSTZonal - Class in org.orekit.propagation.semianalytical.dsst.forces
Zonal contribution to the central body gravitational perturbation.
DSSTZonal(UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Constructor with default reference values.
DSSTZonal(UnnormalizedSphericalHarmonicsProvider, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Simple constructor.
DSSTZonalContext - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in DSSTZonal.
DtcDataLoader - Class in org.orekit.models.earth.atmosphere.data
This class reads solar activity data from DTCFILE files for the class JB2008SpaceEnvironmentData.
DtcDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.DtcDataLoader
Constructor.
DtcDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data
Container class for Solar activity indexes.
DTM2000 - Class in org.orekit.models.earth.atmosphere
This atmosphere model is the realization of the DTM-2000 model.
DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.models.earth.atmosphere.DTM2000
Simple constructor for independent computation.
DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.DTM2000
Simple constructor for independent computation.
DTM2000InputParameters - Interface in org.orekit.models.earth.atmosphere
Container for solar activity data, compatible with DTM2000 Atmosphere model.
DualFrequencyHatchFilter - Class in org.orekit.estimation.measurements.filtering
Hatch Filter using Carrier-Phase measurements taken at two different frequencies, to form a Divergence-Free phase combination.
DualFrequencyHatchFilter(ObservationData, ObservationData, ObservationData, double, double, double, int) - Constructor for class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter
Constructor for the Dual Frequency Hatch Filter.
DualFrequencySmoother - Class in org.orekit.estimation.measurements.filtering
Handler to perform pseudo-range smoothing using Divergence-Free phase combinations.
DualFrequencySmoother(double, int) - Constructor for class org.orekit.estimation.measurements.filtering.DualFrequencySmoother
Simple constructor.
Duration - Class in org.orekit.forces.maneuvers.jacobians
Generator for one column of a Jacobian matrix for special case of maneuver duration.
Duration(String, String, String) - Constructor for class org.orekit.forces.maneuvers.jacobians.Duration
Simple constructor.
DURATION_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Default suffix for duration driver.
DURATION_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Default suffix for duration driver.
durationFrom(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate
Compute the physically elapsed duration between two instants.
durationFrom(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the physically elapsed duration between two instants.
durationFrom(AbsoluteDate) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the physically elapsed duration between two instants.
DutyCycleType - Enum in org.orekit.files.ccsds.definitions
Type of duty cycle used in CCSDS Orbit Comprehensive Messages.
DynamicOutlierFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.
DynamicOutlierFilter(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
Simple constructor.

E

e - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
final eccentricity.
e - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final eccentricity.
e0sq - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
original eccentricity squared.
e0sq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original eccentricity squared.
E_X - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentricity vector first component.
E_Y - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentricity vector second component.
EARTH - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Earth.
EARTH_ANGULAR_VELOCITY - Static variable in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Earth Angular Velocity, in rad/s, from TIRF model.
EARTH_MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Earth-Moon barycenter.
EARTH_RADII - Static variable in class org.orekit.utils.units.Unit
Earth Radii used as Bstar unit in CCSDS OMM.
EARTH_RADIUS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Earth radius in km.
EarthITU453AtmosphereRefraction - Class in org.orekit.models.earth
Implementation of refraction model for Earth exponential atmosphere based on ITU-R P.834-7 recommendation.
EarthITU453AtmosphereRefraction(double) - Constructor for class org.orekit.models.earth.EarthITU453AtmosphereRefraction
Creates a new default instance.
EarthShape - Interface in org.orekit.models.earth
All models of Earth's shape have some common properties that are not shared with arbitrary BodyShapes.
EarthStandardAtmosphereRefraction - Class in org.orekit.models.earth
Implementation of refraction model for Earth standard atmosphere.
EarthStandardAtmosphereRefraction() - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Creates a new default instance.
EarthStandardAtmosphereRefraction(double, double) - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Creates an instance given a specific pressure and temperature.
ECC - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentricity.
ECC_ANOM - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentric anomaly.
ECC_LAT_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentric argument of latitude.
ECC_LON_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentric argument of longitude.
eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit
Computes the mean latitude argument from the eccentric latitude argument.
eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit
Computes the mean longitude argument from the eccentric longitude argument.
eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit
Computes the mean latitude argument from the eccentric latitude argument.
eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
Computes the mean longitude argument from the eccentric longitude argument.
eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit
Computes the true latitude argument from the eccentric latitude argument.
eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit
Computes the true longitude argument from the eccentric longitude argument.
eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit
Computes the true latitude argument from the eccentric latitude argument.
eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
Computes the true longitude argument from the eccentric longitude argument.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Sets the Earth Centered Inertial frame used for propagation.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Sets the Earth Centered Inertial frame used for propagation.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Sets the Earth Centered Inertial frame used for propagation.
eci(Frame) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
Sets the Earth Centered Inertial frame used for propagation.
EcksteinHechlerPropagator - Class in org.orekit.propagation.analytical
This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Private helper constructor.
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit and potential.
EcksteinHechlerPropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, mass and potential provider.
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, mass and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Private helper constructor.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double, PropagationType, double, int) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for Eckstein-Hechler propagator.
EcksteinHechlerPropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new instance.
EcksteinHechlerPropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngle, double, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new instance.
EcksteinHechlerPropagatorBuilder(Orbit, double, double, TideSystem, double, double, double, double, double, OrbitType, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new instance.
EclipseDetector - Class in org.orekit.propagation.events
Finder for satellite eclipse related events.
EclipseDetector(PVCoordinatesProvider, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.EclipseDetector
Build a new eclipse detector.
EclipticProvider - Class in org.orekit.frames
An inertial frame aligned with the ecliptic.
EclipticProvider(IERSConventions) - Constructor for class org.orekit.frames.EclipticProvider
Create a transform provider from MOD to an ecliptically aligned frame.
EclipticProvider(IERSConventions, TimeScales) - Constructor for class org.orekit.frames.EclipticProvider
Create a transform provider from MOD to an ecliptically aligned frame.
ECOM2 - Class in org.orekit.forces.radiation
The Empirical CODE Orbit Model 2 (ECOM2) of the Center for Orbit Determination in Europe (CODE).
ECOM2(int, int, double, ExtendedPVCoordinatesProvider, double) - Constructor for class org.orekit.forces.radiation.ECOM2
Constructor.
ECOM_COEFFICIENT - Static variable in class org.orekit.forces.radiation.ECOM2
Parameter name for ECOM model coefficients enabling Jacobian processing.
eeta - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
original eccentricity * eta.
eeta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original eccentricity * eta.
EGM96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from EGM96 model: -1.08262668355315e-3.
EGM96_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from EGM96 model: 2.53265648533224e-6.
EGM96_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from EGM96 model: 1.619621591367e-6.
EGM96_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from EGM96 model: 2.27296082868698e-7.
EGM96_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from EGM96 model: -5.40681239107085e-7.
EGM96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from EGM96 model: 6378136.3 m.
EGM96_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from EGM96 model: 3.986004415e14 m³/s².
EGM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for EGM files.
EGMFormatReader - Class in org.orekit.forces.gravity.potential
This reader is adapted to the EGM Format.
EGMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader
Simple constructor.
EGMFormatReader(String, boolean, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader
Simple constructor that allows overriding 'standard' EGM96 ae and mu with WGS84 variants.
EIGEN5C_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from EIGEN5C model: -1.082626457231767e-3.
EIGEN5C_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from EIGEN5C model: 2.532547231862799e-6.
EIGEN5C_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from EIGEN5C model: 1.619964434136e-6.
EIGEN5C_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from EIGEN5C model: 2.277928487005437e-7.
EIGEN5C_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from EIGEN5C model: -5.406653715879098e-7.
EIGEN5C_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from EIGEN5C model: 6378136.46 m.
EIGEN5C_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from EIGEN5C model: 3.986004415e14 m³/s².
ElementsType - Enum in org.orekit.files.ccsds.definitions
Orbit element set type used in CCSDS Orbit Comprehensive Messages.
ElevationDetector - Class in org.orekit.propagation.events
Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.
ElevationDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.
ElevationDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.
ElevationExtremumDetector - Class in org.orekit.propagation.events
Detector for elevation extremum with respect to a ground point.
ElevationExtremumDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector
Build a new detector.
ElevationExtremumDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector
Build a detector.
ElevationFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.filtering
Elevation pre-processing filter.
ElevationFilter(GroundStation, double) - Constructor for class org.orekit.estimation.measurements.filtering.ElevationFilter
Constructor.
ElevationMask - Class in org.orekit.utils
Class for modeling the ground elevation values around a given point.
ElevationMask(double[][]) - Constructor for class org.orekit.utils.ElevationMask
Creates an instance of an Elevation mask based on the passed in parameter.
Ellipse - Class in org.orekit.bodies
Model of a 2D ellipse in 3D space.
Ellipse(Vector3D, Vector3D, Vector3D, double, double, Frame) - Constructor for class org.orekit.bodies.Ellipse
Simple constructor.
Ellipsoid - Class in org.orekit.bodies
Modeling of a general three-axes ellipsoid.
Ellipsoid(Frame, double, double, double) - Constructor for class org.orekit.bodies.Ellipsoid
Simple constructor.
EllipsoidTessellator - Class in org.orekit.models.earth.tessellation
Class used to tessellate an interest zone on an ellipsoid in either tiles or grids of geodetic points.
EllipsoidTessellator(OneAxisEllipsoid, TileAiming, int) - Constructor for class org.orekit.models.earth.tessellation.EllipsoidTessellator
Simple constructor.
EllipticalFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with elliptical shape.
EllipticalFieldOfView(Vector3D, Vector3D, double, double, double) - Constructor for class org.orekit.geometry.fov.EllipticalFieldOfView
Build a new instance.
ellipticEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the mean anomaly from the elliptic eccentric anomaly.
ellipticEccentricToMean(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the mean anomaly from the elliptic eccentric anomaly.
ellipticEccentricToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the true anomaly from the elliptic eccentric anomaly.
ellipticEccentricToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the true anomaly from the elliptic eccentric anomaly.
emptyCache() - Static method in class org.orekit.utils.ImmutableTimeStampedCache
Get an empty immutable cache, cast to the correct type.
EnablingPredicate<S extends EventDetector> - Interface in org.orekit.propagation.events
This interface represents an event enabling predicate function.
EncodedMessage - Interface in org.orekit.gnss.metric.parser
Interface for getting bits forming encoded messages.
endMessage(String) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
End CCSDS message.
endMessage(String) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
End CCSDS message.
endMessage(String) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
End CCSDS message.
endParse() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
End parsing.
ensureCompatibleAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldSpacecraftState
Check if two instances have the same set of additional states available.
ensureCompatibleAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.SpacecraftState
Check if two instances have the same set of additional states available.
enterSection(String) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Enter into a new section.
enterSection(String) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Enter into a new section.
enterSection(String) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
Enter into a new section.
enterSection(String) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Enter into a new section.
EOPBasedTransformProvider - Interface in org.orekit.frames
Interface for Transform providers that use Earth Orientation Parameters.
EOPC04_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the EOPC04 files (IAU1980 compatibles).
EOPC04_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the EOPC04 files (IAU2000 compatibles).
EOPEntry - Class in org.orekit.frames
This class holds an Earth Orientation Parameters entry.
EOPEntry(int, double, double, double, double, double, double, double, double, ITRFVersion, AbsoluteDate) - Constructor for class org.orekit.frames.EOPEntry
Simple constructor.
EOPHistory - Class in org.orekit.frames
This class loads any kind of Earth Orientation Parameter data throughout a large time range.
EOPHistory(IERSConventions, Collection<? extends EOPEntry>, boolean) - Constructor for class org.orekit.frames.EOPHistory
Simple constructor.
EOPHistory(IERSConventions, Collection<? extends EOPEntry>, boolean, TimeScales) - Constructor for class org.orekit.frames.EOPHistory
Simple constructor.
EOPHistoryLoader - Interface in org.orekit.frames
Interface for loading Earth Orientation Parameters history.
EOPHistoryLoader.Parser - Interface in org.orekit.frames
Interface for parsing EOP data files.
Ephemeris - Class in org.orekit.propagation.analytical
This class is designed to accept and handle tabulated orbital entries.
Ephemeris(List<SpacecraftState>, int) - Constructor for class org.orekit.propagation.analytical.Ephemeris
Constructor with tabulated states.
Ephemeris(List<SpacecraftState>, int, double) - Constructor for class org.orekit.propagation.analytical.Ephemeris
Constructor with tabulated states.
Ephemeris(List<SpacecraftState>, int, double, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.Ephemeris
Constructor with tabulated states.
EphemerisFile<C extends TimeStampedPVCoordinates,S extends EphemerisFile.EphemerisSegment<C>> - Interface in org.orekit.files.general
An interface for accessing the data stored in an ephemeris file and using the data to create a working Propagator.
EphemerisFile.EphemerisSegment<C extends TimeStampedPVCoordinates> - Interface in org.orekit.files.general
A segment of an ephemeris for a satellite.
EphemerisFile.SatelliteEphemeris<C extends TimeStampedPVCoordinates,S extends EphemerisFile.EphemerisSegment<C>> - Interface in org.orekit.files.general
Contains the information about a single satellite from an EphemerisFile.
EphemerisFileParser<T extends EphemerisFile<?,?>> - Interface in org.orekit.files.general
Parse an ephemeris file.
EphemerisFileWriter - Interface in org.orekit.files.general
An interface for writing out ephemeris files to disk.
EphemerisGenerator - Interface in org.orekit.propagation
Generator for ephemerides.
EphemerisWriter - Class in org.orekit.files.ccsds.ndm.odm.oem
An EphemerisFileWriter generating OEM files.
EphemerisWriter(OemWriter, Header, OemMetadata, FileFormat, String, int) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.EphemerisWriter
Constructor used to create a new OEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
EpochDerivativesEquations - Class in org.orekit.propagation.numerical
This class is a copy of AbsolutePartialDerivativesEquations The computation of the derivatives of the acceleration due to a ThirdBodyAttraction has been added.
EpochDerivativesEquations(String, NumericalPropagator) - Constructor for class org.orekit.propagation.numerical.EpochDerivativesEquations
Simple constructor.
equals(Object) - Method in class org.orekit.bodies.FieldGeodeticPoint
 
equals(Object) - Method in class org.orekit.bodies.GeodeticPoint
 
equals(Object) - Method in class org.orekit.models.earth.displacement.Tide
 
equals(Object) - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Check if this tle equals the provided tle.
equals(Object) - Method in class org.orekit.propagation.analytical.tle.TLE
Check if this tle equals the provided tle.
equals(Object) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
equals(Object) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents the same time as another instance.
equals(Object) - Method in class org.orekit.time.DateComponents
equals(Object) - Method in class org.orekit.time.DateTimeComponents
equals(Object) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents the same time as another instance.
equals(Object) - Method in class org.orekit.time.TimeComponents
equals(Object) - Method in class org.orekit.utils.units.Unit
Check if the instance represents the same unit as another instance.
EquinoctialOrbit - Class in org.orekit.orbits
This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
EquinoctialOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Creates a new instance.
EquinoctialOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Creates a new instance.
EquinoctialOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from Cartesian parameters.
EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from Cartesian parameters.
EquinoctialOrbit(Orbit) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from any kind of orbital parameters.
ErrorState - Class in org.orekit.files.ccsds.utils.parsing
Special ProcessingState that always generate an error message.
ErrorState() - Constructor for class org.orekit.files.ccsds.utils.parsing.ErrorState
 
EskfMeasurementHandler - Class in org.orekit.estimation.sequential
EskfMeasurementHandler(SemiAnalyticalKalmanModel, ExtendedKalmanFilter<MeasurementDecorator>, List<ObservedMeasurement<?>>, AbsoluteDate) - Constructor for class org.orekit.estimation.sequential.EskfMeasurementHandler
Simple constructor.
estimate(Frame, Position, Position, Position) - Method in class org.orekit.estimation.iod.IodGibbs
Give an initial orbit estimation, assuming Keplerian motion.
estimate(Frame, PV, PV, PV) - Method in class org.orekit.estimation.iod.IodGibbs
Give an initial orbit estimation, assuming Keplerian motion.
estimate(Frame, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate) - Method in class org.orekit.estimation.iod.IodGibbs
Give an initial orbit estimation, assuming Keplerian motion.
estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec, double, double, int, boolean) - Method in class org.orekit.estimation.iod.IodGooding
Orbit got from three angular observations.
estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec, double, double) - Method in class org.orekit.estimation.iod.IodGooding
Orbit got from three angular observations.
estimate(Frame, Vector3D, Vector3D, Vector3D, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, double, double, int, boolean) - Method in class org.orekit.estimation.iod.IodGooding
Orbit got from Observed Three Lines of Sight (angles only).
estimate(Frame, Vector3D, Vector3D, Vector3D, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, double, double) - Method in class org.orekit.estimation.iod.IodGooding
Orbit got from Observed Three Lines of Sight (angles only).
estimate(Frame, boolean, int, Position, Position) - Method in class org.orekit.estimation.iod.IodLambert
Estimate an initial orbit from two position measurements.
estimate(Frame, boolean, int, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate) - Method in class org.orekit.estimation.iod.IodLambert
Estimate a Keplerian orbit given two position vectors and a duration.
estimate(Frame, PVCoordinates, AngularRaDec, AngularRaDec, AngularRaDec) - Method in class org.orekit.estimation.iod.IodLaplace
Estimate the orbit from three angular observations at the same location.
estimate(Frame, PVCoordinates, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D) - Method in class org.orekit.estimation.iod.IodLaplace
Estimate orbit from three line of sight angles from the same location.
estimate() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Estimate the orbital, propagation and measurements parameters.
estimate(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Estimate the theoretical value of the measurement.
estimate(int, int, SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Estimate the theoretical value of the measurement.
EstimatedEarthFrameProvider - Class in org.orekit.estimation.measurements
Class modeling an Earth frame whose Earth Orientation Parameters can be estimated.
EstimatedEarthFrameProvider(UT1Scale) - Constructor for class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Build an estimated Earth frame.
EstimatedIonosphericModel - Class in org.orekit.models.earth.ionosphere
An estimated ionospheric model.
EstimatedIonosphericModel(IonosphericMappingFunction, double) - Constructor for class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Build a new instance.
EstimatedMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements
Class holding an estimated theoretical value associated to an observed measurement.
EstimatedMeasurement(T, int, int, SpacecraftState[], TimeStampedPVCoordinates[]) - Constructor for class org.orekit.estimation.measurements.EstimatedMeasurement
Simple constructor.
EstimatedMeasurement.Status - Enum in org.orekit.estimation.measurements
Enumerate for the status of the measurement.
estimatedMeasurementsParameters(ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Configure the estimated measurement parameters.
estimatedMeasurementsParameters(ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder
Configure the estimated measurement parameters.
EstimatedTroposphericModel - Class in org.orekit.models.earth.troposphere
An estimated tropospheric model.
EstimatedTroposphericModel(double, double, MappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Build a new instance using the given environmental conditions.
EstimatedTroposphericModel(MappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Build a new instance using a standard atmosphere model.
estimateRate(Rotation, Rotation, double) - Static method in class org.orekit.utils.AngularCoordinates
Estimate rotation rate between two orientations.
estimateRate(FieldRotation<T>, FieldRotation<T>, double) - Static method in class org.orekit.utils.FieldAngularCoordinates
Estimate rotation rate between two orientations.
estimateRate(FieldRotation<T>, FieldRotation<T>, T) - Static method in class org.orekit.utils.FieldAngularCoordinates
Estimate rotation rate between two orientations.
estimateVelocity(FieldVector3D<T>, FieldVector3D<T>, double) - Static method in class org.orekit.utils.FieldPVCoordinates
Estimate velocity between two positions.
estimateVelocity(Vector3D, Vector3D, double) - Static method in class org.orekit.utils.PVCoordinates
Estimate velocity between two positions.
EstimationModifier<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements
Interface for estimated measurements modifiers used for orbit determination.
EstimationsProvider - Interface in org.orekit.estimation.measurements
Interface for retrieving estimated measurements during orbit determination.
estimationStep(ObservedMeasurement<?>) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Process a single measurement.
eta - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
eta from SPTRCK #3.
eta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
eta from SPTRCK #3.
etasq - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
eta squared.
etasq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
eta squared.
Euler - Class in org.orekit.files.ccsds.ndm.adm.apm
Container for Euler rotations entries.
Euler() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.Euler
Simple constructor.
EulerIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for EulerIntegrator.
EulerIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.EulerIntegratorBuilder
Build a new instance.
EulerKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
Keys for APM Euler angles entries.
evaluateAll(AbsoluteDate) - Method in class org.orekit.data.FundamentalNutationArguments
Evaluate all fundamental arguments for the current date (Delaunay plus planetary).
evaluateAll(FieldAbsoluteDate<T>) - Method in class org.orekit.data.FundamentalNutationArguments
Evaluate all fundamental arguments for the current date (Delaunay plus planetary).
evaluateStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState
Evaluate the impact of the proposed step on the event detector.
evaluateStep(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState
Evaluate the impact of the proposed step on the event detector.
evaluateTC(AbsoluteDate) - Method in enum org.orekit.utils.IERSConventions
Evaluate the date offset between the current date and the reference date.
evaluateTC(AbsoluteDate, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Evaluate the date offset between the current date and the reference date.
evaluateTC(FieldAbsoluteDate<T>) - Method in enum org.orekit.utils.IERSConventions
Evaluate the date offset between the current date and the reference date.
evaluateTC(FieldAbsoluteDate<T>, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Evaluate the date offset between the current date and the reference date.
evaluationPerformed(int, int, Orbit[], ParameterDriversList, ParameterDriversList, ParameterDriversList, EstimationsProvider, LeastSquaresProblem.Evaluation) - Method in interface org.orekit.estimation.leastsquares.BatchLSObserver
Notification callback for the end of each evaluation.
evaluationPerformed(KalmanEstimation) - Method in interface org.orekit.estimation.sequential.KalmanObserver
Notification callback after each one of a Kalman filter estimation.
EventBasedManeuverTriggers - Class in org.orekit.forces.maneuvers.trigger
Maneuver triggers based on start and stop detectors.
EventBasedManeuverTriggers(AbstractDetector<? extends EventDetector>, AbstractDetector<? extends EventDetector>) - Constructor for class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Constructor.
EventBasedManeuverTriggers(AbstractDetector<? extends EventDetector>, AbstractDetector<? extends EventDetector>, boolean) - Constructor for class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Constructor.
EventBasedScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation
Scheduler based on EventDetector for generating measurements sequences.
EventBasedScheduler(MeasurementBuilder<T>, DatesSelector, Propagator, EventDetector, SignSemantic) - Constructor for class org.orekit.estimation.measurements.generation.EventBasedScheduler
Simple constructor.
EventDetector - Interface in org.orekit.propagation.events
This interface represents space-dynamics aware events detectors.
EventEnablingPredicateFilter<T extends EventDetector> - Class in org.orekit.propagation.events
Wrapper used to detect events only when enabled by an external predicated function.
EventEnablingPredicateFilter(T, EnablingPredicate<? super T>) - Constructor for class org.orekit.propagation.events.EventEnablingPredicateFilter
EventHandler<T extends EventDetector> - Interface in org.orekit.propagation.events.handlers
An interface defining how to override event handling behavior in the standard propagator eventing classes without requiring subclassing.
eventIsEnabled(SpacecraftState, S, double) - Method in interface org.orekit.propagation.events.EnablingPredicate
Compute an event enabling function of state.
EventMultipleHandler<D extends EventDetector> - Class in org.orekit.propagation.events.handlers
Facade handlers that allows to use several handlers for one detector.
EventMultipleHandler() - Constructor for class org.orekit.propagation.events.handlers.EventMultipleHandler
Constructor with list initialisation.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
eventOccurred method mirrors the same interface method as in EventDetector and its subclasses, but with an additional parameter that allows the calling method to pass in an object from the detector which would have potential additional data to allow the implementing class to determine the correct return state.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.AbstractDetector
Handle the event.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.AdapterDetector
Handle the event.
eventOccurred(SpacecraftState, boolean) - Method in interface org.orekit.propagation.events.EventDetector
Handle the event.
eventOccurred(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Handle the event.
eventOccurred(FieldSpacecraftState<T>, boolean) - Method in interface org.orekit.propagation.events.FieldEventDetector
Handle the event.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.ContinueOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, T, boolean) - Method in interface org.orekit.propagation.events.handlers.EventHandler
eventOccurred method mirrors the same interface method as in EventDetector and its subclasses, but with an additional parameter that allows the calling method to pass in an object from the detector which would have potential additional data to allow the implementing class to determine the correct return state.
eventOccurred(SpacecraftState, D, boolean) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
eventOccurred method mirrors the same interface method as in EventDetector and its subclasses, but with an additional parameter that allows the calling method to pass in an object from the detector which would have potential additional data to allow the implementing class to determine the correct return state.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldContinueOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler
eventOccurred method mirrors the same interface method as in EventDetector and its subclasses, but with an additional parameter that allows the calling method to pass in an object from the detector which would have potential additional data to allow the implementing class to determine the correct return state.
eventOccurred(FieldSpacecraftState<E>, T, boolean) - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue
 
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnDecreasing
Handle a detection event and choose what to do next.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnIncreasing
Handle a detection event and choose what to do next.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
 
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnDecreasing
Handle a detection event and choose what to do next.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnIncreasing
Handle a detection event and choose what to do next.
EventShifter<T extends EventDetector> - Class in org.orekit.propagation.events
Wrapper shifting events occurrences times.
EventShifter(T, boolean, double, double) - Constructor for class org.orekit.propagation.events.EventShifter
Build a new instance.
EventsLogger - Class in org.orekit.propagation.events
This class logs events detectors events during propagation.
EventsLogger() - Constructor for class org.orekit.propagation.events.EventsLogger
Simple constructor.
EventsLogger.LoggedEvent - Class in org.orekit.propagation.events
Class for logged events entries.
EventSlopeFilter<T extends EventDetector> - Class in org.orekit.propagation.events
Wrapper used to detect only increasing or decreasing events.
EventSlopeFilter(T, FilterType) - Constructor for class org.orekit.propagation.events.EventSlopeFilter
EventState<T extends EventDetector> - Class in org.orekit.propagation.events
This class handles the state for one event detector during integration steps.
EventState(T) - Constructor for class org.orekit.propagation.events.EventState
Simple constructor.
EventState.EventOccurrence - Class in org.orekit.propagation.events
Class to hold the data related to an event occurrence that is needed to decide how to modify integration.
ExceptionalDataContext - Class in org.orekit.data
A data context that always throws a runtime exception when it's methods are used.
ExceptionalDataContext() - Constructor for class org.orekit.data.ExceptionalDataContext
 
exitSection() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Exit last section.
exitSection() - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Exit last section.
exitSection() - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
Exit last section.
exitSection() - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Exit last section.
extend(Gradient, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Add zero derivatives.
extend(FieldVector3D<Gradient>, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Add zero derivatives.
extend(FieldRotation<Gradient>, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Add zero derivatives.
ExtendedPVCoordinatesProvider - Interface in org.orekit.utils
Interface for PV coordinates providers that also support fields.
extendListOfLists(List<List<Double>>, int, int, double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Deprecated.
as of 11.1, not used anymore
extractAccelerationModelRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Extract a range of the AccelerationModel map.
extractBits(int) - Method in class org.orekit.gnss.metric.parser.AbstractEncodedMessages
Extract the next n bits from the encoded message.
extractBits(int) - Method in interface org.orekit.gnss.metric.parser.EncodedMessage
Extract the next n bits from the encoded message.
extractDragSensitiveRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Extract a range of the DragSensitive map.
extractParameters(double[], AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Extract the proper parameter drivers' values from the array in input of the acceleration method.
extractParameters(T[], FieldAbsoluteDate<T>) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Extract the proper parameter drivers' values from the array in input of the acceleration method.
extractParameters(double[], AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Extract the proper parameter drivers' values from the array in input of the acceleration method.
extractParameters(T[], FieldAbsoluteDate<T>) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Extract the proper parameter drivers' values from the array in input of the acceleration method.
extractParameters(double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Extract the proper parameter drivers' values from the array in input of the pathDelay method.
extractParameters(T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Extract the proper parameter drivers' values from the array in input of the pathDelay method.
extractRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Extract a range of the map.

F

F0 - Static variable in enum org.orekit.gnss.Frequency
Common frequency F0 in MHz (10.23 MHz).
Facet(Vector3D, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
Simple constructor.
FactoryManagedFrame - Class in org.orekit.frames
Base class for the predefined frames that are managed by Frames.
FactoryManagedFrame(Frame, TransformProvider, boolean, Predefined) - Constructor for class org.orekit.frames.FactoryManagedFrame
Simple constructor.
feed(Pattern, DataLoader, DataProvidersManager) - Method in class org.orekit.data.AbstractListCrawler
Feed a data file loader by browsing the data collection.
feed(DataLoader) - Method in class org.orekit.data.AbstractSelfFeedingLoader
feed(Pattern, DataLoader, DataProvidersManager) - Method in class org.orekit.data.ClasspathCrawler
Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader, DataProvidersManager) - Method in interface org.orekit.data.DataProvider
Feed a data file loader by browsing the data collection.
feed(String, DataLoader) - Method in class org.orekit.data.DataProvidersManager
Feed a data file loader by browsing all data providers.
feed(Pattern, DataLoader, DataProvidersManager) - Method in class org.orekit.data.DirectoryCrawler
Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader, DataProvidersManager) - Method in class org.orekit.data.ZipJarCrawler
Feed a data file loader by browsing the data collection.
FES_CHAT_EPSILON_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for FES C hat and epsilon tides files.
FES_CNM_SNM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for FES Cnm, Snm tides files.
FES_HF_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for FES Hf tides files.
FESCHatEpsilonReader - Class in org.orekit.forces.gravity.potential
Reader for ocean tides files following the fes2004.dat format.
FESCHatEpsilonReader(String, double, double, OceanLoadDeformationCoefficients, Map<Integer, Double>) - Constructor for class org.orekit.forces.gravity.potential.FESCHatEpsilonReader
Simple constructor.
FESCnmSnmReader - Class in org.orekit.forces.gravity.potential
Reader for ocean tides files following the fes2004_Cnm-Snm.dat format.
FESCnmSnmReader(String, double) - Constructor for class org.orekit.forces.gravity.potential.FESCnmSnmReader
Simple constructor.
fetchByte() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor
Fetch the next byte from the message.
fetchByte() - Method in class org.orekit.gnss.metric.parser.AbstractEncodedMessages
Fetch the next byte from the message.
fetchByte() - Method in class org.orekit.gnss.metric.parser.ByteArrayEncodedMessages
Fetch the next byte from the message.
fetchByte() - Method in class org.orekit.gnss.metric.parser.InputStreamEncodedMessages
Fetch the next byte from the message.
fetchEvaluatedMeasurement(int, EstimatedMeasurement<?>) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Fetch a measurement that was evaluated during propagation.
FieldAbsoluteDate<T extends CalculusFieldElement<T>> - Class in org.orekit.time
This class represents a specific instant in time.
FieldAbsoluteDate(Field<T>, AbsoluteDate) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an AbsoluteDate.
FieldAbsoluteDate(Field<T>) - Constructor for class org.orekit.time.FieldAbsoluteDate
Create an instance with a default value (FieldAbsoluteDate.getJ2000Epoch(Field)).
FieldAbsoluteDate(FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(Field<T>, String, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location (parsed from a string) in a time scale.
FieldAbsoluteDate(Field<T>, DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, DateComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, int, int, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, Month, int, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, Date, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(AbsoluteDate, T) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(FieldAbsoluteDate<T>, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.
FieldAbsolutePVCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
Field implementation of AbsolutePVCoordinates.
FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Build from position, velocity, acceleration.
FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Build from position and velocity.
FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Build from frame, date and FieldPVA coordinates.
FieldAbsolutePVCoordinates(Frame, TimeStampedFieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Build from frame and TimeStampedFieldPVCoordinates.
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Multiplicative constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, FieldAbsolutePVCoordinates<T>, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Subtractive constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Linear constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Linear constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Linear constructor
FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldVector3D<U>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Builds a FieldAbsolutePVCoordinates triplet from a FieldVector3D<DerivativeStructure>.
FieldAbstractAnalyticalPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical
Common handling of FieldPropagator methods for analytical propagators.
FieldAbstractAnalyticalPropagator(Field<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Build a new instance.
FieldAbstractDetector<D extends FieldEventDetector<T>,T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Common parts shared by several orbital events finders.
FieldAbstractDetector(T, T, int, FieldEventHandler<? super D, T>) - Constructor for class org.orekit.propagation.events.FieldAbstractDetector
Build a new instance.
FieldAbstractGaussianContributionContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common "field" parameters used in AbstractGaussianContribution.
FieldAbstractIntegratedPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.integration
Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.
FieldAbstractIntegratedPropagator(Field<T>, FieldODEIntegrator<T>, PropagationType) - Constructor for class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Build a new instance.
FieldAbstractIntegratedPropagator.MainStateEquations<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.integration
Differential equations for the main state (orbit, attitude and mass).
FieldAbstractPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation
Common handling of Propagator methods for analytical propagators.
FieldAbstractPropagator(Field<T>) - Constructor for class org.orekit.propagation.FieldAbstractPropagator
Build a new instance.
FieldAdditionalDerivativesProvider<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.integration
Provider for additional derivatives.
FieldAdditionalEquations<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.integration
Deprecated.
as of 11.1, replaced by FieldAdditionalDerivativesProvider
FieldAdditionalEquationsAdapter<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.integration
Deprecated.
must be removed in 12.0 when AdditionalEquations is removed
FieldAdditionalEquationsAdapter(FieldAdditionalEquations<T>, Supplier<FieldSpacecraftState<T>>) - Constructor for class org.orekit.propagation.integration.FieldAdditionalEquationsAdapter
Deprecated.
Simple constructor.
FieldAdditionalStateProvider<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation
This interface represents providers for additional state data beyond SpacecraftState.
FieldAltitudeDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Finder for satellite altitude crossing events.
FieldAltitudeDetector(T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector
Build a new altitude detector.
FieldAltitudeDetector(T, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector
Build a new altitude detector.
FieldAltitudeDetector(T, T, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector
Build a new altitude detector.
FieldAngularCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
Simple container for rotation / rotation rate pairs, using CalculusFieldElement.
FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a rotation/rotation rate pair.
FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a rotation / rotation rate / rotation acceleration triplet.
FieldAngularCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another one.
FieldAngularCoordinates(Field<T>, AngularCoordinates) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a FieldAngularCoordinates from a field and a regular AngularCoordinates.
FieldAngularCoordinates(FieldRotation<U>) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a FieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.
FieldApsideDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Finder for apside crossing events.
FieldApsideDetector(FieldOrbit<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector
Build a new instance.
FieldApsideDetector(T, FieldOrbit<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector
Build a new instance.
FieldArrayDictionary<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
String → CalculusFieldElement[] mapping, for small number of keys.
FieldArrayDictionary(Field<T>) - Constructor for class org.orekit.utils.FieldArrayDictionary
Constructor with default initial capacity.
FieldArrayDictionary(Field<T>, int) - Constructor for class org.orekit.utils.FieldArrayDictionary
Constructor with specified capacity.
FieldArrayDictionary(FieldArrayDictionary<T>) - Constructor for class org.orekit.utils.FieldArrayDictionary
Constructor from another dictionary.
FieldArrayDictionary(Field<T>, Map<String, T[]>) - Constructor for class org.orekit.utils.FieldArrayDictionary
Constructor from a map.
FieldArrayDictionary.Entry - Class in org.orekit.utils
Entry in a dictionary.
FieldAttitude<T extends CalculusFieldElement<T>> - Class in org.orekit.attitudes
This class handles attitude definition at a given date.
FieldAttitude(Frame, TimeStampedFieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, FieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, Rotation, Vector3D, Vector3D, Field<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(Field<T>, Attitude) - Constructor for class org.orekit.attitudes.FieldAttitude
Builds an instance for a regular Attitude.
FieldAuxiliaryElements<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Container class for common parameters used by all DSST forces.
FieldAuxiliaryElements(FieldOrbit<T>, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Simple constructor.
FieldBodiesElements<T extends CalculusFieldElement<T>> - Class in org.orekit.data
Elements of the bodies having an effect on nutation.
FieldBodiesElements(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldBodiesElements
Simple constructor.
FieldBoundedPropagator<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation
This interface is intended for ephemerides valid only during a time range.
FieldBrouwerLyddanePropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical
This class propagates a FieldSpacecraftState using the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).
FieldBrouwerLyddanePropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Private helper constructor.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, T, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, mass and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, T, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, attitude provider and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, attitude provider and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Private helper constructor.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, PropagationType, double, double, int) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
FieldCartesianOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits
This class holds Cartesian orbital parameters.
FieldCartesianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from Cartesian parameters.
FieldCartesianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from Cartesian parameters.
FieldCartesianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from any kind of orbital parameters.
FieldCircularOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits
This class handles circular orbital parameters.
FieldCircularOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Creates a new instance.
FieldCircularOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Creates a new instance.
FieldCircularOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from Cartesian parameters.
FieldCircularOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from Cartesian parameters.
FieldCircularOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from any kind of orbital parameters.
FieldCjSjCoefficient<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Sj(k, h) and the Cj(k, h) series and their partial derivatives with respect to k and h.
FieldCjSjCoefficient(T, T, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Cj(k, h) and Sj(k, h) constructor.
FieldCombinedDerivatives<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.integration
Container for additional derivatives.
FieldCombinedDerivatives(T[], T[]) - Constructor for class org.orekit.propagation.integration.FieldCombinedDerivatives
Simple constructor.
FieldContinueOnEvent<KK extends FieldEventDetector<T>,T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Event handler which will always return continue as a state.
FieldContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldContinueOnEvent
 
FieldDateDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Finder for date events.
FieldDateDetector(T, T, FieldTimeStamped<T>...) - Constructor for class org.orekit.propagation.events.FieldDateDetector
Build a new instance.
FieldDateDetector(FieldAbsoluteDate<T>) - Constructor for class org.orekit.propagation.events.FieldDateDetector
Build a new instance.
FieldDeepSDP4<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle
This class contains the methods that compute deep space perturbation terms.
FieldDeepSDP4(FieldTLE<T>, AttitudeProvider, T, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldDeepSDP4
Constructor for a unique initial TLE.
FieldDeepSDP4(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldDeepSDP4
Constructor for a unique initial TLE.
FieldDelaunayArguments<T extends CalculusFieldElement<T>> - Class in org.orekit.data
Delaunay arguments used for nutation or tides.
FieldDelaunayArguments(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldDelaunayArguments
Simple constructor.
FieldDSSTNewtonianAttractionContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common "field" parameters used in DSSTNewtonianAttraction.
FieldDSSTPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst
This class propagates orbits using the DSST theory.
FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>, PropagationType) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Create a new instance of DSSTPropagator.
FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>, PropagationType, AttitudeProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Create a new instance of DSSTPropagator.
FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Create a new instance of DSSTPropagator.
FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Create a new instance of DSSTPropagator.
FieldDSSTTesseralContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common "field" parameters used in DSSTTesseral.
FieldDSSTThirdBodyContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common "field" parameters used in DSSTThirdBody.
FieldDSSTZonalContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common "field" parameters used in DSSTZonal.
FieldEcksteinHechlerPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical
This class propagates a FieldSpacecraftState using the analytical Eckstein-Hechler model.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Private helper constructor.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, T, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from orbit and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Private helper constructor.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double, PropagationType, double, int) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEclipseDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Finder for satellite eclipse related events.
FieldEclipseDetector(PVCoordinatesProvider, double, PVCoordinatesProvider, double, Field<T>) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector
Build a new eclipse detector.
FieldEclipseDetector(T, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector
Build a new eclipse detector.
FieldEclipseDetector(T, T, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector
Build a new eclipse detector.
FieldElevationDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.
FieldElevationDetector(Field<T>, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.
FieldElevationDetector(T, T, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.
FieldEphemerisGenerator<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation
Generator for ephemerides.
FieldEquinoctialOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits
This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
FieldEquinoctialOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Creates a new instance.
FieldEquinoctialOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Creates a new instance.
FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from Cartesian parameters.
FieldEquinoctialOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from Cartesian parameters.
FieldEquinoctialOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from any kind of orbital parameters.
FieldEventDetector<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.events
This interface represents space-dynamics aware events detectors.
FieldEventHandler<KK extends FieldEventDetector<T>,T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.events.handlers
An interface defining how to override event handling behavior in the standard propagator eventing classes without requiring subclassing.
FieldEventsLogger<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
This class logs events detectors events during propagation.
FieldEventsLogger() - Constructor for class org.orekit.propagation.events.FieldEventsLogger
Simple constructor.
FieldEventsLogger.FieldLoggedEvent<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Class for logged events entries.
FieldEventState<D extends FieldEventDetector<T>,T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
This class handles the state for one event detector during integration steps.
FieldEventState(D) - Constructor for class org.orekit.propagation.events.FieldEventState
Simple constructor.
FieldEventState.EventOccurrence<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Class to hold the data related to an event occurrence that is needed to decide how to modify integration.
FieldFixedNumberInterpolationGrid<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolation grid where a fixed number of points are evenly spaced between the start and the end of the integration step.
FieldFixedNumberInterpolationGrid(Field<T>, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldFixedNumberInterpolationGrid
Constructor.
FieldForceModelContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
Base class for dsst force models parameter containers.
FieldForceModelContext(FieldAuxiliaryElements<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.FieldForceModelContext
Simple constructor.
FieldFunctionalDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
A detector that implements the FieldFunctionalDetector.g(FieldSpacecraftState) function using a lambda that can be set using FieldFunctionalDetector.withFunction(Function).
FieldFunctionalDetector(Field<T>) - Constructor for class org.orekit.propagation.events.FieldFunctionalDetector
Create an event detector with the default values.
FieldGammaMnsFunction<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Γmn,s(γ) function from equation 2.7.1-(13).
FieldGammaMnsFunction(int, T, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction
Simple constructor.
FieldGeodeticPoint<T extends CalculusFieldElement<T>> - Class in org.orekit.bodies
Point location relative to a 2D body surface, using CalculusFieldElement.
FieldGeodeticPoint(T, T, T) - Constructor for class org.orekit.bodies.FieldGeodeticPoint
Build a new instance.
FieldGHIJjsPolynomials<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Gjs, Hjs, Ijs and Jjs polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
FieldGHIJjsPolynomials(T, T, T, T) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Create a set of Gjs, Hjs, Ijs and Jjs polynomials.
FieldGHmsjPolynomials<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Gmsj and the Hmsj polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
FieldGHmsjPolynomials(T, T, T, T, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Create a set of Gmsj and Hmsj polynomials.
FieldHansenTesseralLinear<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t!=0 and n < 0.
FieldHansenTesseralLinear(int, int, int, int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear
Constructor.
FieldHansenThirdBodyLinear<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n > 0.
FieldHansenThirdBodyLinear(int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear
Constructor.
FieldHansenZonalLinear<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n < 0.
FieldHansenZonalLinear(int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
Constructor.
FieldIntegrableFunction(FieldSpacecraftState<T>, boolean, int, T[], Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldIntegrableFunction
Build a new instance with a new field.
FieldIntegratedEphemeris<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.integration
This class stores sequentially generated orbital parameters for later retrieval.
FieldIntegratedEphemeris(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldStateMapper<T>, PropagationType, FieldDenseOutputModel<T>, Map<String, T[]>, List<FieldAdditionalStateProvider<T>>, String[]) - Constructor for class org.orekit.propagation.integration.FieldIntegratedEphemeris
FieldIntegratedEphemeris(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldStateMapper<T>, PropagationType, FieldDenseOutputModel<T>, FieldArrayDictionary<T>, List<FieldAdditionalStateProvider<T>>, String[]) - Constructor for class org.orekit.propagation.integration.FieldIntegratedEphemeris
FieldIntegratedEphemeris(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldStateMapper<T>, PropagationType, FieldDenseOutputModel<T>, FieldArrayDictionary<T>, List<FieldAdditionalStateProvider<T>>, String[], int[]) - Constructor for class org.orekit.propagation.integration.FieldIntegratedEphemeris
Creates a new instance of IntegratedEphemeris.
FieldInterpolationGrid<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.semianalytical.dsst.utilities
Interface for interpolation grids.
FieldKeplerianOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits
This class handles traditional Keplerian orbital parameters.
FieldKeplerianOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Creates a new instance.
FieldKeplerianOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Creates a new instance.
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from Cartesian parameters.
FieldKeplerianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from Cartesian parameters.
FieldKeplerianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from any kind of orbital parameters.
FieldKeplerianPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical
Simple Keplerian orbit propagator.
FieldKeplerianPropagator(FieldOrbit<T>) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build a propagator from orbit only.
FieldKeplerianPropagator(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build a propagator from orbit and central attraction coefficient μ.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build a propagator from orbit and attitude provider.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build a propagator from orbit, attitude provider and central attraction coefficient μ.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, T, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
FieldLatitudeCrossingDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Detector for geographic latitude crossing.
FieldLatitudeCrossingDetector(Field<T>, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Build a new detector.
FieldLatitudeCrossingDetector(T, T, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Build a detector.
FieldLegendrePolynomials<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
Computes the Pnm(t) coefficients.
FieldLegendrePolynomials(int, int, T) - Constructor for class org.orekit.utils.FieldLegendrePolynomials
Create Legendre polynomials for the given degree and order.
FieldLnsCoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Lns(γ).
FieldLnsCoefficients(int, int, T[][], TreeMap<CoefficientsFactory.NSKey, Double>, T, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients
Create a set of Lns(γ) coefficients.
FieldManeuverTriggersResetter<T extends CalculusFieldElement<T>> - Interface in org.orekit.forces.maneuvers.trigger
Resetter for maneuver triggers.
FieldMaxGapInterpolationGrid<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolation grid where points obey a maximum time gap.
FieldMaxGapInterpolationGrid(Field<T>, T) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldMaxGapInterpolationGrid
Constructor.
FieldNodeDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Finder for node crossing events.
FieldNodeDetector(FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector
Build a new instance.
FieldNodeDetector(T, FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector
Build a new instance.
FieldNumericalPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.numerical
This class propagates orbits using numerical integration.
FieldNumericalPropagator(Field<T>, FieldODEIntegrator<T>) - Constructor for class org.orekit.propagation.numerical.FieldNumericalPropagator
Create a new instance of NumericalPropagator, based on orbit definition mu.
FieldNumericalPropagator(Field<T>, FieldODEIntegrator<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.numerical.FieldNumericalPropagator
Create a new instance of NumericalPropagator, based on orbit definition mu.
FieldOfView - Interface in org.orekit.geometry.fov
Interface representing a spacecraft sensor Field Of View.
FieldOfViewDetector - Class in org.orekit.propagation.events
Finder for target entry/exit events with respect to a satellite sensor Field Of View.
FieldOfViewDetector(PVCoordinatesProvider, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector
Build a new instance.
FieldOfViewDetector(PVCoordinatesProvider, double, VisibilityTrigger, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector
Build a new instance.
FieldOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits
This class handles orbital parameters.
FieldOrbit(Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldOrbit
Default constructor.
FieldOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldOrbit
Set the orbit from Cartesian parameters.
FieldOrekitFixedStepHandler<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware fixed size step handler.
FieldOrekitStepHandler<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step handler.
FieldOrekitStepInterpolator<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step interpolator.
FieldOrekitStepNormalizer<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.sampling
This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.
FieldOrekitStepNormalizer(T, FieldOrekitFixedStepHandler<T>) - Constructor for class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Simple constructor.
FieldParameterDrivenDateIntervalDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events
Detector for date intervals that may be offset thanks to parameter drivers.
FieldParameterDrivenDateIntervalDetector(Field<T>, String, AbsoluteDate, double) - Constructor for class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Build a new instance.
FieldParameterDrivenDateIntervalDetector(Field<T>, String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Build a new instance.
FieldPoleCorrection<T extends CalculusFieldElement<T>> - Class in org.orekit.frames
Simple container class for pole correction parameters.
FieldPoleCorrection(T, T) - Constructor for class org.orekit.frames.FieldPoleCorrection
Simple constructor.
FieldPropagator<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation
This interface provides a way to propagate an orbit at any time.
FieldPVCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
Simple container for Position/Velocity pairs, using CalculusFieldElement.
FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates triplet with zero acceleration.
FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates triplet.
FieldPVCoordinates(Field<T>, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates from a field and a regular PVCoordinates.
FieldPVCoordinates(double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor.
FieldPVCoordinates(T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor.
FieldPVCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Subtractive constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(FieldVector3D<U>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates triplet from a FieldVector3D<FieldDerivativeStructure>.
FieldPVCoordinatesProvider<T extends CalculusFieldElement<T>> - Interface in org.orekit.utils
Interface for PV coordinates providers.
FieldRecordAndContinue<T extends FieldEventDetector<E>,E extends CalculusFieldElement<E>> - Class in org.orekit.propagation.events.handlers
Handler that will record every time an event occurs and always return Action.CONTINUE.
FieldRecordAndContinue() - Constructor for class org.orekit.propagation.events.handlers.FieldRecordAndContinue
Create a new handler using an ArrayList to store events.
FieldRecordAndContinue(List<FieldRecordAndContinue.Event<T, E>>) - Constructor for class org.orekit.propagation.events.handlers.FieldRecordAndContinue
Create a handler using the given collection to store events.
FieldRecordAndContinue.Event<T,F extends CalculusFieldElement<F>> - Class in org.orekit.propagation.events.handlers
A single event detected during propagation.
FieldSGP4<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle
This class contains methods to compute propagated coordinates with the SGP4 model.
FieldSGP4(FieldTLE<T>, AttitudeProvider, T, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldSGP4
Constructor for a unique initial TLE.
FieldSGP4(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldSGP4
Constructor for a unique initial TLE.
FieldShortPeriodicsInterpolatedCoefficient<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolated short periodics coefficients.
FieldShortPeriodicsInterpolatedCoefficient(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient
Simple constructor.
FieldShortPeriodTerms<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.semianalytical.dsst.forces
Additive short period terms contributing to the mean to osculating orbit mapping.
FieldSpacecraftState<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation
This class is the representation of a complete state holding orbit, attitude and mass information at a given date.
FieldSpacecraftState(FieldOrbit<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and attitude.
FieldSpacecraftState(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit and mass.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude and mass.
FieldSpacecraftState(FieldOrbit<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
FieldSpacecraftState(FieldOrbit<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and additional states.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit attitude and additional states.
FieldSpacecraftState(FieldOrbit<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
FieldSpacecraftState(FieldOrbit<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit, mass and additional states.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude, mass and additional states.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude, mass, additional states and derivatives.
FieldSpacecraftState(Field<T>, SpacecraftState) - Constructor for class org.orekit.propagation.FieldSpacecraftState
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and attitude.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and attitude.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude and mass.
FieldStateMapper<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.integration
This class maps between raw double elements and FieldSpacecraftState instances.
FieldStateMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngle, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.FieldStateMapper
Simple constructor.
FieldStepHandlerMultiplexer<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.sampling
This class gathers several OrekitStepHandler instances into one.
FieldStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Simple constructor.
FieldStopOnDecreasing<KK extends FieldEventDetector<T>,T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Handle a detection event and choose what to do next.
FieldStopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnDecreasing
 
FieldStopOnEvent<KK extends FieldEventDetector<T>,T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Event handler which will always return continue as a state.
FieldStopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnEvent
 
FieldStopOnIncreasing<KK extends FieldEventDetector<T>,T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Handle a detection event and choose what to do next.
FieldStopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnIncreasing
 
FieldTimeDerivativesEquations<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.numerical
Interface summing up the contribution of several forces into orbit and mass derivatives.
FieldTimeInterpolable<T extends FieldTimeInterpolable<T,KK>,KK extends CalculusFieldElement<KK>> - Interface in org.orekit.time
This interface represents objects that can be interpolated in time.
FieldTimeShiftable<T extends FieldTimeInterpolable<T,KK>,KK extends CalculusFieldElement<KK>> - Interface in org.orekit.time
This interface represents objects that can be shifted in time.
FieldTimeSpanMap<T,D extends CalculusFieldElement<D>> - Class in org.orekit.utils
Container for objects that apply to spans of time.
FieldTimeSpanMap(T, Field<D>) - Constructor for class org.orekit.utils.FieldTimeSpanMap
Create a map containing a single object, initially valid throughout the timeline.
FieldTimeSpanMap.Transition<S,D extends CalculusFieldElement<D>> - Class in org.orekit.utils
Local class holding transition times.
FieldTimeStamped<T extends CalculusFieldElement<T>> - Interface in org.orekit.time
This interface represents objects that have a AbsoluteDate date attached to them.
FieldTLE<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle
This class is a container for a single set of TLE data.
FieldTLE(Field<T>, String, String) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE
Simple constructor from unparsed two lines.
FieldTLE(Field<T>, String, String, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE
Simple constructor from unparsed two lines using the given time scale as UTC.
FieldTLE(int, char, int, int, String, int, int, FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, int, double) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE
Simple constructor from already parsed elements.
FieldTLE(int, char, int, int, String, int, int, FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, int, double, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE
Simple constructor from already parsed elements using the given time scale as UTC.
FieldTLEPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle
This class provides elements to propagate TLE's.
FieldTLEPropagator(FieldTLE<T>, AttitudeProvider, T, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Protected constructor for derived classes.
FieldTLEPropagator(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Protected constructor for derived classes.
FieldTransform<T extends CalculusFieldElement<T>> - Class in org.orekit.frames
Transformation class in three dimensional space.
FieldTransform(Field<T>, Transform) - Constructor for class org.orekit.frames.FieldTransform
Build a transform from a regular transform.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform, with its first time derivative.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform, with its first and second time derivatives.
FieldTransform(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform, with its first time derivative.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldAngularCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldTransform<T>, FieldTransform<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a transform by combining two existing ones.
FieldTransformGenerator<T extends CalculusFieldElement<T>> - Class in org.orekit.frames
Generator to use field transforms in GenericTimeStampedCache.
FieldTransformGenerator(Field<T>, int, TransformProvider, double) - Constructor for class org.orekit.frames.FieldTransformGenerator
simple constructor.
FIFTIES_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
FIFTIES_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for 1950 dates: 1950-01-01.
FileFormat - Enum in org.orekit.files.ccsds.utils
Enumerate for file format.
FilesListCrawler - Class in org.orekit.data
Provider for data files in an explicit list.
FilesListCrawler(File...) - Constructor for class org.orekit.data.FilesListCrawler
Build a data classpath crawler.
fillHalfRow(T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a single vector.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a single vector.
fillHalfRow(double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHistory(IERSConventions.NutationCorrectionConverter, SortedSet<EOPEntry>) - Method in class org.orekit.files.sinex.SinexLoader
Load celestial body.
fillHistory(IERSConventions.NutationCorrectionConverter, SortedSet<EOPEntry>) - Method in interface org.orekit.frames.EOPHistoryLoader
Load celestial body.
filter(DataSource) - Method in interface org.orekit.data.DataFilter
Filter the data source.
filter(DataSource) - Method in class org.orekit.data.GzipFilter
Filter the data source.
filter(DataSource) - Method in class org.orekit.data.UnixCompressFilter
Filter the data source.
filter(ObservedMeasurement<T>, SpacecraftState) - Method in class org.orekit.estimation.measurements.filtering.ElevationFilter
Apply a filter to an observed measurement.
filter(ObservedMeasurement<T>, SpacecraftState) - Method in interface org.orekit.estimation.measurements.filtering.MeasurementFilter
Apply a filter to an observed measurement.
filter(ObservedMeasurement<T>, SpacecraftState) - Method in class org.orekit.estimation.measurements.filtering.ResidualFilter
Apply a filter to an observed measurement.
filter(DataSource) - Method in class org.orekit.gnss.HatanakaCompressFilter
Filter the data source.
filter(boolean) - Method in class org.orekit.utils.ParameterDriversList
Filter parameters to keep only one type of selection status.
filterData(ObservationData, ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter
This method filters the provided data given the state of the filter.
filterData(ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencyHatchFilter
This method filters the provided data given the state of the filter.
filterDataSet(List<ObservationDataSet>, SatelliteSystem, int, ObservationType, ObservationType) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother
Applies a Dual Frequency Hatch filter to a list of ObservationDataSet.
filterDataSet(List<ObservationDataSet>, SatelliteSystem, int, ObservationType) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother
Applies a Single Frequency Hatch filter to a list of ObservationDataSet.
FiltersManager - Class in org.orekit.data
Manager for data filters.
FiltersManager() - Constructor for class org.orekit.data.FiltersManager
Build an empty manager.
FilterType - Enum in org.orekit.propagation.events
Enumerate for filtering events.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Finalize data after parsing.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Finalize estimation.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Finalize estimation.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Finalize header after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Finalize metadata after parsing.
finalizeMetadata(ContextBinding) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Finalize the metadata.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Finalize metadata after parsing.
finalizeOperationsObservationGrid() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Finalize estimation operations on the observation grid.
findByName(String) - Method in class org.orekit.utils.ParameterDriversList
Find a delegating driver by name.
findEOP(Frame) - Static method in class org.orekit.frames.FramesFactory
Retrieve EOP from a frame hierarchy.
findSatelliteAntenna(SatelliteSystem, int) - Method in class org.orekit.gnss.antenna.AntexLoader
Find the time map for a specific satellite antenna.
finish(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter
Finalize propagation.
finish(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter
Finalize propagation.
finish(SpacecraftState) - Method in class org.orekit.files.ilrs.StreamingCpfWriter.Segment
Finalize propagation.
finish(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler
Finalize propagation.
finish(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler
Finalize propagation.
finish(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Finalize propagation.
finish(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Finalize propagation.
finish(List<SpacecraftState>) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler
Finalize propagation.
finish(SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler
Finalize propagation.
finish(SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Finalize propagation.
finish(SpacecraftState) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Finalize propagation.
finish(SpacecraftState) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Finalize propagation.
finished(TaskEvent) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
 
FiniteDifferencePropagatorConverter - Class in org.orekit.propagation.conversion
Propagator converter using finite differences to compute the Jacobian.
FiniteDifferencePropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter
Simple constructor.
fit() - Method in class org.orekit.utils.SecularAndHarmonic
Fit parameters.
FixedFrameBuilder - Class in org.orekit.attitudes
Builder that assumes angular coordinates are given in a fixed frame.
FixedFrameBuilder(Frame) - Constructor for class org.orekit.attitudes.FixedFrameBuilder
Creates new instance.
FixedNumberInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolation grid where a fixed number of points are evenly spaced between the start and the end of the integration step.
FixedNumberInterpolationGrid(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid
Constructor.
FixedRate - Class in org.orekit.attitudes
This class handles a simple attitude provider at constant rate around a fixed axis.
FixedRate(Attitude) - Constructor for class org.orekit.attitudes.FixedRate
Creates a new instance.
FixedStepSelector - Class in org.orekit.time
Selector generating a continuous stream of dates separated by a constant step.
FixedStepSelector(double, TimeScale) - Constructor for class org.orekit.time.FixedStepSelector
Simple constructor.
FixedTransformProvider - Class in org.orekit.frames
Transform provider using fixed transform.
FixedTransformProvider(Transform) - Constructor for class org.orekit.frames.FixedTransformProvider
Simple constructor.
FixedTroposphericDelay - Class in org.orekit.models.earth.troposphere
A static tropospheric model that interpolates the actual tropospheric delay based on values read from a configuration file (tropospheric-delay.txt) via the DataProvidersManager.
FixedTroposphericDelay(double[], double[], double[][]) - Constructor for class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Creates a new FixedTroposphericDelay instance.
FixedTroposphericDelay(String) - Constructor for class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the default data context.
FixedTroposphericDelay(String, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the specified data manager.
fixIntegerAmbiguities(int, List<ParameterDriver>, RealMatrix) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Fix integer ambiguities.
FLOW_RATE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Parameter name for flow rate.
FLOW_RATE_SCALE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Flow rate scaling factor.
FootprintOverlapDetector - Class in org.orekit.propagation.events
Detector triggered by geographical region entering/leaving a spacecraft sensor Field Of View.
FootprintOverlapDetector(FieldOfView, OneAxisEllipsoid, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.FootprintOverlapDetector
Build a new instance.
ForceModel - Interface in org.orekit.forces
This interface represents a force modifying spacecraft motion.
ForceModelContext - Class in org.orekit.propagation.semianalytical.dsst.forces
Base class for dsst force models attributes containers.
ForceModelContext(AuxiliaryElements) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.ForceModelContext
Simple constructor.
forEach(Consumer<T>) - Method in class org.orekit.utils.TimeSpanMap
Performs an action for each non-null element of map.
format(double) - Static method in class org.orekit.utils.AccurateFormatter
Format a double number.
format(int, int, int, int, int, double) - Static method in class org.orekit.utils.AccurateFormatter
Format a date.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.Aem
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.Apm
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.cdm.Cdm
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.Oem
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.tdm.Tdm
Key for format version.
formatUtcOffset() - Method in class org.orekit.time.TimeComponents
Get the UTC offset as a string in ISO8601 format.
Frame - Class in org.orekit.frames
Tridimensional references frames class.
Frame(Frame, Transform, String) - Constructor for class org.orekit.frames.Frame
Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, TransformProvider, String) - Constructor for class org.orekit.frames.Frame
Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.Frame
Build a frame from its transform with respect to its parent.
Frame(Frame, TransformProvider, String, boolean) - Constructor for class org.orekit.frames.Frame
Build a frame from its transform with respect to its parent.
FrameAncestorException - Exception in org.orekit.errors
This class is the base class for exception thrown by the UpdatableFrame.updateTransform method.
FrameAncestorException(Localizable, Object...) - Constructor for exception org.orekit.errors.FrameAncestorException
Simple constructor.
FrameFacade - Class in org.orekit.files.ccsds.definitions
Facade in front of several frames types in CCSDS messages.
FrameFacade(Frame, CelestialBodyFrame, OrbitRelativeFrame, SpacecraftBodyFrame, String) - Constructor for class org.orekit.files.ccsds.definitions.FrameFacade
Simple constructor.
Frames - Interface in org.orekit.frames
A collection of commonly used Frames.
FramesFactory - Class in org.orekit.frames
Factory for predefined reference frames.
freeze() - Method in class org.orekit.frames.FieldTransform
Get a frozen transform.
freeze() - Method in class org.orekit.frames.Transform
Get a frozen transform.
freezeColumnsNames() - Method in class org.orekit.propagation.AbstractMatricesHarvester
Freeze the names of the Jacobian columns.
freezeColumnsNames() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Freeze the names of the Jacobian columns.
freezeColumnsNames() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Freeze the names of the Jacobian columns.
Frequency - Enum in org.orekit.gnss
Enumerate for GNSS frequencies.
FrequencyPattern - Class in org.orekit.gnss.antenna
Pattern for GNSS antenna model on one frequency.
FrequencyPattern(Vector3D, PhaseCenterVariationFunction) - Constructor for class org.orekit.gnss.antenna.FrequencyPattern
Simple constructor.
fromSeconds(int, double, double, int) - Static method in class org.orekit.time.TimeComponents
Build a time from the second number within the day.
fromSI(double) - Method in class org.orekit.utils.units.Unit
Convert a value from SI units.
fromSI(Double) - Method in class org.orekit.utils.units.Unit
Convert a value from SI units.
FunctionalDetector - Class in org.orekit.propagation.events
A detector that implements the FunctionalDetector.g(SpacecraftState) function using a lambda that can be set using FunctionalDetector.withFunction(ToDoubleFunction).
FunctionalDetector() - Constructor for class org.orekit.propagation.events.FunctionalDetector
Create an event detector with the default values.
FundamentalNutationArguments - Class in org.orekit.data
Class computing the fundamental arguments for nutation and tides.
FundamentalNutationArguments(IERSConventions, TimeScale, InputStream, String) - Constructor for class org.orekit.data.FundamentalNutationArguments
Build a model of fundamental arguments from an IERS table file.
FundamentalNutationArguments(IERSConventions, TimeScale, InputStream, String, TimeScales) - Constructor for class org.orekit.data.FundamentalNutationArguments
Build a model of fundamental arguments from an IERS table file.
FundamentalNutationArguments(IERSConventions, TimeScale, List<double[]>) - Constructor for class org.orekit.data.FundamentalNutationArguments
Build a model of fundamental arguments from an IERS table file.
FundamentalNutationArguments(IERSConventions, TimeScale, List<double[]>, TimeScales) - Constructor for class org.orekit.data.FundamentalNutationArguments
Build a model of fundamental arguments from an IERS table file.
FUTURE_INFINITY - Static variable in class org.orekit.time.AbsoluteDate
Dummy date at infinity in the future direction.

G

g(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AdapterDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AlignmentDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AltitudeDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AngularSeparationDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ApsideDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.BooleanDetector
 
g(SpacecraftState) - Method in class org.orekit.propagation.events.DateDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EclipseDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventShifter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventSlopeFilter
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldApsideDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldDateDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector
 
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Compute the value of the detection function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FieldOfViewDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FunctionalDetector
 
g(SpacecraftState) - Method in class org.orekit.propagation.events.GeographicZoneDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundAtNightDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.HaloXZPlaneCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.MagneticFieldDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.NegateDetector
 
g(SpacecraftState) - Method in class org.orekit.propagation.events.NodeDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.PositionAngleDetector
Compute the value of the detection function.
G0_STANDARD_GRAVITY - Static variable in interface org.orekit.utils.Constants
Standard gravity constant, used in maneuvers definition: 9.80665 m/s².
Galileo - Class in org.orekit.gnss.attitude
Attitude providers for Galileo navigation satellites.
Galileo(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Galileo
Simple constructor.
GALILEO_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of the earth's rotation rate in rad/s for Galileo user.
GALILEO_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.
GALILEO_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for Galileo System Time: 1999-08-22.
GALILEO_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Earth's universal gravitational parameter for Galileo user in m³/s².
GALILEO_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Number of weeks in the Galileo cycle.
GalileoAlmanac - Class in org.orekit.propagation.analytical.gnss.data
Class for Galileo almanac.
GalileoAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Build a new almanac.
GalileoNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a Galileo navigation message.
GalileoNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Constructor.
GalileoScale - Class in org.orekit.time
Galileo system time scale.
GammaMnsFunction - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Γmn,s(γ) function from equation 2.7.1-(13).
GammaMnsFunction(int, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Simple constructor.
generate(List<OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.ContinuousScheduler
Generate a sequence of measurements.
generate(List<OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.EventBasedScheduler
Generate a sequence of measurements.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.Generator
Generate measurements.
generate(List<OrekitStepInterpolator>) - Method in interface org.orekit.estimation.measurements.generation.Scheduler
Generate a sequence of measurements.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.FieldTransformGenerator
Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.TransformGenerator
Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedGenerator
Generate a chronologically sorted list of entries to be cached.
generateCartesianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Generate a Cartesian orbit.
generateException(Exception) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Generate a parse exception for this entry.
generateKeplerianOrbit(Frame) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Generate a keplerian orbit.
generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Generate a keplerian orbit.
generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Generate a keplerian orbit.
generateSpacecraftState() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Generate spacecraft state from the CartesianOrbit generated by generateCartesianOrbit.
generateSpacecraftState() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Generate spacecraft state from the CartesianOrbit generated by generateCartesianOrbit.
generateTLE() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Generate TLE from OMM file.
Generator - Class in org.orekit.estimation.measurements.generation
Main generator for observed measurements.
Generator() - Constructor for class org.orekit.estimation.measurements.generation.Generator
Build a generator with no sequences generator.
Generator - Interface in org.orekit.files.ccsds.utils.generation
Generation interface for CCSDS messages.
GenericGNSS - Class in org.orekit.gnss.attitude
Attitude providers for navigation satellites for which no specialized model is known.
GenericGNSS(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GenericGNSS
Simple constructor.
GenericTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils
Generic thread-safe cache for time-stamped data.
GenericTimeStampedCache(int, int, double, double, TimeStampedGenerator<T>) - Constructor for class org.orekit.utils.GenericTimeStampedCache
Simple constructor.
GeodeticPoint - Class in org.orekit.bodies
Point location relative to a 2D body surface.
GeodeticPoint(double, double, double) - Constructor for class org.orekit.bodies.GeodeticPoint
Build a new instance.
GeographicZoneDetector - Class in org.orekit.propagation.events
Detector for entry/exit of a zone defined by geographic boundaries.
GeographicZoneDetector(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
Build a new detector.
GeographicZoneDetector(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
Build a detector.
Geoid - Class in org.orekit.models.earth
A geoid is a level surface of the gravity potential of a body.
Geoid(NormalizedSphericalHarmonicsProvider, ReferenceEllipsoid) - Constructor for class org.orekit.models.earth.Geoid
Creates a geoid from the given geopotential, reference ellipsoid and the assumptions in the comment for Geoid.
GeoMagneticElements - Class in org.orekit.models.earth
Contains the elements to represent a magnetic field at a single point.
GeoMagneticElements(Vector3D) - Constructor for class org.orekit.models.earth.GeoMagneticElements
Construct a new element with the given field vector.
GeoMagneticField - Class in org.orekit.models.earth
Used to calculate the geomagnetic field at a given geodetic point on earth.
GeoMagneticField(String, double, int, int, double, double) - Constructor for class org.orekit.models.earth.GeoMagneticField
Create a new geomagnetic field model with the given parameters.
GeoMagneticFieldFactory - Class in org.orekit.models.earth
Factory for different GeoMagneticField models.
GeoMagneticFieldFactory.FieldModel - Enum in org.orekit.models.earth
The currently supported geomagnetic field models.
GeoMagneticFields - Interface in org.orekit.models.earth
Methods for obtaining geomagnetic fields.
GeoMagneticModelLoader - Class in org.orekit.models.earth
Loads geomagnetic field models from a given input stream.
GeoMagneticModelLoader() - Constructor for class org.orekit.models.earth.GeoMagneticModelLoader
 
GeometryFreeCombination - Class in org.orekit.estimation.measurements.gnss
Geometry-free combination.
GeometryFreeCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss
Geometry free cycle slip detectors.
GeometryFreeCycleSlipDetector(double, double, int) - Constructor for class org.orekit.estimation.measurements.gnss.GeometryFreeCycleSlipDetector
Constructor.
get(String) - Method in class org.orekit.utils.DoubleArrayDictionary
Get the value corresponding to a key.
get(String) - Method in class org.orekit.utils.FieldArrayDictionary
Get the value corresponding to a key.
get(FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Get the entry valid at a specified date.
get(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Get the entry valid at a specified date.
get24HoursKp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the last 24H mean geomagnetic index.
get24HoursKp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
The Kp index is derived from the Ap index.
get24HoursKp(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Get the last 24H mean geomagnetic index.
getA() - Method in class org.orekit.bodies.Ellipse
Get the semi major axis.
getA() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the first semi-axis.
getA() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the orbit semi-major axis.
getA() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Returns the a coefficients array.
getA() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Returns the a coefficients array.
getA() - Method in class org.orekit.orbits.CartesianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.CircularOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.KeplerianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.Orbit
Get the semi-major axis.
getA() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the semi-major axis.
getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.SpacecraftState
Get the semi-major axis.
getAbscissaGrid() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the abscissa grid for the interpolation function.
getAbsoluteDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the transition field absolute date.
getAbsPVA() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the absolute position-velocity-acceleration.
getAbsPVA() - Method in class org.orekit.propagation.SpacecraftState
Get the absolute position-velocity-acceleration.
getAcceleration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get acceleration.
getAcceleration(SpacecraftState, Attitude, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration(FieldSpacecraftState<T>, FieldAttitude<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration(SpacecraftState, Attitude, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration(FieldSpacecraftState<T>, FieldAttitude<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration() - Method in class org.orekit.frames.FieldTransform
Get the second time derivative of the translation.
getAcceleration() - Method in class org.orekit.frames.Transform
Get the second time derivative of the translation.
getAcceleration() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the acceleration.
getAcceleration() - Method in class org.orekit.utils.PVCoordinates
Gets the acceleration.
getAccelerationDirectionSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get one σ angular off-nominal acceleration direction.
getAccelerationInterpolation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get interpolation mode between current and next acceleration line.
getAccelerationMagnitudeSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get one σ percent error on acceleration magnitude.
getAccelerationModel(AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Get the AccelerationModel model valid at a date.
getAccelerationModelSpan(AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Get the AccelerationModel TimeSpanMap.Span containing a specified date.
getAccuracy(int) - Method in class org.orekit.files.sp3.SP3
Get the formal accuracy for a satellite.
getAccuracy() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
Get the formal accuracy for this satellite.
getAccuracy() - Method in interface org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.AccuracyProvider
Get the accuracy of the ephemeris data from an accuracy index.
getAccuracy() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.GlonassUserRangeAccuracy
Get the accuracy of the ephemeris data from an accuracy index.
getAccuracy() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.SignalInSpaceAccuracy
Get the accuracy of the ephemeris data from an accuracy index.
getAccuracy() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.UserRangeAccuracy
Get the accuracy of the ephemeris data from an accuracy index.
getAccuracyProvider() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
Get the accuracy provider of the ephemeris message.
getAction() - Method in class org.orekit.propagation.events.EventState.EventOccurrence
Get the user requested action.
getAction() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence
Get the user requested action.
getActualOdSpan() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the actual OD time based on the observations available and the RECOMMENDED_OD_SPAN.
getActualOdSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get actual time span used for the OD of the object.
getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the adapted propagator.
getAdditionalDerivatives() - Method in class org.orekit.propagation.integration.CombinedDerivatives
Get the derivatives related to the additional state.
getAdditionalDerivatives() - Method in class org.orekit.propagation.integration.FieldCombinedDerivatives
Get the derivatives related to the additional state.
getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the list of additional equations.
getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get an unmodifiable list of providers for additional derivatives.
getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get an unmodifiable list of providers for additional derivatives.
getAdditionalEquations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
getAdditionalParametersBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Get the additional parameters logical block.
getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.Duration
Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate
Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
Get the additional state.
getAdditionalState(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider
Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Get the additional state.
getAdditionalState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
Get the additional state.
getAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState
Get an additional state.
getAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState
Get an additional state.
getAdditionalStateDerivative(String) - Method in class org.orekit.propagation.FieldSpacecraftState
Get an additional state derivative.
getAdditionalStateDerivative(String) - Method in class org.orekit.propagation.SpacecraftState
Get an additional state derivative.
getAdditionalStateDimension() - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Compute the length of the one-dimensional additional state array needed.
getAdditionalStateProviders() - Method in class org.orekit.propagation.AbstractPropagator
Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in interface org.orekit.propagation.FieldPropagator
Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in interface org.orekit.propagation.Propagator
Get an unmodifiable list of providers for additional state.
getAdditionalStates() - Method in class org.orekit.propagation.FieldSpacecraftState
Deprecated.
getAdditionalStates() - Method in class org.orekit.propagation.SpacecraftState
Deprecated.
getAdditionalStatesDerivatives() - Method in class org.orekit.propagation.FieldSpacecraftState
Get an unmodifiable map of additional states derivatives.
getAdditionalStatesDerivatives() - Method in class org.orekit.propagation.SpacecraftState
Get an unmodifiable map of additional states derivatives.
getAdditionalStatesValues() - Method in class org.orekit.propagation.FieldSpacecraftState
Get an unmodifiable map of additional states.
getAdditionalStatesValues() - Method in class org.orekit.propagation.SpacecraftState
Get an unmodifiable map of additional states.
getAdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the Unique identifier of Attitude Data Message linked to this Orbit Data Message.
getADot() - Method in class org.orekit.orbits.CartesianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.CircularOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.Orbit
Get the semi-major axis derivative.
getAe() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the value of the central body reference radius.
getAe() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the central body reference radius.
getAe() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the value of the central body reference radius.
getAf0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the the SV Clock Bias Correction Coefficient.
getAf0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
Gets the Zeroth Order Clock Correction.
getAf1() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the SV Clock Drift Correction Coefficient.
getAf1() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
Gets the First Order Clock Correction.
getAf2() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the Drift Rate Correction Coefficient.
getAf2() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the Drift Rate Correction Coefficient.
getAf2() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
Gets the Second Order Clock Correction.
getAfter() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the entry valid after transition.
getAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the entry valid after transition.
getAgency() - Method in class org.orekit.files.sp3.SP3
Returns the agency that prepared this SP3 file.
getAgencyName() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the agency name.
getAgencyName() - Method in class org.orekit.gnss.navigation.RinexNavigation
Getter for the agency name.
getAgencyName() - Method in class org.orekit.gnss.RinexObservationHeader
Get name of the agency.
getAGf0() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Gets the Zeroth Order Clock Correction.
getAGf0() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Gets the Zeroth Order Clock Correction.
getAGf1() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Gets the First Order Clock Correction.
getAGf1() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Gets the First Order Clock Correction.
getAlbedoGridSize() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get albedo grid size.
getAlbedoModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get albedo model.
getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector
Get the alignment angle (rad).
getAll() - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get all of the data in this cache.
getAllAmbiguityDrivers() - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Get all the ambiguity parameters drivers.
getAllForceModels() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Get the list of all force models.
getAllForceModels() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Get the list of all force models.
getAllForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAllForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAllForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAllForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAlmanacs() - Method in class org.orekit.gnss.SEMParser
Gets all the GPS almanacs read from the file.
getAlmanacs() - Method in class org.orekit.gnss.YUMAParser
Gets all the GPS almanacs read from the file.
getAlpha() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Returns the alpha coefficients array.
getAlpha(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit
Get the latitude argument.
getAlpha(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit
Get the latitude argument.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get direction cosine α for central body.
getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit
Get the latitude argument derivative.
getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit
Get the latitude argument derivative.
getAlphaE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric latitude argument.
getAlphaE() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric latitude argument.
getAlphaEDot() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric latitude argument derivative.
getAlphaEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric latitude argument derivative.
getAlphaM() - Method in class org.orekit.orbits.CircularOrbit
Get the mean latitude argument.
getAlphaM() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean latitude argument.
getAlphaMDot() - Method in class org.orekit.orbits.CircularOrbit
Get the mean latitude argument derivative.
getAlphaMDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean latitude argument derivative.
getAlphaV() - Method in class org.orekit.orbits.CircularOrbit
Get the true latitude argument.
getAlphaV() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true latitude argument.
getAlphaVDot() - Method in class org.orekit.orbits.CircularOrbit
Get the true latitude argument derivative.
getAlphaVDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true latitude argument derivative.
getAlternateNames() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the alternate names for this space object.
getAltitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the altitude.
getAltitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the altitude.
getAltitude() - Method in class org.orekit.propagation.events.AltitudeDetector
Get the threshold altitude value.
getAltitude() - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Get the threshold altitude value.
getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
Get the driver for phase ambiguity.
getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
Get the driver for phase ambiguity.
getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.Phase
Get the driver for phase ambiguity.
getAmplifierBandwidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the amplifier bandwidth.
getAmplifierGain() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the amplifier gain.
getAmplifierInUse() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the amplifier in use.
getAnalysisCenterID() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the analysis center ID.
getAnalysisCenterName() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the analysis center name.
getAncestor(int) - Method in class org.orekit.frames.Frame
Get the nth ancestor of the frame.
getAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector
Get the fixed angle to be crossed (radians).
getAngle() - Method in class org.orekit.utils.units.Unit
Get the angle exponent.
getAnglesData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the angles data for the data block.
getAngleType() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for angleType.
getAngular() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary angular part.
getAngular() - Method in class org.orekit.frames.Transform
Get the underlying elementary angular part.
getAngularCoordinates() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemData
Get an unmodifiable view of the data points.
getAngularCoordinates() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get an unmodifiable list of attitude data lines.
getAngularCoordinates() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get an unmodifiable list of attitude data lines.
getAngularCoordinates() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get an unmodifiable list of attitude data lines.
getAngularDerivativesFilter() - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Get the angular derivative filter corresponding to the attitude data.
getAngularVelocity() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the mean angular velocity of the Earth for the GNSS model.
getAngularVelocity() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the mean angular velocity of the Earth of the GNSS model.
getAngularVelocity() - Method in class org.orekit.utils.FieldPVCoordinates
Get the angular velocity (spin) of this point as seen from the origin.
getAngularVelocity() - Method in class org.orekit.utils.PVCoordinates
Get the angular velocity (spin) of this point as seen from the origin.
getAnomaly() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the orbit anomaly.
getAnomaly(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the anomaly.
getAnomaly(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit
Get the anomaly.
getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the anomaly derivative.
getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit
Get the anomaly derivative.
getAnomalyType() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the type of anomaly (true or mean).
getAntennaAzimuth() - Method in class org.orekit.gnss.RinexObservationHeader
Get the azimuth of the zero direction of a fixed antenna.
getAntennaBSight() - Method in class org.orekit.gnss.RinexObservationHeader
Get the antenna B.Sight.
getAntennaHeight() - Method in class org.orekit.gnss.RinexObservationHeader
Get the antenna height.
getAntennaNumber() - Method in class org.orekit.gnss.RinexObservationHeader
Get the number of the antenna.
getAntennaPhaseCenter() - Method in class org.orekit.gnss.RinexObservationHeader
Get the antenna phasecenter.
getAntennaReferencePoint() - Method in class org.orekit.gnss.RinexObservationHeader
Get the position of antenna reference point for antenna on vehicle.
getAntennaType() - Method in class org.orekit.gnss.RinexObservationHeader
Get the type of the antenna.
getAntennaZeroDirection() - Method in class org.orekit.gnss.RinexObservationHeader
Get the zero direction of antenna.
getAODC() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
Getter for the Age Of Data Clock (AODC).
getAODE() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
Getter for the Age Of Data Ephemeris (AODE).
getAoR3Pow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get the value of a / R3 up to power maxAR3Pow.
getAoR3Pow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get the value of a / R3 up to power maxAR3Pow.
getAp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the Ap geomagnetic indices.
getAp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the Ap geomagnetic indices.
getAp(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Get the Ap geomagnetic indices.
getApAvg() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the arithmetic average of all eight Ap indices for the current entry.
getApplicableWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the applicable wavelength.
getAppliedVoltage() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the applied voltage.
getApproxPos() - Method in class org.orekit.gnss.RinexObservationHeader
Get the Approximate Marker Position.
getArbitraryEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Get an arbitrary date.
getArea() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
Get facet area.
getAreaDRG() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the effective area of the object exposed to atmospheric drag.
getAreaPC() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the actual area of the object.
getAreaSRP() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the effective area of the object exposed to solar radiation pressure.
getAstronomicalAmplitudesMap() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Get astronomical amplitudes map.
getAtmosphere() - Method in class org.orekit.forces.drag.DragForce
Get the atmospheric model.
getAtmosphere() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the atmospheric model.
getAtmosphericModel() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get name of atmospheric model.
getAtmosphericModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get name of atmospheric model.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FixedRate
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.InertialProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.InertialProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.SpinStabilized
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the attitude corresponding to an orbital state.
getAttitude(Frame, PVCoordinatesProvider) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm
Get the attitude.
getAttitude(Frame, PVCoordinatesProvider) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Get the attitude.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the attitude.
getAttitude() - Method in class org.orekit.propagation.SpacecraftState
Get the attitude.
getAttitudeActuatorType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the type of actuator for attitude control.
getAttitudeControlAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the accuracy of attitude control.
getAttitudeControlMode() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the attitude control mode.
getAttitudeFromFrame(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Compute the attitude for DIRECTION_IN_FRAME or DIRECTION_IN_LOF types.
getAttitudeKnowledgeAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the accuracy of attitude knowledge.
getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the Attitude Provider to use during maneuver.
getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the attitude override used for the maneuver.
getAttitudePointingAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the overall accuracy of spacecraft to maintain attitude.
getAttitudeProvider() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get the attitude provider for this attitude ephemeris segment.
getAttitudeProvider() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get the attitude provider for this attitude ephemeris segment.
getAttitudeProvider() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
Get the attitude provider corresponding to this ephemeris, combining data from all segments.
getAttitudeProvider() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get the attitude provider for this attitude ephemeris segment.
getAttitudeProvider() - Method in class org.orekit.propagation.AbstractPropagator
Get attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get attitude provider.
getAttitudeProvider() - Method in interface org.orekit.propagation.FieldPropagator
Get attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get the attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.integration.StateMapper
Get the attitude provider.
getAttitudeProvider() - Method in interface org.orekit.propagation.Propagator
Get attitude provider.
getAttitudeType() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the format of the data lines in the message.
getAugmentedInitialState(int) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Compute the additional state from the additionalEquations.
getAugmentedInitialState(SpacecraftState, AdditionalEquations) - Method in class org.orekit.utils.AbstractMultipleShooting
Deprecated.
getAugmentedInitialState(int) - Method in class org.orekit.utils.AbstractMultipleShooting
Compute the additional state from the additionalEquations.
getAugmentedInitialState(int) - Method in class org.orekit.utils.MultipleShooter
Compute the additional state from the additionalEquations.
getAuthentication(String) - Static method in enum org.orekit.gnss.metric.ntrip.Authentication
Get the authentication type corresponding to a keyword.
getAuthentication() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the authentication method.
getAuthentication() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Get the authentication method.
getAuxiliaryElements() - Method in class org.orekit.propagation.semianalytical.dsst.forces.ForceModelContext
Method to get the auxiliary elements related to the ForceModelContext.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get which derivatives of angular data are available in this attitude ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
Get which derivatives of position are available in this state.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
Get the derivatives available in the block.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get which derivatives of angular data are available in this attitude ephemeris segment.
getAvailableDerivatives() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get which derivatives of angular data are available in this attitude ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
 
getAverageFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the 81 day average of F10.7 solar flux centered on current day.
getAverageFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the 81 day average of F10.7 solar flux centered on current day.
getAverageFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Get the value of the 81 day average of F10.7 solar flux centered on current day.
getAx2oA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get ax2oA = 2 * a / A .
getAx2oA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get ax2oA = 2 * a / A .
getAzimuth() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the azimuth angle.
getAzimuth(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the azimuth of a point with regards to the topocentric frame center point.
getAzimuth(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the azimuth of a point with regards to the topocentric frame center point.
getAzimuthRate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the azimuth rate.
getB() - Method in class org.orekit.bodies.Ellipse
Get the semi minor axis.
getB() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the second semi-axis.
getb() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get b = 1 / (1 + sqrt(1 - e²)) = 1 / (1 + B).
getb() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get b = 1 / (1 + sqrt(1 - e²)) = 1 / (1 + B).
getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get B = sqrt(1 - e²).
getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get B = sqrt(1 - e²).
getB1() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Get the Jacobian matrix B1 (B1 = ∂εη/∂Y).
getB2(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Get the Jacobian matrix B2 (B2 = ∂Y/∂Y₀).
getB3(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Get the Jacobian matrix B3 (B3 = ∂Y/∂P).
getB4() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Get the Jacobian matrix B4 (B4 = ∂εη/∂c).
getBase() - Method in class org.orekit.utils.units.PowerTerm
Get the base term.
getBaseDate() - Method in class org.orekit.utils.DateDriver
Get the base (unshifted) date.
getBaseEquipment() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame
Get the quipment on which the frame is located.
getBaseFrame() - Method in class org.orekit.estimation.measurements.GroundStation
Get the base frame associated with the station.
getBaseName(T) - Method in class org.orekit.data.AbstractListCrawler
Get the base name of an input.
getBaseName(File) - Method in class org.orekit.data.FilesListCrawler
Get the base name of an input.
getBaseName(URL) - Method in class org.orekit.data.NetworkCrawler
Get the base name of an input.
getBaseProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get a time-independent provider containing base harmonics coefficients.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the base system state at given date, without compensation.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the base system state at given date, without compensation.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the base system state at given date, without compensation.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the base system state at given date, without compensation.
getBaseWeight() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the base weight associated with the measurement
getBaseWeight() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the base weight associated with the measurement
getBaseWeight() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the base weight associated with the measurement
getBasicDimension() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get state vector dimension without additional parameters.
getBasicDimension() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get state vector dimension without additional parameters.
getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get B².
getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get B * B.
getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get B².
getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get B * B.
getBBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get B³.
getBBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get B³.
getBDT() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getBDT() - Method in interface org.orekit.time.TimeScales
Get the BeiDou Navigation Satellite System time scale.
getBDT() - Static method in class org.orekit.time.TimeScalesFactory
Get the BeiDou Navigation Satellite System time scale.
getBeacon() - Method in class org.orekit.propagation.events.AngularSeparationDetector
Get the beacon at the center of the proximity zone.
getBeamDivergence() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the beam divergence.
getBefore() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the entry valid before transition.
getBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the entry valid before transition.
getBeginDate(Frequency) - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
Return the date of validity beginning of the detector.
getBeidouEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getBeidouEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for BeiDou weeks: 2006-01-01T00:00:00 UTC.
getBeidouNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Get the Beidou navigation message corresponding to the current RTCM data.
getBeidouNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Get the Beidou navigation message corresponding to the current RTCM data.
getBeidouNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation
Get all the Beidou navigation messages contained in the file.
getBeidouNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Get the Beidou navigation messages for the given satellite Id.
getBeidouToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Get the Beidou time of clock.
getBeta() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Returns the beta coefficients array.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get direction cosine β for central body.
getBGDE1E5a() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Getter for the E1/E5a broadcast group delay.
getBGDE5bE1() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Getter for the the Broadcast Group Delay E5b/E1.
getBitRate() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the bit rate.
getBN() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS Bn Word.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get B / A.
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get BoABpo = B / A(1 + B).
getBody(String) - Method in interface org.orekit.bodies.CelestialBodies
Get a celestial body.
getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Get a celestial body.
getBody(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Get a celestial body.
getBody() - Method in class org.orekit.files.ccsds.definitions.BodyFacade
Get the celestial body.
getBody() - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get third body.
getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing
Get the body frame.
getBodyFrame() - Method in interface org.orekit.bodies.BodyShape
Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.models.earth.Geoid
 
getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
Get a body oriented, body centered frame.
getBodyShape() - Method in class org.orekit.propagation.events.AltitudeDetector
Get the body shape.
getBodyShape() - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Get the body shape.
getBolDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the total ΔV capability at beginning of life.
getBStar() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the SGP/SGP4 drag-like coefficient.
getBStar() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the ballistic coefficient.
getBStar() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the ballistic coefficient.
getBuilder() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler
Get the measurements builder.
getBuilders() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Getter for the propagators.
getBusModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the bus model name.
getC() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the third semi-axis.
getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get C = 1 + p² + q².
getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get C = 1 + p² + q².
getC2n0(int) - Method in class org.orekit.models.earth.ReferenceEllipsoid
Get the fully normalized coefficient C2n,0 for the normal gravity potential.
getCacheSlotsNumber() - Static method in class org.orekit.utils.OrekitConfiguration
Get the number of slots to use in caches.
getCalendarWeek() - Method in class org.orekit.time.DateComponents
Get the calendar week number.
getCalls() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the number of calls to the differential equations computation method.
getCalls() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the number of calls to the differential equations computation method.
getCapitalizedAbbreviation() - Method in enum org.orekit.time.Month
Get the capitalized three letters abbreviation.
getCapitalizedName() - Method in enum org.orekit.time.Month
Get the capitalized full name.
getCarrierPhase(String) - Static method in enum org.orekit.gnss.metric.ntrip.CarrierPhase
Get the carrier phase corresponding to a code.
getCarrierPhase() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the carrier phase.
getCartesian() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary Cartesian part.
getCartesian() - Method in class org.orekit.frames.Transform
Get the underlying elementary Cartesian part.
getCartesianIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getCartesianIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getCasters() - Method in class org.orekit.gnss.metric.ntrip.SourceTable
Get the casters records.
getCatalogName() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the satellite catalog used for the object.
getCatalogName() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the specification of satellite catalog source.
getCcsdsEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getCCSDSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4):
getCcsdsEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).
getCDAreaOverMass() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the object’s Cd x A/m used to propagate the state vector and covariance to TCA.
getCdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the Unique identifier of Conjunction Data Message linked to this Orbit Data Message.
getCdrgdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [7,7] in covariance matrix (with index starting at 1).
getCdrgn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [7,3] in covariance matrix (with index starting at 1).
getCdrgndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [7,6] in covariance matrix (with index starting at 1).
getCdrgr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [7,1] in covariance matrix (with index starting at 1).
getCdrgrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [7,4] in covariance matrix (with index starting at 1).
getCdrgt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [7,2] in covariance matrix.
getCdrgtdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [7,5] in covariance matrix (with index starting at 1).
getCelestialBodies() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the instance of CelestialBodies that is called by the static methods in this class.
getCelestialBodies() - Method in class org.orekit.data.CompositeDataContext
 
getCelestialBodies() - Method in interface org.orekit.data.DataContext
Get a factory constructing CelestialBodys based on the auxiliary data in this context.
getCelestialBodies() - Method in class org.orekit.data.ExceptionalDataContext
 
getCelestialBodies() - Method in class org.orekit.data.LazyLoadedDataContext
 
getCelestialBody() - Method in enum org.orekit.files.ccsds.definitions.CenterName
Get the celestial body corresponding to the CCSDS constant.
getCelestialBody(CelestialBodies) - Method in enum org.orekit.files.ccsds.definitions.CenterName
Get the celestial body corresponding to the CCSDS constant.
getCelestialSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the source and version of celestial body (e.g.
getCenter() - Method in class org.orekit.bodies.Ellipse
Get the center of the 2D ellipse.
getCenter() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Get the body at origin of reference frame.
getCenter() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Get the origin of reference frame.
getCenter() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get the origin of reference frame.
getCenter() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get the direction of the FOV center, in spacecraft frame.
getCenter() - Method in class org.orekit.models.earth.tessellation.Tile
Get the center point.
getCenterMass() - Method in class org.orekit.gnss.RinexObservationHeader
Get the current center of mass of vehicle in body fixed coordinate system.
getCenterName() - Method in class org.orekit.files.ccsds.definitions.ModifiedFrame
Get the CCSDS center name.
getCenterOfCurvature(Vector2D) - Method in class org.orekit.bodies.Ellipse
Find the center of curvature (point on the evolute) at the nadir of a point.
getCenterOfMassOffset() - Method in class org.orekit.files.ilrs.CPFHeader
Get the approximate center of mass to reflector offset.
getCentralBody() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
Get the central body.
getCentralBodyRotation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get central body angular rotation rate.
getChi() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getChi() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getChi2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get Χ².
getChi2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get Χ².
getChildren() - Method in class org.orekit.frames.OrphanFrame
Get all children of the instance.
getCic() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the Cic parameter.
getCic() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the Cic parameter.
getCic() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination.
getCij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldFourierCjSjCoefficients
Get the coefficient Cij.
getCij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FourierCjSjCoefficients
Get the coefficient Cij.
getCircularEx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the circular eccentricity vector.
getCircularEx() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the circular eccentricity vector.
getCircularExDot() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the circular eccentricity vector derivative.
getCircularExDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the circular eccentricity vector derivative.
getCircularEy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the circular eccentricity vector.
getCircularEy() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the circular eccentricity vector.
getCircularEyDot() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the circular eccentricity vector derivative.
getCircularEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the circular eccentricity vector derivative.
getCIRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getCIRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the CIRF2000 reference frame.
getCIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the CIRF2000 reference frame.
getCis() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the Cis parameter.
getCis() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the Cis parameter.
getCis() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination.
getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the Cj coefficient.
getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the Cj coefficient.
getCk0() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Get the un-normalized zonal coefficients.
getCk0() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Get the un-normalized zonal coefficients.
getClassification() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the message classification.
getClassification() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the classification.
getClassification() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the classification.
getClassificationType() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the classification type.
getClkOffset() - Method in class org.orekit.gnss.RinexObservationHeader
Get the realtime-derived receiver clock offset.
getClockAcceleration() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
Getter for the clock acceleration.
getClockAccelerationSigma() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
Getter for the clock acceleration sigma.
getClockBias() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
Getter for the clock bias.
getClockBiasSigma() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
Getter for the clock bias sigma.
getClockConstraint() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock
Getter for the clock constraint.
getClockCorrection() - Method in class org.orekit.files.sp3.SP3.SP3Coordinate
Returns the clock correction value.
getClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data
Get the clock correction data.
getClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
Get the clock correction data.
getClockCount() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get clock count.
getClockData() - Method in class org.orekit.gnss.clock.RinexClock
Getter for an unmodifiable map of clock data.
getClockDataTypes() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the different clock data types.
getClockDriftDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station clock drift (which is related to measurement date).
getClockDriftDriver() - Method in class org.orekit.estimation.measurements.ObservableSatellite
Get the clock drift parameter driver.
getClockID() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock
Getter for the clock ID.
getClockOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station clock (which is related to measurement date).
getClockOffsetDriver() - Method in class org.orekit.estimation.measurements.ObservableSatellite
Get the clock offset parameter driver.
getClockRate() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get clock rate.
getClockRate() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
Getter for the clock rate.
getClockRateChange() - Method in class org.orekit.files.sp3.SP3.SP3Coordinate
Returns the clock rate.
getClockRateSigma() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
Getter for the clock rate sigma.
getCndotn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [6,3] in covariance matrix (with index starting at 1).
getCndotndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [6,6] in covariance matrix (with index starting at 1).
getCndotr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [6,1] in covariance matrix (with index starting at 1).
getCndotrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [6,4] in covariance matrix (with index starting at 1).
getCndott() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [6,2] in covariance matrix (with index starting at 1).
getCndottdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [6,5] in covariance matrix (with index starting at 1).
getCnm() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Get the cosine parameters of spherical harmonics expansion of degree N and order M.
getCnn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [3,3] in covariance matrix (with index starting at 1).
getCnr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [3,1] in covariance matrix (with index starting at 1).
getCnt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [3,2] in covariance matrix (with index starting at 1).
getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get co2AB = C / 2AB.
getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get Co2AB = C / 2AB.
getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get co2AB = C / 2AB.
getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get Co2AB = C / 2AB.
getCodeBias() - Method in class org.orekit.gnss.metric.messages.ssr.igm.CodeBias
Get the code bias associated to the signal ID.
getCodeBias(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
Get the code bias for a given signal ID.
getCodeBiases() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
Get the code biases for the current satellite.
getCoefficients() - Method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Get the load deformation coefficients for ocean tides.
getCoefficients(String) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Get the coefficients for a given site.
getCoefficients(FieldAbsoluteDate<T>, Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients
Computes the coefficients involved in the contributions.
getCoefficients(AbsoluteDate, Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients
Computes the coefficients involved in the contributions.
getCoefficients(FieldAbsoluteDate<T>, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms
Computes the coefficients involved in the contributions.
getCoefficients(AbsoluteDate, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
Computes the coefficients involved in the contributions.
getCoefficientsKeyPrefix() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients
Get the prefix for short period coefficients keys.
getCoefficientsKeyPrefix() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients
Get the prefix for short period coefficients keys.
getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms
Get the prefix for short period coefficients keys.
getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
Get the prefix for short period coefficients keys.
getCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the probability (between 0.0 and 1.0) that Object1 and Object2 will collide.
getCollisionProbaMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the method that was used to calculate the collision probability.
getCombinationType() - Method in class org.orekit.gnss.CombinedObservationData
Get the type of the combination of measurements used to build the instance.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCombination
Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.IonosphereFreeCombination
Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.NarrowLaneCombination
Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.WideLaneCombination
Get the combined frequency of two measurements.
getCombinedMHzFrequency() - Method in class org.orekit.gnss.CombinedObservationData
Get the value of the combined frequency in MHz.
getCombinedProvider(TransformProvider, TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils
Combine two transform providers.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Get the combined observed value of two measurements.
getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCombination
Get the combined observed value of two measurements.
getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.GRAPHICCombination
Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.IonosphereFreeCombination
Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.NarrowLaneCombination
Get the combined observed value of two measurements.
getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCombination
Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.WideLaneCombination
Get the combined observed value of two measurements.
getComment() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get comment for relative metadata.
getComments() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the comments.
getComments() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Get the comments.
getComments() - Method in class org.orekit.files.ccsds.ndm.Ndm
Get an unmodifiable view of the comments.
getComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer
Get the comments.
getComments() - Method in class org.orekit.files.ilrs.CPF
Get the comments contained in the file.
getComments() - Method in class org.orekit.files.ilrs.CRD
Get the comments contained in the file.
getComments() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the comments.
getComments() - Method in class org.orekit.gnss.navigation.RinexNavigation
Getter for the comments.
getCompleteName(T) - Method in class org.orekit.data.AbstractListCrawler
Get the complete name of a input.
getCompleteName(File) - Method in class org.orekit.data.FilesListCrawler
Get the complete name of a input.
getCompleteName(URL) - Method in class org.orekit.data.NetworkCrawler
Get the complete name of a input.
getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components.
getComponents(int) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a local time.
getComponents(int, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a local time.
getComponents(TimeZone) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a time zone.
getComponents(TimeZone, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a time zone.
getComponents(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components.
getComponents(int) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a local time.
getComponents(int, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a local time.
getComponents(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a time zone.
getComponents(TimeZone, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a time zone.
getCompressionEncryption() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the compression/encryption algorithm applied.
getConfidence() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get confidence metric.
getConfiguration(String, int) - Method in class org.orekit.frames.ITRFVersionLoader
 
getConfiguration(String, int) - Method in interface org.orekit.frames.ItrfVersionProvider
Get the ITRF version configuration defined by a given file at specified date.
getConfigurationRecords() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the system configuration records.
getConsiderN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get number of consider parameters.
getConsiderParameters() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get description of consider parameters.
getConstantNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the constant gravity field coefficients provider from the first supported file.
getConstantNormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get a constant gravity field normalized coefficients provider.
getConstantNormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get a constant gravity field normalized coefficients provider.
getConstantProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Deprecated.
as of 11.1, not used anymore
getConstantUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the constant gravity field coefficients provider from the first supported file.
getConstantUnnormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get a constant gravity field unnormalized coefficients provider.
getConstantUnnormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get a constant gravity field unnormalized coefficients provider.
getConstellation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the name of the constellation this space object belongs to.
getConstituents() - Method in class org.orekit.files.ccsds.ndm.Ndm
Get an unmodifiable view of the constituents.
getConstraintsMap() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the map of patch points components which are constrained.
getContentAsBoolean() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as a boolean.
getContentAsDouble() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as a double.
getContentAsEnum(Class<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as an enum.
getContentAsEnumList(Class<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as a list of enum.
getContentAsInt() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as an integer.
getContentAsNormalizedList() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as a list of free-text strings.
getContentAsNormalizedString() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry.
getContentAsUppercaseCharacter() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as an uppercase character.
getContentAsUppercaseList() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as a list of normalized and uppercased strings.
getContentAsUppercaseString() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as normalized and uppercased.
getContentAsVector() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the content of the entry as a vector.
getContext() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Get the current context.
getContext() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Get the current context.
getConventions() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Get the IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Get IERS conventions.
getConventions() - Method in class org.orekit.frames.EOPHistory
Get the IERS conventions to which these EOP apply.
getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester
Get the conversion Jacobian between state parameters and parameters used for derivatives.
getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.numerical.AbsoluteJacobiansMapper
Get the conversion Jacobian between state parameters and parameters used for derivatives.
getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get the conversion Jacobian between state parameters and parameters used for derivatives.
getConverter(ContextBinding) - Method in enum org.orekit.files.ccsds.definitions.TimeSystem
Get associated TimeConverter.
getConverter(ITRFVersion, ITRFVersion) - Static method in enum org.orekit.frames.ITRFVersion
Find a converter between specified ITRF frames.
getConverter(ITRFVersion, ITRFVersion, TimeScale) - Static method in enum org.orekit.frames.ITRFVersion
Find a converter between specified ITRF frames.
getCoordinates(SpacecraftState, int, int) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Get Cartesian coordinates as derivatives.
getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
Get an unmodifiable view of the data points.
getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
 
getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3
Returns the coordinate system of the entries in this orbit file.
getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the estimated measurement.
getCorrectedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the estimated measurement.
getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the estimated measurement.
getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the corrected spacecraft states.
getCorrectedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the corrected spacecraft states.
getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the corrected spacecraft states.
getCorrection() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.PhaseShiftCorrection
Get the Phase Shift Corrections.
getCorrection() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.ScaleFactorCorrection
Get the Scale Factor.
getCorrectionAberrationDiurnal() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the diurnal aberration correction.
getCorrectionAberrationYearly() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the yearly aberration correction.
getCorrectionAngle1() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the correctionAngle1.
getCorrectionAngle2() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the correctionAngle2.
getCorrectionDoppler() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the correctionDoppler.
getCorrectionMagnitude() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the magnitude correction.
getCorrectionRange(RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the raw correction for range in meters.
getCorrectionRcs() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the radar cross section correction.
getCorrectionReceive() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the correctionReceive.
getCorrectionsApplied() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the correctionApplied.
getCorrectionTransmit() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the correctionTransmit.
getCorrelationCoefficientsMatrix() - Method in class org.orekit.estimation.measurements.Position
Get the correlation coefficients matrix.
getCorrelationCoefficientsMatrix() - Method in class org.orekit.estimation.measurements.PV
Get the correlation coefficients matrix.
getCosparID() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get COSPAR ID.
getCount() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the evaluations counter.
getCountry() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the name of the country where the space object owner is based.
getCountry() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the country.
getCountry() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the country.
getCovariance() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
getCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Get the covariance matrix logical block.
getCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get the covariance matrix logical block.
getCovarianceBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Get covariance logical blocks.
getCovarianceMatrices() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
Get an unmodifiable view of Covariance Matrices.
getCovarianceMatrices() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get an unmodifiable view of Covariance Matrices.
getCovarianceMatrix() - Method in class org.orekit.estimation.measurements.Position
Get the covariance matrix.
getCovarianceMatrix() - Method in class org.orekit.estimation.measurements.PV
Get the covariance matrix.
getCovarianceMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Get the Position/Velocity covariance matrix.
getCovarianceMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the method name used to calculate covariance during OD.
getCovariances() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistory
Get the covariances.
getCovBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Get basis of this covariance time history data.
getCovBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Get identification number of the orbit determination or simulation upon which this covariance is based.
getCovConfidence() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Get the measure of confidence in covariance error matching reality.
getCovFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Get epoch of the covariance reference frame.
getCovID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Get covariance identification number.
getCovNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Get identification number of next covariance.
getCovOrdering() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Get covariance ordering.
getCovPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Get identification number of previous covariance.
getCovReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Get reference frame of the covariance.
getCovScaleMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Get the maximum scale factor to apply to achieve realism.
getCovScaleMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Get the minimum scale factor to apply to achieve realism.
getCovType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Get covariance element set type.
getCovUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Get covariance element set units.
getCr3bpSystem() - Method in class org.orekit.orbits.RichardsonExpansion
Get the considered CR3BP system.
getCRAreaOverMass() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the object’s Cr x A/m used to propagate the state vector and covariance to TCA.
getCrc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the Crc parameter.
getCrc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the Crc parameter.
getCrc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius.
getCrdotn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [4, 3] in covariance matrix (with index starting at 1) .
getCrdotr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [4,1] in covariance matrix (with index starting at 1).
getCrdotrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [4, 4] in covariance matrix (with index starting at 1).
getCrdott() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [4,2] in covariance matrix (with index starting at 1).
getCreationDate() - Method in class org.orekit.files.ccsds.section.Header
Get the file creation date and time in UTC.
getCreationDate() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the creation date.
getCreationDate() - Method in class org.orekit.gnss.navigation.RinexNavigation
Getter for the creation date.
getCreationDateString() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the creation date of the file as a string.
getCreationDateString() - Method in class org.orekit.gnss.navigation.RinexNavigation
Getter for the creation date of the file as a string.
getCreationTimeString() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the creation time of the file as a string.
getCreationTimeString() - Method in class org.orekit.gnss.navigation.RinexNavigation
Getter for the creation time of the file as a string.
getCreationTimeZoneString() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the creation time zone of the file as a string.
getCreationTimeZoneString() - Method in class org.orekit.gnss.navigation.RinexNavigation
Getter for the creation time zone of the file as a string.
getCrr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [1,1] in covariance matrix (with index starting at 1).
getCrs() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the Crs parameter.
getCrs() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the Crs parameter.
getCrs() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius.
getCrsIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header
Get the Global/Regional CRS Indicator.
getCrsIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header
Get the Global/Regional CRS Indicator.
getCsrpdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,7] in covariance matrix (with index starting at 1).
getCsrpn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,3] in covariance matrix (with index starting at 1).
getCsrpndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,6] in covariance matrix (with index starting at 1).
getCsrpr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,1] in covariance matrix (with index starting at 1).
getCsrprdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,4] in covariance matrix (with index starting at 1).
getCsrpsrp() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,8] in covariance matrix (with index starting at 1).
getCsrpt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,2] in covariance matrix (with index starting at 1).
getCsrptdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [8,5] in covariance matrix (with index starting at 1).
getCtdotn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [5,3] in covariance matrix (with index starting at 1).
getCtdotr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [5, 1] in covariance matrix (with index starting at 1).
getCtdotrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [5,4] in covariance matrix (with index starting at 1).
getCtdott() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [5,2] in covariance matrix (with index starting at 1).
getCtdottdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [5,5] in covariance matrix (with index starting at 1).
getCthrdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,7] in covariance matrix (with index starting at 1).
getCthrn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,3] in covariance matrix (with index starting at 1).
getCthrndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,6] in covariance matrix (with index starting at 1).
getCthrr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,1] in covariance matrix (with index starting at 1).
getCthrrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,4] in covariance matrix (with index starting at 1).
getCthrsrp() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,8] in covariance matrix (with index starting at 1).
getCthrt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,2] in covariance matrix (with index starting at 1).
getCthrtdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,5] in covariance matrix (with index starting at 1).
getCthrthr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [9,9] in covariance matrix (with index starting at 1).
getCtr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [2,1] in covariance matrix (with index starting at 1).
getCtr81Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the centered 81-day arithmetic average of F10.7 (adjusted).
getCtr81Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the centered 81-day arithmetic average of F10.7 (observed).
getCtt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the object [2,2] in covariance matrix (with index starting at 1).
getCuc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the Cuc parameter.
getCuc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the Cuc parameter.
getCuc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude.
getCurrent() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Get the current processing state.
getCurrent() - Method in class org.orekit.utils.units.Unit
Get the current exponent.
getCurrentDate() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the current date.
getCurrentDate() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the current date.
getCurrentDate() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the current date.
getCurrentDate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
Get the current date.
getCurrentDate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the current date.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the current measurement number.
getCurrentMeasurementNumber() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the current measurement number.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the current measurement number.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
Get the current measurement number.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the current measurement number.
getCurrentState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Get the state at previous grid point date.
getCurrentState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the state at current grid point date.
getCus() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the Cus parameter.
getCus() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the Cus parameter.
getCus() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude.
getCXO2N2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get (C * χ) / ( 2 * n² * a² ).
getCXO2N2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get (C * χ) / ( 2 * n² * a² ).
getCycleDuration() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the duration of the GNSS cycle in seconds.
getCycleDuration() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
Gets the duration of the GNSS cycle in seconds.
getCycleDuration() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the duration of the GNSS cycle in seconds.
getCycleSlipMap() - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
Get the cycle slip Map with contains the results.
getD() - Method in class org.orekit.data.DelaunayArguments
Get the mean elongation of the Moon from the Sun.
getD() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean elongation of the Moon from the Sun.
getDailyFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the daily F10.7 solar flux for previous day.
getDailyFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the daily F10.7 solar flux for previous day.
getDailyFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Get the value of the daily F10.7 solar flux for previous day.
getDarkCount() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the dark count.
getData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm
Get the file data.
getData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Get the data from the single segment.
getData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Get the file data.
getData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Get the file data.
getData() - Method in class org.orekit.files.ccsds.section.Segment
Get the segment data.
getData() - Method in class org.orekit.files.ilrs.CRD.Meteo
Get an unmodifiable view of the tabulated meteorological data.
getData() - Method in class org.orekit.gnss.metric.messages.rtcm.RtcmMessage
Get the data.
getData() - Method in class org.orekit.gnss.metric.messages.ssr.SsrMessage
Get the data.
getData() - Method in class org.orekit.utils.DoubleArrayDictionary
Get an unmodifiable view of the dictionary entries.
getData() - Method in class org.orekit.utils.FieldArrayDictionary
Get an unmodifiable view of the dictionary entries.
getData() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the data valid during this time span.
getDataBlocks() - Method in class org.orekit.files.ilrs.CRD
Get the data blocks contain in the file.
getDataContext() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Get the data context.
getDataContext() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
Get the data context.
getDataContext() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get the data context used for getting frames, time scales, and celestial bodies.
getDataContext() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Get the data context used for getting frames, time scales, and celestial bodies.
getDataFormat(String) - Static method in enum org.orekit.gnss.metric.ntrip.DataFormat
Get the message type corresponding to a keyword.
getDataObject1() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm
Get the file data.
getDataObject2() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm
Get the file data.
getDataProvidersManager() - Method in class org.orekit.data.AbstractSelfFeedingLoader
Get the data provider manager.
getDataProvidersManager() - Method in class org.orekit.data.LazyLoadedDataContext
Get the provider of auxiliary data for this data context.
getDataProvidersManager() - Method in class org.orekit.frames.LazyLoadedEop
Get the data providers manager for this instance.
getDataQuality() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the dataQuality.
getDataReleaseFlag() - Method in class org.orekit.files.ilrs.CRDHeader
Get the flag indicating the data release.
getDataSet() - Method in class org.orekit.estimation.measurements.filtering.SmoothedObservationDataSet
Get the original observation data set used to compute the smoothed observation data.
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Getter for the data set.
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader
Getter for the data set.
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader
Gets the data set.
getDataStreams() - Method in class org.orekit.gnss.metric.ntrip.SourceTable
Get the data streams records.
getDataType() - Method in class org.orekit.files.ilrs.CRDHeader
Get the data type.
getDataType() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
Getter for the clock data type.
getDataTypes() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get observation data types used.
getDataTypes() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the data types in the data section.
getDataUsed() - Method in class org.orekit.files.sp3.SP3
Returns the data used indicator from the SP3 file.
getDate() - Method in class org.orekit.attitudes.Attitude
Get the date of attitude parameters.
getDate() - Method in class org.orekit.attitudes.FieldAttitude
Get the date of attitude parameters.
getDate() - Method in class org.orekit.data.DelaunayArguments
Get the date.
getDate() - Method in class org.orekit.data.FieldDelaunayArguments
Get the date.
getDate() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the date.
getDate() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Covariance
Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Get the date.
getDate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the date.
getDate() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
Get the date.
getDate() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement
Get the date.
getDate() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the date.
getDate() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the date of the maneuver.
getDate() - Method in class org.orekit.frames.EOPEntry
Get the date.
getDate() - Method in class org.orekit.frames.FieldTransform
Get the date.
getDate() - Method in class org.orekit.frames.Transform
Get the date.
getDate() - Method in class org.orekit.gnss.CombinedObservationDataSet
Get the date.
getDate() - Method in class org.orekit.gnss.DOP
Gets the calculation date of the DOP.
getDate() - Method in class org.orekit.gnss.ObservationDataSet
Get the date.
getDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
 
getDate() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader.LineParameters
 
getDate() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
 
getDate() - Method in class org.orekit.orbits.FieldOrbit
Get the date of orbital parameters.
getDate() - Method in class org.orekit.orbits.Orbit
Get the date of orbital parameters.
getDate() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the reference date of the ephemeris.
getDate() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the ephemeris reference date.
getDate() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getDate() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getDate() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the TLE current date.
getDate() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the TLE current date.
getDate() - Method in class org.orekit.propagation.events.DateDetector
Get the current event date according to the propagator.
getDate() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the date.
getDate() - Method in class org.orekit.propagation.events.FieldDateDetector
Get the current event date according to the propagator.
getDate() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the date.
getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the date of the orbit.
getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the date of the orbit.
getDate() - Method in class org.orekit.propagation.SpacecraftState
Get the date.
getDate() - Method in class org.orekit.time.AbsoluteDate
Get the date.
getDate() - Method in class org.orekit.time.DateTimeComponents
Get the date component.
getDate() - Method in class org.orekit.time.FieldAbsoluteDate
Get the date.
getDate() - Method in interface org.orekit.time.FieldTimeStamped
Get the date.
getDate() - Method in class org.orekit.time.GLONASSDate
 
getDate() - Method in class org.orekit.time.GNSSDate
Get the date.
getDate() - Method in interface org.orekit.time.TimeStamped
Get the date.
getDate() - Method in class org.orekit.time.UTCTAIOffset
Get the date of the start of the leap.
getDate() - Method in class org.orekit.utils.DateDriver
Get the shifted date.
getDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the transition absolute date.
getDate() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the transition date.
getDate() - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedPVCoordinates
Get the date.
getDateAndTime() - Method in class org.orekit.files.ilrs.CRDHeader
Get the date and time as the string value.
getDates() - Method in class org.orekit.propagation.events.DateDetector
Get all event dates currently managed, in chronological order.
getDay() - Method in class org.orekit.time.DateComponents
Get the day.
getDayFraction() - Method in class org.orekit.files.sp3.SP3
Returns the day fraction for this SP3 file.
getDayNumber() - Method in class org.orekit.time.GLONASSDate
Get the number of the current day in a four year interval.
getDayOfWeek() - Method in class org.orekit.time.DateComponents
Get the day of week.
getDayOfYear() - Method in class org.orekit.time.DateComponents
Get the day number in year.
getDcBodyFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get spacecraft body frame in which ManeuverHistoryMetadata.getDcBodyTrigger() is specified.
getDcBodyTrigger() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get direction in body frame for triggering duty cycle.
getDcExecStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get the start time of initial duty cycle-based maneuver execution.
getDcExecStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get the end time of final duty cycle-based maneuver execution.
getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dCj / dh coefficient.
getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the dCj / dh coefficient.
getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dCj / dk coefficient.
getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the dCj / dk coefficient.
getDcMaxCycles() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get the maximum number of "ON" duty cycles.
getDcMinCycles() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get the minimum number of "ON" duty cycles.
getDcPhaseStartAngle() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get phase angle of pulse start.
getDcPhaseStopAngle() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get phase angle of pulse stop.
getDcRefDir() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get reference direction for triggering duty cycle.
getDcRefTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get duty cycle thrust reference time.
getDcTimePulseDuration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get duty cycle pulse "ON" duration.
getDcTimePulsePeriod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get duty cycle elapsed time between start of a pulse and start of next pulse.
getDcType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get type of duty cycle.
getDcWindowClose() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get the end time of duty cycle-based maneuver window.
getDcWindowOpen() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get the start time of duty cycle-based maneuver window.
getDdEps() - Method in class org.orekit.frames.EOPEntry
Get the correction for nutation in obliquity δΔε.
getDdim() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP distance between the two bodies.
getDDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean elongation of the Moon from the Sun time derivative.
getDDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean elongation of the Moon from the Sun time derivative.
getDdPsi() - Method in class org.orekit.frames.EOPEntry
Get the correction for nutation in longitude δΔΨ.
getDecimalYear(int, int, int) - Static method in class org.orekit.models.earth.GeoMagneticField
Utility function to get a decimal year for a given day.
getDeclination() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the declination of the magnetic field in radians.
getDecorrelatedReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the reference decorrelated ambiguities.
getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
Get the decreasing events time shift.
getDefault() - Static method in interface org.orekit.data.DataContext
Get the default data context that is used to implement the static factories (TimeScalesFactory, FramesFactory, etc) and loaders that feed themselves (e.g.
getDefaultInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Get the default interpolation degree.
getDefaultLaw(Frames) - Static method in interface org.orekit.propagation.Propagator
Get a default law using the given frames.
getDefaultMass() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Get the default mass.
getDefaultModel() - Static method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Returns the default model, loading delay values from the file "tropospheric-delay.txt" via the default data context.
getDefaultTimeSystem(TimeScales) - Method in enum org.orekit.gnss.SatelliteSystem
Get default time scale for satellite system.
getDefaultVersion() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Get the default format version.
getDefaultVersion() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Get the default format version.
getDefaultYawRate(int) - Static method in class org.orekit.gnss.attitude.GPSBlockIIA
Get the default yaw rate for a satellite.
getDelaunayMultipliers() - Method in class org.orekit.models.earth.displacement.Tide
Get the multipliers for Delaunay arguments (l, l', F, D, Ω).
getDeltaClockC0() - Method in class org.orekit.gnss.metric.messages.ssr.igm.ClockCorrection
Get the delta clock C0.
getDeltaClockC1() - Method in class org.orekit.gnss.metric.messages.ssr.igm.ClockCorrection
Get the delta clock C1.
getDeltaClockC2() - Method in class org.orekit.gnss.metric.messages.ssr.igm.ClockCorrection
Get the delta clock C2.
getDeltaI() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getDeltaI() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the correction to the mean value of inclination.
getDeltaMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get mass change.
getDeltaMass() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Get mass change during maneuver (value is < 0).
getDeltaOrbitAlongTrack() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection
Get the along-track orbit correction for broadcast ephemeris.
getDeltaOrbitCrossTrack() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection
Get the cross-track orbit correction for broadcast ephemeris.
getDeltaOrbitRadial() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection
Get the radial orbit correction for broadcast ephemeris.
getDeltaT() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getDeltaT() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the correction to the mean value of Draconian period.
getDeltaTDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getDeltaTDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the rate of change of Draconian period.
getDeltaTN() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the deltaTauN value.
getDeltaVSat() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the velocity increment in satellite frame.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the local density.
getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the local density with initial entries.
getDensity(int, T, T, T, T, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the local density.
getDensity(Vector3D, Vector3D) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the local density.
getDensity(Vector3D, FieldVector3D<T>) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the local density at some position.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the local density at some position.
getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the local density with initial entries.
getDensity(T, T, T, T, T, T, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the local density.
getDensity(int) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00.FieldOutput
Get one of the stored densities.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
 
getDeployDirSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get one σ angular off-nominal deployment vector direction.
getDeployDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get velocity increment of deployed "child" object.
getDeployDvCda() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.
getDeployDvRatio() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get ratio of child-to-host ΔV vectors.
getDeployDvSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get one σ percent error on deployment ΔV magnitude.
getDeployId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get identifier of resulting "child" object deployed from this host.
getDeployMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get decrement in host mass as a result of deployment.
getDepth() - Method in class org.orekit.frames.Frame
Get the depth of the frame.
getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction
Get Γ function derivative.
getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Get Γ function derivative.
getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear
Compute the value of the derivative dKj-n-1, s / de².
getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear
Compute the value of the Hansen coefficient dK₀n, s / dΧ.
getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
Get the dK₀-n-1,s / dΧ coefficient derivative.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Compute the value of the derivative dKj-n-1, s / de².
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the value of the Hansen coefficient dK₀n, s / dΧ.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Get the dK₀-n-1,s / dΧ coefficient derivative.
getDerivativesDrivers() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get all the drivers with set derivatives.
getDerivativesToEpoch(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttractionEpoch
Compute derivatives of the state w.r.t epoch.
getDesignator() - Method in class org.orekit.gnss.clock.RinexClock.Receiver
Getter for the designator.
getDestination() - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Get the destination ITRF.
getDestination() - Method in class org.orekit.frames.ITRFVersion.Converter
Get the destination ITRF.
getDetector() - Method in class org.orekit.propagation.events.AdapterDetector
Get the wrapped detector.
getDetector() - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
Get the wrapped raw detector.
getDetector() - Method in class org.orekit.propagation.events.EventShifter
Get the detector for the raw unshifted event.
getDetector() - Method in class org.orekit.propagation.events.EventSlopeFilter
Get the wrapped raw detector.
getDetector() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event
Get the detector.
getDetector() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
Get the detector.
getDetectorId() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the detector configuration ID.
getDetectorRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the detector configuration record.
getDetectors() - Method in class org.orekit.propagation.events.BooleanDetector
Get the list of original detectors.
getDetectorType() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the detector type.
getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dGjs / dα coefficient.
getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dα coefficient.
getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dGjs / dβ coefficient.
getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dβ coefficient.
getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dGjs / dh coefficient.
getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dh coefficient.
getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dGjs / dk coefficient.
getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dk coefficient.
getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dGmsj / dα coefficient.
getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dα coefficient.
getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dGmsj / dβ coefficient.
getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dβ coefficient.
getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dGmsj / dh coefficient.
getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dh coefficient.
getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dGmsj / dk coefficient.
getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dk coefficient.
getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dHjs / dα coefficient.
getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dα coefficient.
getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dHjs / dβ coefficient.
getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dβ coefficient.
getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dHjs / dh coefficient.
getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dh coefficient.
getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dHjs / dk coefficient.
getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dk coefficient.
getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dHmsj / dα coefficient.
getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dα coefficient.
getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dHmsj / dβ coefficient.
getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dβ coefficient.
getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dHmsj / dh coefficient.
getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dh coefficient.
getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dHmsj / dk coefficient.
getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dk coefficient.
getDiagReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get a reference to the diagonal matrix of the decomposition.
getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dIjs / dα coefficient.
getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dα coefficient.
getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dIjs / dβ coefficient.
getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dβ coefficient.
getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dIjs / dh coefficient.
getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dh coefficient.
getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dIjs / dk coefficient.
getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dk coefficient.
getDimension() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the dimension of the measurement.
getDimension() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the dimension of the measurement.
getDimension() - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
Get the dimension of the generated column.
getDimension() - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
Get the dimension of the generated derivative.
getDimension() - Method in class org.orekit.propagation.integration.AdditionalEquationsAdapter
Deprecated.
Get the dimension of the generated derivative.
getDimension() - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
Get the dimension of the generated derivative.
getDimension() - Method in class org.orekit.propagation.integration.FieldAdditionalEquationsAdapter
Deprecated.
Get the dimension of the generated derivative.
getDimension() - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Get the dimension of the generated derivative.
getDimension() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Get the dimension of the generated derivative.
getDimension() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Deprecated.
Get the dimension of the generated derivative.
getDimension() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Deprecated.
Get the dimension of the generated derivative.
getDirection() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the direction.
getDirection() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust direction in S/C frame.
getDirection(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the thrust direction in spacecraft frame.
getDirectionFlag() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the direction flag (0 = transmit & receive ; 1 = transmit ; 2 = receive).
getDiscontinuityCounter() - Method in class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias
Get the signal phase discontinuity counter.
getDisplacements() - Method in class org.orekit.estimation.measurements.GroundStation
Get the displacement models.
getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dJjs / dα coefficient.
getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dα coefficient.
getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dJjs / dβ coefficient.
getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dβ coefficient.
getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dJjs / dh coefficient.
getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dh coefficient.
getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dJjs / dk coefficient.
getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dk coefficient.
getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients
Get the value of dLns / dγ (γ).
getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Get the value of dLns / dγ (γ).
getDnl(double, double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Dnl(Χ).
getDnl(T, T, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Dnl(Χ).
getDockedWith() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the other space objects this object is docked to.
getDomes() - Method in class org.orekit.files.sinex.Station
Get the site DOMES number.
getDoodson() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the Doodson number for the wave.
getDoodsonMultipliers() - Method in class org.orekit.models.earth.displacement.Tide
Get the multipliers for Doodson arguments (τ, s, h, p, N', ps).
getDoodsonNumber() - Method in class org.orekit.models.earth.displacement.Tide
Get the Doodson number.
getDopplerCountBias() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Get the Doppler count bias.
getDopplerCountScale() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Get the Doppler count scale.
getDotOrbitDeltaAlongTrack() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection
Get the velocity of along-track orbit correction for broadcast ephemeris.
getDotOrbitDeltaCrossTrack() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection
Get the velocity of cross-track orbit correction for broadcast ephemeris.
getDotOrbitDeltaRadial() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection
Get the velocity of radial orbit correction for broadcast ephemeris.
getDrag() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get drag force.
getDragArea() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Get the drag area.
getDragCoeff() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Get the drag coefficient.
getDragCoefficient() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the nominal drag coefficient.
getDragConstantArea() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
getDragParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get the drivers for supported parameters.
getDragParametersDrivers() - Method in interface org.orekit.forces.drag.DragSensitive
Get the drivers for supported parameters.
getDragParametersDrivers() - Method in class org.orekit.forces.drag.IsotropicDrag
Get the drivers for supported parameters.
getDragSensitive(AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Get the DragSensitive model valid at a date.
getDragSensitiveSpan(AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Get the DragSensitive TimeSpanMap.Span containing a specified date.
getDragUncertainty() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the drag coefficient 1σ uncertainty.
getDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier
Get the drivers for this modifier.
getDrivers(double, Orbit, PositionAngle) - Method in enum org.orekit.orbits.OrbitType
Get parameters drivers initialized from a reference orbit.
getDrivers() - Method in class org.orekit.utils.ParameterDriversList
Get delegating drivers for all parameters.
getDryMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the mass without propellant.
getDSDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Compute density and its derivatives.
getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dSj / dh coefficient.
getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the dSj / dh coefficient.
getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dSj / dk coefficient.
getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the dSj / dk coefficient.
getDSTDTC() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader.LineParameters
Get the DSTDTC parameter.
getDSTDTC(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the temperature change computed from Dst index.
getDSTDTC(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the temperature change computed from Dst index.
getDuration() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Get duration (value is 0 for impulsive maneuver).
getDuration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get duration.
getDuration() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Get duration (value is 0 for impulsive maneuver).
getDuration() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the duration of the maneuver (s).
getDuration() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Get the duration of the maneuver (s).
getDurationDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Get the driver for duration.
getDurationDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Get the driver for duration.
getDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get velocity increment.
getDV() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Get velocity increment.
getDvDirSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get one σ angular off-nominal ΔV direction.
getDvMagSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get one σ percent error on ΔV magnitude.
getDx() - Method in class org.orekit.frames.EOPEntry
Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getDy() - Method in class org.orekit.frames.EOPEntry
Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getE() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the orbit eccentricity.
getE() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.Orbit
Get the eccentricity.
getE() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the eccentricity.
getE() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getE() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the Eccentricity.
getE() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Eccentricity.
getE() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the eccentricity.
getE() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the eccentricity.
getE() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the eccentricity.
getE() - Method in class org.orekit.propagation.SpacecraftState
Get the eccentricity.
getE2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get ecc².
getE2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get ecc².
getEarliest() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the earliest cached entry.
getEarliest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get the earliest entry in this cache.
getEarliest() - Method in interface org.orekit.utils.TimeStampedCache
Get the earliest entry in this cache.
getEarth() - Method in interface org.orekit.bodies.CelestialBodies
Get the Earth singleton body.
getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Earth singleton body.
getEarth() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getEarth() - Method in class org.orekit.forces.gravity.DeSitterRelativity
Get the Earth model used to compute De Sitter effect.
getEarthMoonBarycenter() - Method in interface org.orekit.bodies.CelestialBodies
Get the Earth-Moon barycenter singleton bodies pair.
getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Earth-Moon barycenter singleton bodies pair.
getEarthMoonBarycenter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getEarthMoonBarycenterSemiMajorAxis(AbsoluteDate, TimeScale) - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants
Get the Earth-Moon barycenter semi-major axis.
getEarthMoonCR3BP() - Static method in class org.orekit.bodies.CR3BPFactory
Get the Earth-Moon CR3BP singleton bodies pair.
getEarthOrientationAngleFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the raw Earth Orientation Angle.
getEarthOrientationAngleFunction(TimeScale, TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the raw Earth Orientation Angle.
getEarthTides() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get boolean that indicates if Earth and ocean tides are taken into account or not.
getEast() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.frames.TopocentricFrame
Get the east direction of topocentric frame, expressed in parent shape frame.
getEastOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station position along East axis.
getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the eccentricity.
getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the eccentricity.
getEccentricAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric anomaly.
getEccentricAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric anomaly.
getEccentricAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric anomaly derivative.
getEccentricAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric anomaly derivative.
getEccentricities() - Method in class org.orekit.files.sinex.Station
Get the last known station antenna eccentricities.
getEccentricities(AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Get the station antenna eccentricities for the given epoch.
getEccentricities(Frequency) - Method in class org.orekit.gnss.antenna.Antenna
Get the phase center eccentricities.
getEccentricities() - Method in class org.orekit.gnss.antenna.FrequencyPattern
Get the phase center eccentricities.
getEccentricities() - Method in class org.orekit.gnss.RinexObservationHeader
Get the eccentricities of antenna center.
getEccentricitiesTimeSpanMap() - Method in class org.orekit.files.sinex.Station
Get the TimeSpanMap of site antenna eccentricities.
getEccRefSystem() - Method in class org.orekit.files.sinex.Station
Get the reference system used to define the eccentricity vector (local or cartesian).
getEccRefSystem(String) - Static method in enum org.orekit.files.sinex.Station.ReferenceSystem
Get the eccentricity reference system corresponding to the given value.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Gets the Earth Centered Earth Fixed frame used to propagate GLONASS orbits.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Gets the Earth Centered Earth Fixed frame used to propagate GNSS orbits according to the Interface Control Document.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Gets the Earth Centered Earth Fixed frame used to propagate GNSS orbits.
getECI() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Gets the Earth Centered Inertial frame used to propagate the orbit.
getECI() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Gets the Earth Centered Inertial frame used to propagate the orbit.
getECI() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Gets the Earth Centered Inertial frame used to propagate the orbit.
getEclipseAngles(Vector3D, Vector3D) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Get the useful angles for eclipse computation.
getEclipseAngles(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Get the useful angles for eclipse computation.
getEcliptic(IERSConventions) - Method in class org.orekit.frames.AbstractFrames
 
getEcliptic(IERSConventions) - Method in interface org.orekit.frames.Frames
Get the ecliptic frame.
getEcliptic(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the ecliptic frame.
getEDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.Orbit
Get the eccentricity derivative.
getEffects() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the differential effects.
getElem(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Get the value of an element.
getElementNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the element number.
getElementNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the element number.
getElements() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
Get trajectory elements.
getElementSetNumber() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the element set number for this satellite.
getElevation() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the elevation angle.
getElevation(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the elevation of a point with regards to the local point.
getElevation(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the elevation of a point with regards to the local point.
getElevation(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Get the elevation value.
getElevation(double) - Method in class org.orekit.utils.ElevationMask
Get the interpolated elevation for a given azimuth according to the mask.
getElevationMask() - Method in class org.orekit.gnss.DOPComputer
Get the elevation mask.
getElevationMask() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured elevation mask.
getElevationMask() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured elevation mask.
getElevationRate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the elevation rate.
getEllipsoid() - Method in interface org.orekit.models.earth.EarthShape
Get the underlying ellipsoid model that defines latitude and longitude.
getEllipsoid() - Method in class org.orekit.models.earth.Geoid
 
getEllipsoid() - Method in class org.orekit.models.earth.ReferenceEllipsoid
 
getEME2000() - Method in class org.orekit.frames.AbstractFrames
 
getEME2000() - Method in interface org.orekit.frames.Frames
Get the unique EME2000 frame.
getEME2000() - Static method in class org.orekit.frames.FramesFactory
Get the unique EME2000 frame.
getEmitterStation() - Method in class org.orekit.estimation.measurements.BistaticRange
 
getEmitterStation() - Method in class org.orekit.estimation.measurements.BistaticRangeRate
Get the emitter ground station.
getEn() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS En Word.
getEnd() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the end of the measurements time span.
getEnd() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the end of this time span.
getEndDate(Frequency) - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
Return the end date at the given frequency.
getEndDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the end date.
getEndDate() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Get the end date.
getEndDate() - Method in class org.orekit.frames.EOPHistory
Get the date of the last available Earth Orientation Parameters.
getEndDate() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock
Getter for the validity period end date.
getEndEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the ending epoch (UTC).
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the endpoints (i.e.
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Get the endpoints (i.e.
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Get the endpoints (i.e.
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the endpoints (i.e.
getEndTransition() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the transition at end of this time span.
getEntries() - Method in class org.orekit.frames.EOPHistory
Get a non-modifiable view of the EOP entries.
getEntries() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the total number of entries cached.
getEntry(String) - Method in class org.orekit.utils.DoubleArrayDictionary
Get a complete entry.
getEntry(String) - Method in class org.orekit.utils.FieldArrayDictionary
Get a complete entry.
getEOPHistory() - Method in interface org.orekit.frames.EOPBasedTransformProvider
Get the EOP history.
getEOPHistory(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get Earth Orientation Parameters history.
getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get Earth Orientation Parameters history.
getEOPHistory() - Method in class org.orekit.frames.GTODProvider
Get the EOP history.
getEOPHistory(IERSConventions, boolean, TimeScales) - Method in class org.orekit.frames.LazyLoadedEop
Get Earth Orientation Parameters history.
getEOPHistory(IERSConventions, boolean) - Method in class org.orekit.frames.LazyLoadedFrames
Get Earth Orientation Parameters history.
getEopHistory(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
Get the EOP history for the given conventions.
getEopHistory(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
 
getEOPHistory() - Method in class org.orekit.time.UT1Scale
Get the EOP history.
getEopSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the source and version of Earth Orientation Parameters.
getEOPTidalCorrection() - Method in enum org.orekit.utils.IERSConventions
Get the function computing tidal corrections for Earth Orientation Parameters.
getEOPTidalCorrection(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing tidal corrections for Earth Orientation Parameters.
getEphemeridesDataLines() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
Get the list of Ephemerides data lines.
getEphemeridesDataLines() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the list of Ephemerides data lines.
getEphemerisData() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisMessage
Get the ephemeris data contain in the ephemeris message.
getEphemerisGenerator() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in interface org.orekit.propagation.FieldPropagator
Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in interface org.orekit.propagation.Propagator
Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisNames() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for external ephemeris names for participants.
getEphemerisType() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the ephemeris type.
getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the type of ephemeris.
getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the type of ephemeris.
getEphemName() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the unique name of the external ephemeris used for OD.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Get the epoch of the data.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Get matrix epoch.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get epoch of state vector, Keplerian elements and covariance matrix data.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get time tag for orbit determination solved-for state.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
Get epoch of state vector, Keplerian elements and covariance matrix data.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation
Getter for the epoch.
getEpoch() - Method in class org.orekit.files.sinex.Station
Get the coordinates reference epoch.
getEpoch() - Method in class org.orekit.files.sp3.SP3
Returns the start epoch of the orbit file.
getEpoch() - Method in class org.orekit.frames.HelmertTransformation
Get the reference epoch of the transform.
getEpoch() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
Get data line epoch.
getEpoch(TimeScale) - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
Get data line epoch.
getEpoch() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the epoch for this magnetic field model.
getEpochDelayCorrection() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Get the epoch delay correction.
getEpochEigenInt() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get positional error ellipsoid 1σ intermediate eigenvalue at the epoch of OD.
getEpochEigenMaj() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get positional error ellipsoid 1σ major eigenvalue at the epoch of OD.
getEpochEigenMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get positional error ellipsoid 1σ minor eigenvalue at the epoch of OD.
getEpochEvent() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement
Get the indicator for the time event reference.
getEpochIdentifier() - Method in class org.orekit.files.ilrs.CRDHeader
Get the epoch identifier.
getEpochIgnition() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Get epoch ignition.
getEpochInterval() - Method in class org.orekit.files.sp3.SP3
Returns the time interval between epochs (in seconds).
getEpochStart() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Get epoch start.
getEpochT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the epoch to which all relative times are referenced in data blocks.
getEpochToc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the time of clock epoch.
getEpochToc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the time of clock epoch.
getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the equatorial radius of the body.
getEquatorialRadius() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get oblate spheroid equatorial radius of central body.
getEquatorialRadius() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Getter for equatorial radius.
getEquatorialRadius() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the central body equatorial radius.
getEquinoctialEx() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.Orbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEx() - Method in class org.orekit.propagation.SpacecraftState
Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialExDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.Orbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.Orbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the second component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEy() - Method in class org.orekit.propagation.SpacecraftState
Get the second component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEyDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.Orbit
Get the second component of the equinoctial eccentricity vector.
getEquinoxNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for equinox-based paradigm.
getEquinoxNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for equinox-based paradigm.
getEstimate() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the current corrected estimate.
getEstimate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the current corrected estimate.
getEstimatedEarthFrame() - Method in class org.orekit.estimation.measurements.GroundStation
Get the estimated Earth frame, including the estimated linear models for pole and prime meridian.
getEstimatedMeasurement(int) - Method in interface org.orekit.estimation.measurements.EstimationsProvider
Get one estimated measurement.
getEstimatedMeasurements() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement
Get the underlying estimated measurements.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the list of estimated measurements parameters.
getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the list of estimated orbital parameters.
getEstimatedOrbitalParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the list of estimated orbital parameters.
getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the list of estimated orbital parameters.
getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the list of estimated propagation parameters.
getEstimatedPropagationParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the list of estimated propagation parameters.
getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the list of estimated propagation parameters.
getEstimatedPropagator() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the propagator estimated with the values set in the propagator builder.
getEstimatedPropagators() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the propagators estimated with the values set in the propagators builders.
getEstimatedUT1() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the estimated UT1 time scale.
getEstimatedUT1() - Method in class org.orekit.estimation.measurements.GroundStation
Get the estimated UT1 scale, including the estimated linear models for prime meridian.
getEstimatedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the estimated value.
getEulerBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the Euler angles logical block.
getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the rotation order of Euler angles.
getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Get the rotation order of Euler angles.
getEvaluations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the number of objective function evaluations.
getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Get the evaluations count.
getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the number of evaluations used for last estimation.
getEventDate() - Method in class org.orekit.propagation.events.EventState
Get the occurrence time of the event triggered in the current step.
getEventDate() - Method in class org.orekit.propagation.events.FieldEventState
Get the occurrence time of the event triggered in the current step.
getEventDetector() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.EventState
Get the underlying event detector.
getEventDetector() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.FieldEventState
Get the underlying event detector.
getEvents() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue
Get the events passed to this handler.
getEvents() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
Get the events passed to this handler.
getEventsDetectors() - Method in class org.orekit.forces.drag.DragForce
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.drag.TimeSpanDragForce
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.empirical.ParametricAcceleration
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.forces.ForceModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.DeSitterRelativity
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.LenseThirringRelativity
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.OceanTides
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.Relativity
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.SolidTides
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.inertia.InertialForces
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Get the event detectors associated with the triggers.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Get the event detectors associated with the triggers.
getEventsDetectors() - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Get the event detectors associated with the triggers.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Get the event detectors associated with the triggers.
getEventsDetectors() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.propagation.Propagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Get the discrete events related to the model.
getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
getException() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor
Retrieve exception caught during monitoring.
getExponent() - Method in class org.orekit.utils.units.PowerTerm
Get the fractional exponent.
getExternalClockReference() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the external clock reference.
getExternalFrame() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Get the external frame.
getExternalSignalProcessing() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the external signal processing.
getExtrapolationThreshold() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the maximum timespan outside of the stored ephemeris that is allowed for extrapolation.
getF() - Method in class org.orekit.data.DelaunayArguments
Get L - Ω where L is the mean longitude of the Moon.
getF() - Method in class org.orekit.data.FieldDelaunayArguments
Get L - Ω where L is the mean longitude of the Moon.
getF10(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the value of the instantaneous solar flux index (1e-22*Watt/(m²*Hertz)).
getF10() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the value of the instantaneous solar flux index (1e-22*Watt/(m²*Hertz)).
getF10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the value of the instantaneous solar flux index (1e-22*Watt/(m²*Hertz)).
getF107Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the 10.7-cm Solar Radio Flux (F10.7) Adjusted to 1 AU.
getF107Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the observed (unadjusted) value of F10.7.
getF10B(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the value of the mean solar flux.
getF10B() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the value of the mean solar flux.
getF10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the value of the mean solar flux.
getFactoryKey() - Method in class org.orekit.frames.FactoryManagedFrame
Get the key of the frame within the factory.
getFallbackHostOrIPAddress() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the fallback host or IP address.
getFallbackPort() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the fallback port number.
getFDot() - Method in class org.orekit.data.DelaunayArguments
Get L - Ω where L is the mean longitude of the Moon time derivative.
getFDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get L - Ω where L is the mean longitude of the Moon time derivative.
getField(int) - Method in class org.orekit.gnss.metric.ntrip.Record
Get one field from the parsed sourcetable.
getField(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the GeoMagneticField for the given model type and year.
getField(GeoMagneticFieldFactory.FieldModel, double) - Method in interface org.orekit.models.earth.GeoMagneticFields
Get the GeoMagneticField for the given model type and year.
getField(GeoMagneticFieldFactory.FieldModel, double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
 
getField() - Method in class org.orekit.propagation.FieldAbstractPropagator
Field getter.
getField() - Method in class org.orekit.time.FieldAbsoluteDate
Get the field.
getField() - Method in class org.orekit.utils.FieldArrayDictionary
Get the field to which elements belong.
getFieldAuxiliaryElements() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldForceModelContext
Method to get the auxiliary elementsrelated to the ForceModelContext.
getFieldDate() - Method in class org.orekit.frames.FieldTransform
Get the date.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.drag.DragForce
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.empirical.ParametricAcceleration
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.forces.ForceModel
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.DeSitterRelativity
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
 
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.LenseThirringRelativity
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.OceanTides
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.Relativity
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
 
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
 
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SolidTides
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.inertia.InertialForces
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.Maneuver
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Get the event detectors associated with the triggers.
getFieldEventsDetectors(Field<S>) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Get the event detectors associated with the triggers.
getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Get the event detectors associated with the triggers.
getFieldEventsDetectors(Field<S>) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Get the event detectors associated with the triggers.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
 
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Get the discrete events related to the model.
getFieldsNumber() - Method in class org.orekit.gnss.metric.ntrip.Record
Get the number of fields.
getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the magnetic field vector in nTesla.
getFiftiesEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getFiftiesEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
getFiftiesEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
getFileDate(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the date of the file from which data at the specified date comes from.
getFileFormat() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Get the file format.
getFileName() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the name of the file.
getFileType() - Method in class org.orekit.gnss.navigation.RinexNavigation
Get the file type.
getFilter(int) - Static method in enum org.orekit.utils.AngularDerivativesFilter
Get the filter corresponding to a maximum derivation order.
getFilter(int) - Static method in enum org.orekit.utils.CartesianDerivativesFilter
Get the filter corresponding to a maximum derivation order.
getFilteredDataMap() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother
Get the map of the filtered data.
getFilteredDataMap() - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother
Get the map of the filtered data.
getFiltersManager() - Method in class org.orekit.data.DataProvidersManager
Get the manager for filters.
getFiringIntervalDetector() - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Getter for the firing interval detector.
getFirings() - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Get the firings detected during last propagation.
getFirstFrequencyPhaseHistory() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter
Get the history of phase values of the first frequency.
getFirstKnownLeapSecond() - Method in class org.orekit.time.UTCScale
Get the date of the first known leap second.
getFirstSpan() - Method in class org.orekit.forces.drag.TimeSpanDragForce
Get the first time span of the drag sensitive time span map.
getFirstSpan() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Get the first time span of the acceleration model time span map.
getFirstSpan() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Get the first time span of the tropospheric model time span map.
getFirstSpan() - Method in class org.orekit.utils.TimeSpanMap
Get the first (earliest) span.
getFirstTransition() - Method in class org.orekit.utils.TimeSpanMap
Get the first (earliest) transition.
getFittedParameters() - Method in class org.orekit.utils.SecularAndHarmonic
Get a copy of the last fitted parameters.
getFixedF10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux Unit daily proxy F10.7.
getFixedF10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux Unit 81-day running center-average proxy F10.7.
getFixedGeomagneticAp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the planetary 3-hour-range geomagnetic index aₚ.
getFixedGeomagneticDst() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the planetary 1-hour-range geomagnetic index Dst.
getFixedGeomagneticKp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the planetary 3-hour-range geomagnetic index Kₚ.
getFixedM10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux daily proxy M10.7.
getFixedM10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy M10.7.
getFixedS10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux daily proxy S10.7.
getFixedS10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy S10.7.
getFixedStepHandler() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Get the underlying fixed step handler.
getFixedStepHandler() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Get the underlying fixed step handler.
getFixedTimeStep() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Get the fixed time step.
getFixedTimeStep() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Get the fixed time step.
getFixedY10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux daily proxy Y10.7.
getFixedY10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy Y10.7.
getFlattening() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the flattening of the body: f = (a-b)/a.
getFlowRate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the flow rate.
getFlowRate(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the flow rate (kg/s).
getFluxQualifier() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the Flux Qualifier.
getFocus1() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Get first focus in spacecraft frame.
getFocus2() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Get second focus in spacecraft frame.
getFootprint(Transform, OneAxisEllipsoid, double) - Method in interface org.orekit.geometry.fov.FieldOfView
Get the footprint of the Field Of View on ground.
getFootprint(Transform, OneAxisEllipsoid, double) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView
Get the footprint of the Field Of View on ground.
getFootprint(Transform, OneAxisEllipsoid, double) - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get the footprint of the Field Of View on ground.
getFormat() - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Get the generated file format.
getFormat() - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
Get the generated file format.
getFormat() - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Get the generated file format.
getFormat() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the file format.
getFormat() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the data format.
getFormatDetails() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the format details.
getFormatVersion() - Method in class org.orekit.files.ccsds.section.Header
Get the CCSDS NDM (ADM, ODM or TDM) format version.
getFormatVersion() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the format version.
getFormatVersion() - Method in class org.orekit.gnss.navigation.RinexNavigation
Getter for the format version.
getFormatVersionKey() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
Get the key for format version.
getFormatVersionKey() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Get the key for format version.
getFOV() - Method in class org.orekit.propagation.events.FieldOfViewDetector
Get the Field Of View.
getFOV() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Get the Field Of View.
getFOV() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Get the Field Of View.
getFrame() - Method in class org.orekit.bodies.Ellipse
Get the defining frame.
getFrame() - Method in class org.orekit.bodies.Ellipsoid
Get the ellipsoid central frame.
getFrame(IERSConventions, boolean, DataContext) - Method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
Get the frame corresponding to the CCSDS constant.
getFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).
getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Get the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).
getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get the reference frame for this ephemeris segment.
getFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
 
getFrame(Predefined) - Method in class org.orekit.frames.AbstractFrames
 
getFrame(Predefined) - Method in interface org.orekit.frames.Frames
Get one of the predefined frames.
getFrame(Predefined) - Static method in class org.orekit.frames.FramesFactory
Get one of the predefined frames.
getFrame() - Method in class org.orekit.frames.OrphanFrame
Get the associated frame.
getFrame() - Method in class org.orekit.gnss.clock.RinexClock
Get the reference frame for the station positions.
getFrame() - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
Get the frame of the central body.
getFrame() - Method in class org.orekit.orbits.FieldOrbit
Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.orbits.Orbit
Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.propagation.AbstractPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.Ephemeris
 
getFrame() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the frame of the initial state.
getFrame() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.events.FieldNodeDetector
Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Get the sensor reference frame.
getFrame() - Method in class org.orekit.propagation.events.NodeDetector
Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in interface org.orekit.propagation.FieldPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the defining frame.
getFrame() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
 
getFrame() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get the inertial frame.
getFrame() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
 
getFrame() - Method in class org.orekit.propagation.integration.StateMapper
Get the inertial frame.
getFrame() - Method in interface org.orekit.propagation.Propagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the definition frame of the orbit.
getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the definition frame of the orbit.
getFrame() - Method in class org.orekit.propagation.SpacecraftState
Get the defining frame.
getFrame() - Method in class org.orekit.utils.AbsolutePVCoordinates
Get the frame in which the coordinates are defined.
getFrame() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get the frame in which the coordinates are defined.
getFrameA() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Get frame A.
getFrameB() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Get frame B.
getFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Get epoch of reference frame, if not intrinsic to the definition of the reference frame.
getFrameName() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the frame name.
getFrames() - Method in class org.orekit.data.CompositeDataContext
 
getFrames() - Method in interface org.orekit.data.DataContext
Get a factory constructing Frames based on the auxiliary data in this context.
getFrames() - Method in class org.orekit.data.ExceptionalDataContext
 
getFrames() - Method in class org.orekit.data.LazyLoadedDataContext
 
getFrames() - Static method in class org.orekit.frames.FramesFactory
Get the instance of Frames that is called by the static methods in this class.
getFreeAmbiguityDrivers() - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Get the ambiguity parameters drivers that have not been fixed yet.
getFreeAmbiguityIndirection(int, List<ParameterDriver>) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Get ambiguity indirection array for ambiguity parameters drivers that have not been fixed yet.
getFreeEpochMap() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the flags representing the free epoch of patch points.
getFreePatchPointMap() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the flags representing the free components of patch points.
getFreeStateParameters() - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Get the number of free state parameters.
getFreqOffset() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the freqOffset.
getFrequencies() - Method in class org.orekit.gnss.antenna.Antenna
Get supported frequencies.
getFrequency(SatelliteSystem) - Method in enum org.orekit.gnss.ObservationType
Get the frequency for a specified satellite system.
getFrequencyChannel() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Get the frequency channel.
getFrequencyNumber() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Getter for the frequency number.
getFrequencySource() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Get the frequency source.
getFrom() - Method in class org.orekit.utils.units.UnitsConverter
Get the source unit.
getFrozenFrame(Frame, AbsoluteDate, String) - Method in class org.orekit.frames.Frame
Get a new version of the instance, frozen with respect to a reference frame.
getFT() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS FT Word.
getFunction() - Method in class org.orekit.propagation.events.FieldFunctionalDetector
Get the switching function.
getFunction() - Method in class org.orekit.propagation.events.FunctionalDetector
Get the switching function.
getFutureInfinity() - Method in class org.orekit.time.AbstractTimeScales
 
getFutureInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Dummy date at infinity in the future direction.
getFutureInfinity() - Method in interface org.orekit.time.TimeScales
Dummy date at infinity in the future direction.
getGalileoDataValidityStatus() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Get the Galileo data validity status.
getGalileoEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getGalileoEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
getGalileoEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.
getGalileoNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Get the Galileo navigation message corresponding to the current RTCM data.
getGalileoNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Get the Galileo navigation message corresponding to the current RTCM data.
getGalileoNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation
Get all the Galileo navigation messages contained in the file.
getGalileoNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Get the Galileo navigation messages for the given satellite Id.
getGalileoToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Get the Galileo time of clock.
getGamma(LagrangianPoints) - Method in class org.orekit.bodies.CR3BPSystem
Get the position of the Lagrangian point in the CR3BP Rotating frame.
getGamma() - Method in class org.orekit.data.DelaunayArguments
Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.data.FieldDelaunayArguments
Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get direction cosine γ for central body.
getGammaDot() - Method in class org.orekit.data.DelaunayArguments
Get the tide parameter γ = GMST + π time derivative.
getGammaDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the tide parameter γ = GMST + π time derivative.
getGammaN() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Get the relative deviation of predicted satellite carrier frequency from nominal value.
getGammaN() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the relative deviation of predicted satellite carrier frequency from nominal value.
getGASTFunction(TimeScale, EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich apparent sidereal time, in radians.
getGASTFunction(TimeScale, EOPHistory, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich apparent sidereal time, in radians.
getGCRF() - Method in class org.orekit.frames.AbstractFrames
 
getGCRF() - Method in interface org.orekit.frames.Frames
Get the unique GCRF frame.
getGCRF() - Static method in class org.orekit.frames.FramesFactory
Get the unique GCRF frame.
getGdop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get generalize Dilution Of Precision.
getGdop() - Method in class org.orekit.gnss.DOP
Gets the geometric dilution of precision.
getGeneralEclipseAngles(Vector3D, Vector3D, double, Vector3D, double) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Get the useful angles for eclipse computation.
getGeneralEclipseAngles(FieldVector3D<T>, FieldVector3D<T>, T, FieldVector3D<T>, T) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Get the useful angles for eclipse computation.
getGeneralEclipseRatio(Vector3D, Vector3D, double, Vector3D, double) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get eclipse ratio between to bodies seen from a specific object.
getGeneralEclipseRatio(FieldVector3D<T>, FieldVector3D<T>, T, FieldVector3D<T>, T) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get eclipse ratio between to bodies seen from a specific object.
getGenerateCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of calls to the generate method.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.EphemerisGenerator
Get the ephemeris generated during the propagation.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.FieldEphemerisGenerator
Get the ephemeris generated during the propagation.
getGenerator() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the hardware or software generator.
getGenerator() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the generator.
getGeoMagneticFields() - Method in class org.orekit.data.CompositeDataContext
 
getGeoMagneticFields() - Method in interface org.orekit.data.DataContext
Get a factory constructing GeoMagneticFields based on the auxiliary data in this context.
getGeoMagneticFields() - Method in class org.orekit.data.ExceptionalDataContext
 
getGeoMagneticFields() - Method in class org.orekit.data.LazyLoadedDataContext
 
getGeoMagneticFields() - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the instance of GeoMagneticFields that is called by methods in this class.
getGeometryFreeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Geometry-Free combination of measurements.
getGetNeighborsCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of calls to the GenericTimeStampedCache.getNeighbors(AbsoluteDate) method.
getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the Gjs coefficient.
getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Gjs coefficient.
getGlo2UTC() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Get the correction from GLONASS to UTC.
getGLONASS() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getGLONASS() - Method in interface org.orekit.time.TimeScales
Get the GLObal NAvigation Satellite System time scale.
getGLONASS() - Static method in class org.orekit.time.TimeScalesFactory
Get the GLObal NAvigation Satellite System time scale.
getGlonassEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getGlonassEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for GLONASS four-year interval number: 1996-01-01T00:00:00 GLONASS time.
getGlonassNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the Glonass navigation message corresponding to the current RTCM data.
getGlonassNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the Glonass navigation message corresponding to the current RTCM data.
getGlonassNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation
Get all the Glonass navigation messages contained in the file.
getGlonassNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Get the Glonass navigation messages for the given satellite Id.
getGLONASSOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Gets the underlying GLONASS orbital elements.
getGLONASSOrbitalElements() - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
Gets the underlying GLONASS orbital elements.
getGloOffset() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Get the correction of time relative to GLONASS system time.
getGM() - Method in interface org.orekit.bodies.CelestialBody
Get the attraction coefficient of the body.
getGm() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get gravitational coefficient of attracting body.
getGM() - Method in class org.orekit.models.earth.ReferenceEllipsoid
Gets the gravitational parameter that is part of the definition of the reference ellipsoid.
getGM() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttractionContext
Get standard gravitational parameter μ for the body in m³/s².
getGM() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTNewtonianAttractionContext
Get standard gravitational parameter μ for the body in m³/s².
getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the Gmsj coefficient.
getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the Gmsj coefficient.
getGMST(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
 
getGMST() - Method in class org.orekit.time.GLONASSDate
Get the Greenwich Mean Sidereal Time.
getGMST(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
 
getGMST(IERSConventions, boolean) - Method in interface org.orekit.time.TimeScales
Get the Greenwich Mean Sidereal Time scale.
getGMST(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory
Get the Greenwich Mean Sidereal Time scale.
getGMSTFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time, in radians.
getGMSTFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time, in radians.
getGMSTRateFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time rate, in radians per second.
getGMSTRateFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time rate, in radians per second.
getGnssIod() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
Get the GNSS IOD.
getGnssIod() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
Get the GNSS IOD.
getGnssNb() - Method in class org.orekit.gnss.DOP
Gets the number of GNSS satellites taken into account for DOP computation.
getGPS() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getGPS() - Method in interface org.orekit.time.TimeScales
Get the Global Positioning System scale.
getGPS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Global Positioning System scale.
getGPS2Glo() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Get the correction to GPS time relative GLONASS.
getGpsCodeOnL2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Get the GPS code on L2.
getGpsEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getGPSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
getGpsEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
getGpsFitInterval() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Get the GPS fit interval.
getGpsL2PDataFlag() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Get the GPS L2 P-Code data flag.
getGpsNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Get the GPS navigation message corresponding to the current RTCM data.
getGpsNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Get the GPS navigation message corresponding to the current RTCM data.
getGPSNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation
Get all the GPS navigation messages contained in the file.
getGPSNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Get the GPS navigation messages for the given satellite Id.
getGpsToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Get the GPS time of clock.
getGpsWeek() - Method in class org.orekit.files.sp3.SP3
Returns the GPS week as contained in the SP3 file.
getGradientConverter() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Get the gradient converter related to the analytical orbit propagator.
getGradientDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D<Gradient>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Compute density and its derivatives.
getGRAPHICCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the GRAPHIC combination of measurements.
getGravitationalAssist() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get the origin of gravitational assist.
getGravityDegree() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get degree of the gravity model.
getGravityDegree() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get degree of the gravity model.
getGravityFields() - Method in class org.orekit.data.CompositeDataContext
 
getGravityFields() - Method in interface org.orekit.data.DataContext
Get a factory constructing gravity fields based on the auxiliary data in this context.
getGravityFields() - Method in class org.orekit.data.ExceptionalDataContext
 
getGravityFields() - Method in class org.orekit.data.LazyLoadedDataContext
 
getGravityFields() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the instance of GravityFields that is called by the static methods of this class.
getGravityModel() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get gravity model name.
getGravityModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get gravity model name.
getGravityOrder() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get order of the gravity model.
getGravityOrder() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get order of the gravity model.
getGridPoints() - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the number of interpolation grid points.
getGridPoints() - Method in class org.orekit.frames.ShiftingTransformProvider
Get the number of interpolation grid points.
getGridPoints(T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldFixedNumberInterpolationGrid
Get grid points that are within the current step.
getGridPoints(T, T) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.FieldInterpolationGrid
Get grid points that are within the current step.
getGridPoints(T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldMaxGapInterpolationGrid
Get grid points that are within the current step.
getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid
Get grid points that are within the current step.
getGridPoints(double, double) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.InterpolationGrid
Get grid points that are within the current step.
getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid
Get grid points that are within the current step.
getGrs80(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the GRS80 ellipsoid, attached to the given body frame.
getGST() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getGST() - Method in interface org.orekit.time.TimeScales
Get the Galileo System Time scale.
getGST() - Static method in class org.orekit.time.TimeScalesFactory
Get the Galileo System Time scale.
getGTOD(boolean) - Method in class org.orekit.frames.AbstractFrames
 
getGTOD(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getGTOD(boolean) - Method in interface org.orekit.frames.Frames
Get the GTOD reference frame.
getGTOD(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the GTOD reference frame.
getGTOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the GTOD reference frame.
getGTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the GTOD reference frame.
getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the y component of eccentricity vector.
getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the y component of eccentricity vector.
getHalfAperture() - Method in class org.orekit.geometry.fov.CircularFieldOfView
get the FOV half aperture angle.
getHalfApertureAlongX() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
get the FOV half aperture angle for spreading along Xell (i.e.
getHalfApertureAlongY() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
get the FOV half aperture angle for spreading along Yell (i.e.
getHaloOrbitalPeriod(double) - Method in class org.orekit.orbits.RichardsonExpansion
Return the orbital period of the Halo Orbit.
getHandler() - Method in class org.orekit.propagation.events.AbstractDetector
Get the handler.
getHandler() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get the handler.
getHandlers() - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Retrieve managed handlers list.
getHandlers() - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Get an unmodifiable view of all handlers.
getHandlers() - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Get an unmodifiable view of all handlers.
getHarmonicAmplitude() - Method in class org.orekit.utils.SecularAndHarmonic
Get an upper bound of the fitted harmonic amplitude.
getHarvester() - Method in class org.orekit.propagation.AbstractPropagator
Get the harvester.
getHasCreatableBody() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Get boolean testing whether the body corresponding to the centerName attribute can be created through the CelestialBodies.
getHdop() - Method in class org.orekit.gnss.DOP
Gets the horizontal dilution of precision.
getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
Get the header.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Get file header to fill.
getHeader() - Method in class org.orekit.files.ilrs.CPF
Get the CPF file header.
getHeader() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the header of the current data block.
getHeader() - Method in class org.orekit.gnss.CombinedObservationDataSet
Get the Rinex header associated with this data set.
getHeader() - Method in class org.orekit.gnss.metric.messages.ssr.SsrMessage
Get the header.
getHeader() - Method in class org.orekit.gnss.ObservationDataSet
Get the Rinex header associated with this data set.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the health status.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
Gets the Health status.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Get the Health status.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Gets the Health status.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
Gets the Health status.
getHealthE1() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Gets the E1-B/C signal health status.
getHealthE5a() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Gets the E5a signal health status.
getHealthE5b() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Gets the E5b signal health status.
getHeightIonosphericLayer() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Get the height of the ionospheric layer.
getHighRateClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data
Get the high rate clock correction to be added to the polynomial clock correction.
getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the Hjs coefficient.
getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Hjs coefficient.
getHK() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get h * k.
getHK() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get h * k.
getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the Hmsj coefficient.
getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the Hmsj coefficient.
getHorizontalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the horizontal intensity of the magnetic field (= norm of the vector in the plane spanned by the x/y components of the field vector).
getHost() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Get the caster host.
getHostOrIPAddress() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the host or IP address.
getHour() - Method in class org.orekit.time.TimeComponents
Get the hour number.
getHumidity() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
Get the relative humidity at the surface.
getHumiSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the humidity sensor manufacturer.
getHumiSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the humidity sensor model.
getHumiSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the humidity sensor serial number.
getHx() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.Orbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the first component of the inclination vector (as per equinoctial parameters).
getHx() - Method in class org.orekit.propagation.SpacecraftState
Get the first component of the inclination vector (as per equinoctial parameters).
getHxDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.Orbit
Get the first component of the inclination vector derivative.
getHXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get hXXX = h * Χ³.
getHXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get hXXX = h * Χ³.
getHy() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.Orbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the second component of the inclination vector (as per equinoctial parameters).
getHy() - Method in class org.orekit.propagation.SpacecraftState
Get the second component of the inclination vector (as per equinoctial parameters).
getHyDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.Orbit
Get the second component of the inclination vector derivative.
getI() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the orbit inclination.
getI() - Method in class org.orekit.orbits.CartesianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.CircularOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.KeplerianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.Orbit
Get the inclination.
getI() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the inclination.
getI() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the inclination.
getI() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the inclination.
getI() - Method in class org.orekit.propagation.SpacecraftState
Get the inclination.
getI0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the inclination angle at reference time.
getI0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Inclination Angle at Reference Time.
getI11() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Get the moment of Inertia about the 1-axis (N.m²).
getI12() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Get the moment of Inertia about the 1 and 2 axes (N.m²).
getI13() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Get the moment of Inertia about the 1 and 3 axes (N.m²).
getI22() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Get the moment of Inertia about the 2-axis (N.m²).
getI23() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Get the moment of Inertia about the 2 and 3 axes (N.m²).
getI33() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Get the moment of Inertia about the 3-axis (N.m²).
getICRF() - Method in class org.orekit.frames.AbstractFrames
 
getICRF() - Method in interface org.orekit.frames.Frames
Get the unique ICRF frame.
getICRF() - Static method in class org.orekit.frames.FramesFactory
Get the unique ICRF frame.
getId() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get identification number.
getId() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
Get the satellite ID.
getId() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
Get the satellite ID.
getId() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
 
getId() - Method in class org.orekit.gnss.metric.ntrip.StreamedMessage
Get message id.
getIdentifier() - Method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter
Get the regular expression for identifying line.
getIdentity(Field<T>) - Static method in class org.orekit.frames.FieldTransform
Get the identity transform.
getIdentity() - Static method in interface org.orekit.frames.StaticTransform
Get the identity static transform.
getIdentity(Field<T>) - Static method in class org.orekit.utils.FieldAngularCoordinates
Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).
getIDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.CircularOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.Orbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the rate of inclination angle.
getIDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the rate of inclination angle.
getIDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Rate of Inclination Angle.
getIers2003(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the IERS2003 ellipsoid, attached to the given body frame.
getIers2010(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the IERS2010 ellipsoid, attached to the given body frame.
getIers96(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the IERS96 ellipsoid, attached to the given body frame.
getIGRF(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the IGRF model for the given year.
getIGRF(double) - Method in interface org.orekit.models.earth.GeoMagneticFields
Get the IGRF model for the given year.
getIGRF(double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
 
getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the Ijs coefficient.
getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Ijs coefficient.
getIlrsSatelliteId() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the IRLS satellite ID (based on COSPAR ID).
getImaginary(int, int) - Method in class org.orekit.utils.LoveNumbers
Get the imaginary part of a nominal Love numbers.
getInclination() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the inclination of the magnetic field in radians.
getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
Get the increasing events time shift.
getIndicator() - Method in enum org.orekit.files.ilrs.CRDHeader.RangeType
Get the range type indicator.
getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the inertial velocity increment of the maneuver.
getInertialFrame() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get the inertial reference frame for this ephemeris segment.
getInertialFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the inertial reference frame for this ephemeris segment.
getInertialFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get the inertial reference frame for this ephemeris segment.
getInertialFrame() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the inertial frame in which the velocity increment is defined.
getInertiallyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
Get an inertially oriented, body centered frame.
getInertiaMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the inertia matrix.
getInertiaReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Get the coordinate system for the inertia tensor.
getInitialCovarianceMatrix(SpacecraftState) - Method in class org.orekit.estimation.sequential.AbstractCovarianceMatrixProvider
Get the initial covariance matrix.
getInitialCovarianceMatrix(SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider
Get the initial covariance matrix.
getInitialFlowrate() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
 
getInitialIntegrationState() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get the initial state for integration.
getInitialJacobianColumn(String) - Method in class org.orekit.propagation.AbstractMatricesHarvester
Get the initial column of Jacobian matrix with respect to named parameter.
getInitialOrbitDate() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the date of the initial orbit.
getInitialOrbitDate() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the date of the initial orbit.
getInitialPV() - Method in class org.orekit.orbits.LibrationOrbit
Return the initialPV on the libration orbit.
getInitialState() - Method in class org.orekit.propagation.AbstractPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getInitialState() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.FieldPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.Propagator
Get the propagator initial state.
getInitialStateTransitionMatrix() - Method in class org.orekit.propagation.AbstractMatricesHarvester
Get the initial State Transition Matrix.
getInitialThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
 
getInitialWetMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the total mass at beginning of life.
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
getInputs() - Method in class org.orekit.data.AbstractListCrawler
Get the list of inputs supported by the instance.
getInstantFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the instantaneous solar flux.
getInstantFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the instantaneous solar flux.
getInstantFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Get the value of the instantaneous solar flux.
getIntegrationInterval() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the integrationInterval.
getIntegrationRef() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the integrationRef.
getIntegrator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the integrator used by the propagator.
getIntegrator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the integrator used by the propagator.
getIntegratorBuilder() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Get the integrator builder.
getIntegratorBuilder() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Get the integrator builder.
getInternationalDes() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the international designator for the object.
getInternationalDesignator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the international designator for the object.
getInterpMethodEOP() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the interpolation method for Earth Orientation Parameters.
getInterpMethodSW() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get the interpolation method for Space Weather data.
getInterpolatedPoint(double, double) - Method in class org.orekit.models.earth.tessellation.Tile
Get an interpolated point inside the tile.
getInterpolatedState(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Get the state at interpolated date.
getInterpolatedState(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the state at interpolated date.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the interpolation degree.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get the interpolation degree.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Get the interpolation degree.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Get the interpolation degree.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Get the interpolation method to be used.
getInterpolationMethod() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get the interpolation method to be used.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
 
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid
Get the intersection point of a line with the surface of the body.
getInterval() - Method in class org.orekit.gnss.RinexObservationHeader
Get the observation interval in seconds.
getIntervalNumber() - Method in class org.orekit.time.GLONASSDate
Get the number of the current four year interval.
getIntrackThrust() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get boolean that indicates if intrack thrust modeling was into account or not.
getInverse() - Method in class org.orekit.frames.FieldTransform
Get the inverse transform of the instance.
getInverse() - Method in interface org.orekit.frames.StaticTransform
Get the inverse transform of the instance.
getInverse() - Method in class org.orekit.frames.Transform
Get the inverse transform of the instance.
getIOD() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Gets the Issue of Data (IOD).
getIOD() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Gets the GLONASS Issue Of Data (IOD).
getIODC() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
Getter for the Issue Of Data Clock (IODC).
getIODC() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
Getter for the Issue Of Data Clock (IODC).
getIODE() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
Getter for the Issue Of Data Ephemeris (IODE).
getIODE() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
Getter for the Issue Of Data Ephemeris (IODE).
getIODEC() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Getter for the Issue Of Data Ephemeris and Clock (IODEC).
getIODN() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Gets the Issue Of Data Navigation (IODN).
getIODN() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Gets the Issue Of Data Navigation (IODN).
getIODNav() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Getter for the the Issue Of Data (IOD).
getIodSsr() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Get the IOD SSR.
getIonoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier
Get the ionospheric delay model.
getIonoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier
Get the ionospheric delay model.
getIonosphereFreeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Ionosphere-Free combination of measurements.
getIonosphericCorrectionType() - Method in class org.orekit.gnss.navigation.RinexNavigation
Getter for the ionospheric correction type.
getIonosphericModel() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201
Get the ionospheric model adapted to the current IM201 message.
getIRNSS() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getIRNSS() - Method in interface org.orekit.time.TimeScales
Get the Indian Regional Navigation Satellite System time scale.
getIRNSS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Indian Regional Navigation Satellite System time scale.
getIrnssEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getIrnssEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for IRNSS weeks: 1999-08-22T00:00:00 IRNSS time.
getIRNSSNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation
Get all the IRNSS navigation messages contained in the file.
getIRNSSNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Get the IRNSS navigation messages for the given satellite Id.
getISP() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Get the specific impulse.
getISP() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the specific impulse.
getIsp() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the specific impulse.
getIsp() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the specific impulse.
getIsp(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the specific impulse (s).
getIteration() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the iteration number.
getIterationsCount() - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Get the iterations count.
getIterationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the number of iterations used for last estimation.
getITRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getITRF(ITRFVersion, IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getITRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get an unspecified International Terrestrial Reference Frame.
getITRF(ITRFVersion, IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get an specific International Terrestrial Reference Frame.
getITRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get an unspecified International Terrestrial Reference Frame.
getITRF(ITRFVersion, IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get an specific International Terrestrial Reference Frame.
getITRFEquinox(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getITRFEquinox(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the equinox-based ITRF reference frame.
getITRFEquinox(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the equinox-based ITRF reference frame.
getITRFType() - Method in class org.orekit.frames.EOPEntry
Get the ITRF version this entry defines.
getITRFVersion() - Method in class org.orekit.files.sinex.SinexLoader
Get the ITRF version used for the EOP entries processing.
getITRFVersion(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the ITRF version.
getITRFVersion(int) - Static method in enum org.orekit.frames.ITRFVersion
Find an ITRF version from its reference year.
getITRFVersion(String) - Static method in enum org.orekit.frames.ITRFVersion
Find an ITRF version from its name.
getITRFVersion() - Method in class org.orekit.frames.VersionedITRF
Get the ITRF version.
getJ2000Day() - Method in class org.orekit.time.DateComponents
Get the day number with respect to J2000 epoch.
getJ2000Epoch() - Method in class org.orekit.time.AbstractTimeScales
 
getJ2000Epoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
getJ2000Epoch() - Method in interface org.orekit.time.TimeScales
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
getJacobian(Orbit, PositionAngle, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the Jacobian of the orbit with respect to maneuver parameters.
getJacobian(CartesianDerivativesFilter, T[][]) - Method in class org.orekit.frames.FieldTransform
Compute the Jacobian of the FieldTransform.transformPVCoordinates(FieldPVCoordinates) method of the transform.
getJacobian(CartesianDerivativesFilter, double[][]) - Method in class org.orekit.frames.Transform
Compute the Jacobian of the Transform.transformPVCoordinates(PVCoordinates) method of the transform.
getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in interface org.orekit.propagation.MatricesHarvester
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobianWrtCartesian(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtParameters(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJacobianWrtParameters(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJavaEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getJavaEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
getJavaEpoch() - Method in interface org.orekit.time.TimeScales
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
getJD0() - Method in class org.orekit.time.GLONASSDate
Get the current Julian date JD0.
getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the Jjs coefficient.
getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Jjs coefficient.
getJulianDay() - Method in class org.orekit.files.sp3.SP3
Returns the julian day for this SP3 file.
getJulianEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
getJulianEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
getJupiter() - Method in interface org.orekit.bodies.CelestialBodies
Get the Jupiter singleton body.
getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Jupiter singleton body.
getJupiter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getJupiterSemiMajorAxis(AbsoluteDate, TimeScale) - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants
Get the Jupiter semi-major axis.
getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the x component of eccentricity vector.
getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the x component of eccentricity vector.
getK2MH2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get k² - h².
getK2MH2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get k² - h².
getK2MH2O2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get (k² - h²) / 2.
getK2MH2O2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get (k² - h²) / 2.
getKeplerianElementsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Get the Keplerian elements logical block.
getKeplerianElementsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get the Keplerian elements logical block.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.FieldOrbit
Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.Orbit
Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.SpacecraftState
Get the Keplerian mean motion.
getKeplerianPeriod() - Method in class org.orekit.orbits.FieldOrbit
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.orbits.Orbit
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.SpacecraftState
Get the Keplerian period.
getKey() - Method in enum org.orekit.gnss.clock.RinexClock.ClockDataType
Get the key for the system.
getKey() - Method in enum org.orekit.gnss.SatelliteSystem
Get the key for the system.
getKey() - Method in enum org.orekit.gnss.TimeSystem
Get the key for the system.
getKey() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
Get the entry key.
getKey() - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Get the entry key.
getKlobucharAlpha() - Method in class org.orekit.gnss.navigation.RinexNavigation
Get the "alpha" ionospheric parameters.
getKlobucharBeta() - Method in class org.orekit.gnss.navigation.RinexNavigation
Get the "beta" ionospheric parameters.
getKpSum() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the sum of all eight Kp indices for the current entry.
getKXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get kXXX = h * Χ³.
getKXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get kXXX = h * Χ³.
getL() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Moon.
getL() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Moon.
getL(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit
Get the longitude argument.
getL(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the longitude argument.
getLabel() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame
Get the frame label.
getLagrangianPoint() - Method in class org.orekit.orbits.RichardsonExpansion
Get the considered lagrangian point.
getLambda() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getLambda() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the longitude of ascending node of orbit.
getLaserId() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the laser configuration ID.
getLaserRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the laser configuration record.
getLaserType() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the laser type.
getLast() - Static method in enum org.orekit.frames.ITRFVersion
Get last supported ITRF version.
getLastDailyPredictedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Gets the day (at data start) of the last daily data entry.
getLastEstimations() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the last estimations performed.
getLastKnownLeapSecond() - Method in class org.orekit.time.UTCScale
Get the date of the last known leap second.
getLastObservedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Gets the day (at data start) of the last observed data entry.
getLastSpan() - Method in class org.orekit.utils.TimeSpanMap
Get the last (latest) span.
getLastTransition() - Method in class org.orekit.utils.TimeSpanMap
Get the last (latest) transition.
getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the latest cached entry.
getLatest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get the latest entry in this cache.
getLatest() - Method in interface org.orekit.utils.TimeStampedCache
Get the latest entry in this cache.
getLatitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the latitude.
getLatitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the latitude.
getLatitude() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the latitude.
getLatitude() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the latitude.
getLatitude() - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Get the fixed latitude to be crossed (radians).
getLatitude() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Get the fixed latitude to be crossed (radians).
getLaunchNumber() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Get the launch number.
getLaunchNumber() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Get the launch number.
getLaunchNumber(String) - Method in class org.orekit.files.ccsds.section.Metadata
Get the launch number.
getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the launch number.
getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch number.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Get the piece of launch.
getLaunchPiece(String) - Method in class org.orekit.files.ccsds.section.Metadata
Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the launch piece.
getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch piece.
getLaunchYear() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Get the launch year.
getLaunchYear() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Get the launch year.
getLaunchYear(String) - Method in class org.orekit.files.ccsds.section.Metadata
Get the launch year.
getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the launch year.
getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch year.
getLDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Moon time derivative.
getLDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Moon time derivative.
getLDot(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit
Get the longitude argument derivative.
getLDot(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the longitude argument derivative.
getLE() - Method in class org.orekit.data.BodiesElements
Get the mean Earth longitude.
getLE() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Earth longitude.
getLE() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.Orbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the eccentric latitude argument (as per equinoctial parameters).
getLe() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the eccentric longitude.
getLE() - Method in class org.orekit.propagation.SpacecraftState
Get the eccentric latitude argument (as per equinoctial parameters).
getLeap() - Method in class org.orekit.files.ilrs.CPF.CPFCoordinate
Get the leap second flag (= 0 or the value of the new leap second).
getLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
Get the value of the previous leap.
getLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
Get the value of the previous leap.
getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
Get the value of the previous leap.
getLeap() - Method in class org.orekit.time.UTCTAIOffset
Get the value of the leap at offset validity start (in seconds).
getLeapSeconds() - Method in class org.orekit.gnss.RinexObservationHeader
Get the Number of leap seconds since 6-Jan-1980.
getLeapSecondsDayNum() - Method in class org.orekit.gnss.RinexObservationHeader
Get the respective leap second day number.
getLeapSecondsFuture() - Method in class org.orekit.gnss.RinexObservationHeader
Get the future or past leap seconds.
getLeapSecondsWeekNum() - Method in class org.orekit.gnss.RinexObservationHeader
Get the respective leap second week number.
getLEDot() - Method in class org.orekit.data.BodiesElements
Get the mean Earth longitude time derivative.
getLEDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Earth longitude time derivative.
getLEDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.Orbit
Get the eccentric longitude argument derivative.
getLength() - Method in class org.orekit.utils.units.Unit
Get the length exponent.
getLf() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the eccentric longitude.
getLightingRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the lighting ratio ([0-1]).
getLightingRatio(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the lighting ratio ([0-1]).
getLine() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader
Deprecated.
Get the last line read from the stream.
getLine1() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the first line.
getLine1() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the first line.
getLine2() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the second line.
getLine2() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the second line.
getLineNumber() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the number of the line in the CCSDS data message.
getLineNumber() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader
Deprecated.
Get the line number of the last line read from the file.
getListAppliedDCBS() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the applied differential code bias corrections.
getListAppliedDCBS() - Method in class org.orekit.gnss.RinexObservationHeader
Get the list of applied differential code bias corrections.
getListAppliedPCVS() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the applied phase center variations.
getListAppliedPCVS() - Method in class org.orekit.gnss.RinexObservationHeader
Get the list of antenna center variation corrections.
getLJu() - Method in class org.orekit.data.BodiesElements
Get the mean Jupiter longitude.
getLJu() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Jupiter longitude.
getLJuDot() - Method in class org.orekit.data.BodiesElements
Get the mean Jupiter longitude time derivative.
getLJuDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Jupiter longitude time derivative.
getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Compute the limits in L, the true longitude, for integration.
getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Compute the limits in L, the true longitude, for integration.
getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Compute the limits in L, the true longitude, for integration.
getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Compute the limits in L, the true longitude, for integration.
getLM() - Method in class org.orekit.orbits.CartesianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.CircularOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.Orbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the mean longitude argument (as per equinoctial parameters).
getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the mean longitude.
getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the mean longitude.
getLM() - Method in class org.orekit.propagation.SpacecraftState
Get the mean longitude argument (as per equinoctial parameters).
getLMa() - Method in class org.orekit.data.BodiesElements
Get the mean Mars longitude.
getLMa() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mars longitude.
getLMaDot() - Method in class org.orekit.data.BodiesElements
Get the mean Mars longitude time derivative.
getLMaDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mars longitude time derivative.
getLMDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.CircularOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.Orbit
Get the mean longitude argument derivative.
getLMe() - Method in class org.orekit.data.BodiesElements
Get the mean Mercury longitude.
getLMe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mercury longitude.
getLMeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Mercury longitude time derivative.
getLMeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mercury longitude time derivative.
getLNe() - Method in class org.orekit.data.BodiesElements
Get the mean Neptune longitude.
getLNe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Neptune longitude.
getLNeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Neptune longitude time derivative.
getLNeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Neptune longitude time derivative.
getLNFifthString() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS ln Word extracted from fifth string of the subframe.
getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients
Get the value of Lns(γ).
getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Get the value of Lns(γ).
getLNThirdString() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS ln Word extracted from third string of the subframe.
getLoadedAstronomicalUnit() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get astronomical unit.
getLoadedConstant(String...) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get a constant defined in the ephemerides headers.
getLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager
Get an unmodifiable view of the set of data file names that have been loaded.
getLoadedEarthMoonMassRatio() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get Earth/Moon mass ratio.
getLoadedGravitationalCoefficient(JPLEphemeridesLoader.EphemerisType) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get the gravitational coefficient of a body.
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitInternalError
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIOException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitParseException
getLocalizedString(Locale) - Method in enum org.orekit.errors.OrekitMessages
getLocalTimingId() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Get the local timing system configuration ID.
getLocation() - Method in class org.orekit.gnss.DOP
Gets the location with respect to the Earth where DOP was calculated.
getLod() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the length of day.
getLOD() - Method in class org.orekit.frames.EOPEntry
Get the LoD (Length of Day) value.
getLOD(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the LoD (Length of Day) value.
getLOD(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the LoD (Length of Day) value.
getLofCartesianOrbitalParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the lofCartesianOrbitalParametersEvolution.
getLofType() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the lofType.
getLofType() - Method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Get the type of Local Orbital frame.
getLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger
Get an immutable copy of the logged events.
getLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger
Get an immutable copy of the logged events.
getLongitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the longitude.
getLongitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the longitude.
getLongitude() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the longitude.
getLongitude() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the longitude.
getLongitude() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Get the fixed longitude to be crossed (radians).
getLossOfLockIndicator() - Method in class org.orekit.gnss.ObservationData
Get the Loss of Lock Indicator.
getLoveNumbers() - Method in enum org.orekit.utils.IERSConventions
Get the Love numbers.
getLowElevationThreshold() - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
Get the low elevation threshold value for path delay computation.
getLowerCaseAbbreviation() - Method in enum org.orekit.time.Month
Get the lower case three letters abbreviation.
getLowerCaseName() - Method in enum org.orekit.time.Month
Get the lower case full name.
getLowReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get a reference to the lower triangular matrix of the decomposition.
getLPosition(LagrangianPoints) - Method in class org.orekit.bodies.CR3BPSystem
Get the position of the Lagrangian point in the CR3BP Rotating frame.
getLPrime() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Sun.
getLPrime() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Sun.
getLPrimeDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Sun time derivative.
getLPrimeDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Sun time derivative.
getLSa() - Method in class org.orekit.data.BodiesElements
Get the mean Saturn longitude.
getLSa() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Saturn longitude.
getLSaDot() - Method in class org.orekit.data.BodiesElements
Get the mean Saturn longitude time derivative.
getLSaDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Saturn longitude time derivative.
getLst81Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the last 81-day arithmetic average of F10.7 (adjusted).
getLst81Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the last 81-day arithmetic average of F10.7 (observed).
getLUr() - Method in class org.orekit.data.BodiesElements
Get the mean Uranus longitude.
getLUr() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Uranus longitude.
getLUrDot() - Method in class org.orekit.data.BodiesElements
Get the mean Uranus longitude time derivative.
getLUrDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Uranus longitude time derivative.
getLv() - Method in class org.orekit.orbits.CartesianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.CircularOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.Orbit
Get the true longitude argument.
getLv() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the true latitude argument (as per equinoctial parameters).
getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the true longitude.
getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the true longitude.
getLv() - Method in class org.orekit.propagation.SpacecraftState
Get the true latitude argument (as per equinoctial parameters).
getLvDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.CircularOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.Orbit
Get the true longitude argument derivative.
getLVe() - Method in class org.orekit.data.BodiesElements
Get the mean Venus longitude.
getLVe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Venus longitude.
getLVeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Venus longitude time derivative.
getLVeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Venus longitude time derivative.
getLyapunovOrbitalPeriod(double) - Method in class org.orekit.orbits.RichardsonExpansion
Return the orbital period of the Halo Orbit.
getM() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS M Word.
getM0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the mean anomaly at reference time.
getM0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Mean Anomaly at Reference Time.
getM2() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Get the value of the M2 drag parameter.
getM2() - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Get the value of the M2 drag parameter.
getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get m2aoA = -2 * a / A.
getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get m2aoA = -2 * a / A.
getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get m2aoA = -2 * a / A.
getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get m2aoA = -2 * a / A.
getMainStateDerivativesIncrements() - Method in class org.orekit.propagation.integration.CombinedDerivatives
Get the derivatives increments related to the main state.
getMainStateDerivativesIncrements() - Method in class org.orekit.propagation.integration.FieldCombinedDerivatives
Get the derivatives increments related to the main state.
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
 
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get the differential equations to integrate (for main state only).
getManagedAdditionalStates() - Method in class org.orekit.propagation.AbstractPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.analytical.Ephemeris
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.FieldPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.Propagator
Get all the names of all managed states.
getManBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get basis of this maneuver history data.
getManBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get identification number of the orbit determination or simulation upon which this maneuver is based.
getManComposition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get maneuver elements of information.
getManDeviceID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get identifier of the device used for this maneuver.
getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get a maneuver.
getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Get a maneuver.
getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get a maneuver.
getManeuverable() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the ability of object to maneuver or not.
getManeuverAttitudeProvider() - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Attitude provider to use.
getManeuverBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Get maneuvers logical blocks.
getManeuvers() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get a list of all maneuvers.
getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistory
Get the maneuvers.
getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Get a list of all maneuvers.
getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get a list of all maneuvers.
getManeuversFrequency() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the average frequency of orbit or attitude maneuvers (in SI units, hence per second).
getManeuversPerYear() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the average number of orbit or attitude maneuvers per year.
getManeuverTriggers() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the maneuver triggers.
getManFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get epoch of the maneuver reference frame.
getManID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get maneuver identification number.
getManifolds(SpacecraftState, boolean) - Method in class org.orekit.orbits.LibrationOrbit
Return a manifold direction from one position on a libration Orbit.
getManNextEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get start time of next maneuver.
getManNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get identification number of next maneuver.
getManPredSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get prediction source on which this maneuver is based.
getManPrevEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get completion time of previous maneuver.
getManPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get identification number of previous maneuver.
getManPurpose() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get the purposes of the maneuver.
getManReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get reference frame of the maneuver.
getManufacturer() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get manufacturer name.
getManUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Get maneuver elements of information units.
getMapFilters() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother
Get the map storing the filters for each observation type.
getMapFilters() - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother
Get the map storing the filters for each observation type.
getMapper() - Method in class org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations
Deprecated.
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMapper() - Method in class org.orekit.propagation.numerical.AbsolutePartialDerivativesEquations
Deprecated.
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMapper() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMapper() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Deprecated.
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMapper() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Deprecated.
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMappers() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Deprecated.
as of 11.1, not used anymore
getMargin() - Method in class org.orekit.geometry.fov.AbstractFieldOfView
Get the angular margin to apply (radians).
getMargin() - Method in interface org.orekit.geometry.fov.FieldOfView
Get the angular margin to apply (radians).
getMargin() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the angular margin to apply (radians).
getMarkerName() - Method in class org.orekit.gnss.RinexObservationHeader
Get name of the antenna marker.
getMarkerNumber() - Method in class org.orekit.gnss.RinexObservationHeader
Get number of the antenna marker.
getMarkerType() - Method in class org.orekit.gnss.RinexObservationHeader
Get type of the antenna marker.
getMars() - Method in interface org.orekit.bodies.CelestialBodies
Get the Mars singleton body.
getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Mars singleton body.
getMars() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getMass() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the mass of the object.
getMass() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Get the mass.
getMass() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get the mass.
getMass() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Get the spacecraft mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the mass.
getMass() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Get the mass.
getMass() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Get the mass.
getMass() - Method in class org.orekit.propagation.FieldSpacecraftState
Gets the current mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the mass.
getMass() - Method in class org.orekit.propagation.SpacecraftState
Gets the current mass.
getMass() - Method in class org.orekit.utils.units.Unit
Get the mass exponent.
getMassDepletionDelay() - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
Get the mass depletion effect processor.
getMassDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the mass derivative (i.e.
getMassDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the mass derivative (i.e.
getMassDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the mass derivative (i.e.
getMassDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the mass derivative (i.e.
getMassRatio() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP mass ratio of the system mu2/(mu1+mu2).
getMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Covariance
Get the covariance matrix.
getMatrixLine(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Get a line of the matrix.
getMaxAlt() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the maximal altitude for the model.
getMaxAR3Pow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get the value of max power for a/R3 in the serie expansion.
getMaxAR3Pow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get the value of max power for a/R3 in the serie expansion.
getMaxAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the maximum cross-sectional area for collision probability estimation purposes.
getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the maximal degree available in the last file parsed.
getMaxAvailableOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the maximal order available in the last file parsed.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.AbstractDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.AdapterDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.EventDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.FieldEventDetector
Get maximal time interval between switching function checks.
getMaxChunksDuration() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get the maximal chunks duration.
getMaxDate() - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
Get the last date of the range.
getMaxDate() - Method in interface org.orekit.attitudes.BoundedAttitudeProvider
Get the last date of the range.
getMaxDate() - Method in class org.orekit.attitudes.TabulatedLofOffset
Get the last date of the range.
getMaxDate() - Method in class org.orekit.attitudes.TabulatedProvider
Get the last date of the range.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getMaxDate() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator
Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator
Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the last date of the range.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the maximal supported degree.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the maximum supported degree.
getMaxDegree() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the maximal supported degree.
getMaxDistance() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the maximum of distance among the solutions found.
getMaxEccPow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get the value of max power for e in the serie expansion.
getMaxEccPow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get the value of max power for e in the serie expansion.
getMaxFreqF() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get the value of max frequency of F.
getMaxFreqF() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get the value of max frequency of F.
getMaximumObsGap() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get maximum time between observations in the OD of the object.
getMaxIterationCount() - Method in class org.orekit.propagation.events.AbstractDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.AdapterDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.EventDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.FieldEventDetector
Get maximal number of iterations in the event time search.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the maximal supported order.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the maximum supported order.
getMaxOrder() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the maximal supported order.
getMaxOrder() - Method in enum org.orekit.utils.AngularDerivativesFilter
Get the maximum derivation order.
getMaxOrder() - Method in enum org.orekit.utils.CartesianDerivativesFilter
Get the maximum derivation order.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the degree limit for the next file parsing.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the degree limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the order limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the order limit for the next file parsing.
getMaxPredictedEigenMaj() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get maximum predicted major eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
getMaxRcs() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the maximum radar cross-section.
getMaxSigma() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
Get the value of the outlier detection limit.
getMaxSlots() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the maximum number of independent cached time slots.
getMaxSolution() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the maximum number of solutions seeked.
getMaxSpan() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the maximum duration span in seconds of one slot.
getMaxThrust() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the maximum composite thrust the spacecraft can accomplish.
getMaxTimeBeetween2Measurement() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Get the maximum time lapse between 2 measurements without considering a cycle-slip has occurring between both.
getMaxValue() - Method in class org.orekit.utils.ParameterDriver
Get maximum parameter value.
getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get mCo2AB = -C / 2AB.
getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get mCo2AB = -C / 2AB.
getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get mCo2AB = -C / 2AB.
getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get mCo2AB = -C / 2AB.
getMeanAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean anomaly.
getMeanAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean anomaly derivative.
getMeanAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean anomaly derivative.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AbstractGaussianContribution.GaussQuadrature, double, double, AbstractGaussianContributionContext, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, AbstractGaussianContribution.GaussQuadrature, T, T, FieldAbstractGaussianContributionContext<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Computes the mean equinoctial elements rates dai / dt.
getMeanElementTheory() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
Get the description of the Mean Element Theory.
getMeanFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the mean solar flux.
getMeanFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the mean solar flux.
getMeanFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Get the value of the mean solar flux.
getMeanMotion() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the orbit mean motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Getter for the mean motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Getter for the mean motion.
getMeanMotion() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Mean Motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the mean motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the Keplerian mean motion.
getMeanMotionDot() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the first time derivative of the mean motion.
getMeanMotionDotDot() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the second time derivative of the mean motion.
getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the mean motion first derivative.
getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion first derivative.
getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the mean motion second derivative.
getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion second derivative.
getMeanObliquityFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing mean obliquity of the ecliptic.
getMeanObliquityFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing mean obliquity of the ecliptic.
getMeasurement() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation
Getter for the measurement.
getMeasurements() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement
Get the underlying measurements.
getMeasurementsParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the measurements parameters supported by this estimator (including measurements and modifiers).
getMeasurementsParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the measurementsParametersEvolution.
getMeasurementType() - Method in class org.orekit.gnss.CombinedObservationData
Get the measurement type.
getMeasurementType() - Method in enum org.orekit.gnss.ObservationType
Get the measurement type.
getMedianDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Get the driver for median date.
getMedianDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Get the driver for median date.
getMelbourneWubbenaCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Melbourne-Wübbena combination of measurements.
getMercury() - Method in interface org.orekit.bodies.CelestialBodies
Get the Mercury singleton body.
getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Mercury singleton body.
getMercury() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getMessage(Locale) - Method in interface org.orekit.errors.LocalizedException
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalArgumentException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalStateException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitInternalError
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitInternalError
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIOException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitIOException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitParseException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitParseException
getMessageFor() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmHeader
Get the spacecraft name for which the CDM is provided stored in MESSAGE_FOR key.
getMessageId() - Method in class org.orekit.files.ccsds.section.Header
Get the ID that uniquely identifies a message from a given originator.
getMessageType(String) - Method in class org.orekit.gnss.metric.parser.IgsSsrMessagesParser
Get the message type corresponding to the message number.
getMessageType(String) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
Get the message type corresponding to a message number.
getMessageType(String) - Method in class org.orekit.gnss.metric.parser.MessagesParser
Get the message type corresponding to the message number.
getMessageType(String) - Method in class org.orekit.gnss.metric.parser.RtcmMessagesParser
Get the message type corresponding to the message number.
getMessageType(String) - Static method in enum org.orekit.gnss.metric.parser.RtcmMessageType
Get the message type corresponding to a message number.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm
Get the file metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistory
Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistory
Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Get the metadata from the single segment.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Get the file metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Get the file metadata.
getMetadata() - Method in class org.orekit.files.ccsds.section.Segment
Get the segment metadata.
getMetadataObject1() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm
Get the file metadata.
getMetadataObject2() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm
Get the file metadata.
getMeteo(AbsoluteDate) - Method in class org.orekit.files.ilrs.CRD.Meteo
Get the meteorological parameters at a given date.
getMeteoData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the meteorological data for the data block.
getMeteorologicalId() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the meteorological configuration ID.
getMeteorologicalRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the meteorological record.
getMethod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get orbit determination method.
getMHzFrequency() - Method in enum org.orekit.gnss.Frequency
Get the value of the frequency in MHz.
getMilliInWeek() - Method in class org.orekit.time.GNSSDate
Get the number of milliseconds since week start.
getMinAlt() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the minimal altitude for the model.
getMinAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the minimum cross-sectional area for collision probability estimation purposes.
getMinDate() - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
Get the first date of the range.
getMinDate() - Method in interface org.orekit.attitudes.BoundedAttitudeProvider
Get the first date of the range.
getMinDate() - Method in class org.orekit.attitudes.TabulatedLofOffset
Get the first date of the range.
getMinDate() - Method in class org.orekit.attitudes.TabulatedProvider
Get the first date of the range.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getMinDate() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.BoundedPropagator
Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator
Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the first date of the range.
getMinElevation() - Method in class org.orekit.gnss.DOPComputer
Get the minimum elevation.
getMinElevation() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured minimum valid elevation value.
getMinElevation() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured minimum valid elevation value.
getMinMeasurementNumber() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Get the minimum number of measurement needed before being able to figure out cycle-slip occurrence.
getMinPredictedEigenMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get minimum predicted minor eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
getMinRcs() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the minimum radar cross-section.
getMinute() - Method in class org.orekit.time.TimeComponents
Get the minute number.
getMinutesFromUTC() - Method in class org.orekit.time.TimeComponents
Get the offset between the specified date and UTC.
getMinValue() - Method in class org.orekit.utils.ParameterDriver
Get minimum parameter value.
getMisc() - Method in class org.orekit.gnss.metric.ntrip.Record
Get miscellaneous information.
getMissDistance() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the norm of relative position vector at TCA.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Get the mission reference date or Mission Elapsed Time or Mission Relative Time time systems.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.adm.AdmParser
Get reference date for Mission Elapsed Time and Mission Relative Time time systems.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
Get reference date for Mission Elapsed Time and Mission Relative Time time systems.
getMjd() - Method in class org.orekit.frames.EOPEntry
Get the entry date (modified julian day, 00h00 UTC scale).
getMJD() - Method in class org.orekit.time.DateComponents
Get the modified julian day.
getMJD() - Method in class org.orekit.time.UTCTAIOffset
Get the date of the start of the leap as Modified Julian Day.
getMJDRef() - Method in class org.orekit.time.OffsetModel
Get the reference date of the linear model as a modified julian day.
getMoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get μ / a .
getMoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get μ / a .
getMOD(boolean) - Method in class org.orekit.frames.AbstractFrames
 
getMOD(IERSConventions) - Method in class org.orekit.frames.AbstractFrames
 
getMOD(boolean) - Method in interface org.orekit.frames.Frames
Get the MOD reference frame.
getMOD(IERSConventions) - Method in interface org.orekit.frames.Frames
Get the MOD reference frame.
getMOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the MOD reference frame.
getMOD(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the MOD reference frame.
getMode() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the mode.
getModel() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the Jacobian of the function computing position/velocity at sample points.
getModel() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter
Get the Jacobian of the function computing position/velocity at sample points.
getModel() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter
Get the Jacobian of the function computing position/velocity at sample points.
getModelName() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the model name.
getModels() - Method in class org.orekit.models.earth.GeoMagneticModelLoader
Returns a Collection of the GeoMagneticField models that have been successfully loaded.
getModifiedJulianEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getModifiedJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
getModifiedJulianEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
getModifiedRodrigues(double) - Method in class org.orekit.utils.AngularCoordinates
Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.
getModifiedRodrigues(double) - Method in class org.orekit.utils.FieldAngularCoordinates
Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.
getModifiers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the modifiers that apply to a measurement.
getModifiers() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the modifiers that apply to a measurement.
getModifiers() - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Get the modifiers that apply to a measurement.
getModifiers() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the modifiers that apply to a measurement.
getMomentum() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the momentum.
getMomentum() - Method in class org.orekit.utils.PVCoordinates
Gets the momentum.
getMonth() - Method in class org.orekit.time.DateComponents
Get the month.
getMonth(int) - Static method in enum org.orekit.time.Month
Get the month corresponding to a number.
getMonthEnum() - Method in class org.orekit.time.DateComponents
Get the month as an enumerate.
getMoon() - Method in interface org.orekit.bodies.CelestialBodies
Get the Moon singleton body.
getMoon() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Moon singleton body.
getMoon() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getMoonSemiMajorAxis() - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants
Get the Moon semi-major axis.
getMountPoint() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the mount point.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the gravitational coefficient.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Get the gravitational coefficient.
getMu() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the standard gravitational parameter for the satellite.
getMu() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
 
getMu() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the central attraction coefficient μ.
getMu(Field<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the central body attraction coefficient.
getMu() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the central body attraction coefficient.
getMu() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the central body attraction coefficient.
getMu() - Method in class org.orekit.orbits.FieldOrbit
Get the central attraction coefficient used for position and velocity conversions (m³/s²).
getMu() - Method in class org.orekit.orbits.Orbit
Get the central acceleration constant.
getMu() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the Earth's universal gravitational parameter.
getMu() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Earth's universal gravitational parameter.
getMU() - Static method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Get the Earth gravity coefficient used for GLONASS propagation.
getMU() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Gets the Earth gravity coefficient used for GNSS propagation.
getMU() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Get the Earth gravity coefficient used for SBAS propagation.
getMU() - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Get the Earth gravity coefficient used for TLE propagation.
getMU() - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the Earth gravity coefficient used for TLE propagation.
getMu() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the central attraction coefficient (µ - m³/s²) value.
getMu() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the central attraction coefficient.
getMu() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.StateMapper
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get central attraction coefficient.
getMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get central attraction coefficient.
getMu() - Method in class org.orekit.propagation.SpacecraftState
Get the central attraction coefficient.
getMultiplexer() - Method in class org.orekit.propagation.AbstractPropagator
Get the multiplexer holding all step handlers.
getMultiplexer() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the multiplexer holding all step handlers.
getMultiplexer() - Method in interface org.orekit.propagation.FieldPropagator
Get the multiplexer holding all step handlers.
getMultiplexer() - Method in interface org.orekit.propagation.Propagator
Get the multiplexer holding all step handlers.
getMuoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get μ / a .
getMuoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get μ / a .
getMuoR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get muoR3 = mu3 / R3.
getMuoR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get muoR3 = mu3 / R3.
getMuSet() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
Get the gravitational coefficient set at construction.
getN() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
Get n.
getN4() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the four-year interval number starting from 1996.
getN4() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getN4() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getN4() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the number of the current four year interval.
getNA() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS NA Word.
getNa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getNa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getNa() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the number of the current day in a four year interval.
getNadir() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction below the point, expressed in parent shape frame.
getNadir() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction below the point, expressed in parent shape frame.
getNadir() - Method in class org.orekit.frames.TopocentricFrame
Get the nadir direction of topocentric frame, expressed in parent shape frame.
getName() - Method in interface org.orekit.bodies.CelestialBody
Get the name of the body.
getName() - Method in class org.orekit.bodies.CR3BPSystem
Get the name of the CR3BP system.
getName() - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
 
getName() - Method in class org.orekit.data.DataSource
Get the name of the data.
getName() - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Get the name of the combination of measurements.
getName() - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Get the name of the combination of measurements.
getName() - Method in enum org.orekit.estimation.measurements.gnss.CombinationType
Get the name of the combination of measurements.
getName() - Method in interface org.orekit.estimation.measurements.gnss.MeasurementCombination
Get the name of the combination of measurements.
getName() - Method in class org.orekit.estimation.measurements.gnss.MelbourneWubbenaCombination
Get the name of the combination of measurements.
getName() - Method in class org.orekit.files.ccsds.definitions.BodyFacade
Get the CCSDS name for the body.
getName() - Method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
Get the name of celestial body frame.
getName() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the CCSDS name for the frame.
getName() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade
Get the name of the method.
getName() - Method in class org.orekit.files.ccsds.definitions.PocMethodFacade
Get the name of the method.
getName() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the name of the block or entry.
getName() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the satellite target name.
getName() - Method in enum org.orekit.files.sinex.Station.ReferenceSystem
Get the name used to define the reference system in SINEX file.
getName() - Method in class org.orekit.forces.maneuvers.jacobians.Duration
Get the name of the additional state.
getName() - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate
Get the name of the additional state.
getName() - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
Get the name of the additional state.
getName() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the name of the maneuver.
getName() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the maneuver name.
getName() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the maneuver name.
getName() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Get the maneuver name.
getName() - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Get the maneuver name.
getName() - Method in class org.orekit.frames.Frame
Get the name.
getName() - Method in enum org.orekit.frames.ITRFVersion
Get the name the frame version.
getName() - Method in enum org.orekit.frames.Predefined
Get the name of the frame.
getName() - Method in enum org.orekit.gnss.antenna.SatelliteType
Get the IGS name for the antenna code.
getName() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
Getter for the receiver/satellite name.
getName() - Method in enum org.orekit.gnss.Frequency
Get the RINEX name for the frequency.
getName() - Method in interface org.orekit.propagation.AdditionalStateProvider
Get the name of the additional state.
getName() - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Get the name of the additional state.
getName() - Method in class org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations
Deprecated.
Get the name of the additional state.
getName() - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
Get the name of the additional state.
getName() - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Get the name of the partial Jacobians.
getName() - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in interface org.orekit.propagation.integration.AdditionalEquations
Deprecated.
Get the name of the additional state.
getName() - Method in class org.orekit.propagation.integration.AdditionalEquationsAdapter
Deprecated.
Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations
Deprecated.
Get the name of the additional state.
getName() - Method in class org.orekit.propagation.integration.FieldAdditionalEquationsAdapter
Deprecated.
Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Deprecated.
Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Deprecated.
Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.time.BDTScale
Get the name time scale.
getName() - Method in class org.orekit.time.GalileoScale
Get the name time scale.
getName() - Method in class org.orekit.time.GLONASSScale
Get the name time scale.
getName() - Method in class org.orekit.time.GMSTScale
Get the name time scale.
getName() - Method in class org.orekit.time.GPSScale
Get the name time scale.
getName() - Method in class org.orekit.time.IRNSSScale
Get the name time scale.
getName() - Method in class org.orekit.time.QZSSScale
Get the name time scale.
getName() - Method in class org.orekit.time.SatelliteClockScale
Get the name time scale.
getName() - Method in class org.orekit.time.TAIScale
Get the name time scale.
getName() - Method in class org.orekit.time.TCBScale
Get the name time scale.
getName() - Method in class org.orekit.time.TCGScale
Get the name time scale.
getName() - Method in class org.orekit.time.TDBScale
Get the name time scale.
getName() - Method in interface org.orekit.time.TimeScale
Get the name time scale.
getName() - Method in class org.orekit.time.TTScale
Get the name time scale.
getName() - Method in class org.orekit.time.UT1Scale
Get the name time scale.
getName() - Method in class org.orekit.time.UTCScale
Get the name time scale.
getName() - Method in class org.orekit.utils.ParameterDriver
Get name.
getName() - Method in class org.orekit.utils.units.Unit
Get the name of the unit.
getNarrowLaneCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Narrow-Lane combination of measurements.
getNavigationSystem(String) - Static method in enum org.orekit.gnss.metric.ntrip.NavigationSystem
Get the navigation system corresponding to a keyword.
getNavigationSystems() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the navigation systems.
getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the number of maneuvers present in the APM.
getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Get the number of maneuvers present in the OPM.
getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get the number of maneuvers present in the APM.
getNBodyPerturbations() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get n-body perturbation bodies.
getNBodyPerturbations() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get n-body perturbation bodies.
getNbParams() - Method in class org.orekit.utils.ParameterDriversList
Get the number of parameters with different names.
getNbSpecies() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the number of species.
getNbTides(int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the number of tides for one species.
getNeighbors(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in class org.orekit.utils.GenericTimeStampedCache
Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedCache
Get the entries surrounding a central date.
getNeighborsSize() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the fixed size of the arrays to be returned by GenericTimeStampedCache.getNeighbors(AbsoluteDate).
getNeighborsSize() - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get the fixed size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate).
getNeighborsSize() - Method in interface org.orekit.utils.TimeStampedCache
Get the fixed size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate).
getNeptune() - Method in interface org.orekit.bodies.CelestialBodies
Get the Neptune singleton body.
getNeptune() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Neptune singleton body.
getNeptune() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getNeQuickAlpha() - Method in class org.orekit.gnss.navigation.RinexNavigation
Get the "alpha" ionospheric parameters.
getNetwork() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the network.
getNetworkIdentifier() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Get the network identifier.
getNetworkInfoAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Get the web address for network information.
getNetworks() - Method in class org.orekit.gnss.metric.ntrip.SourceTable
Get the networks records.
getNewSlotQuantumGap() - Method in class org.orekit.utils.GenericTimeStampedCache
Get quantum gap above which a new slot is created instead of extending an existing one.
getNewState() - Method in class org.orekit.propagation.events.EventState.EventOccurrence
Get the new state for a reset action.
getNewState() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence
Get the new state for a reset action.
getNextLeapEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the epoch of next leap second.
getNextLeapTaimutc() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the difference (TAI – UTC) in seconds incorporated at epoch OcmMetadata.getNextLeapEpoch().
getNextMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the creation date of next message from a given originator.
getNextMessageID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the unique ID identifying next message from a given originator.
getNode(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole
Get the body Q Node direction in ICRF frame.
getNode(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole
Get the body Q Node direction in ICRF frame.
getNoise() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Generate a noise vector.
getNominalFireRate() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the nominal fire rate.
getNominalTidalDisplacement() - Method in enum org.orekit.utils.IERSConventions
Get the nominal values of the displacement numbers.
getNonInterpolatingEOPHistory() - Method in class org.orekit.frames.EOPHistory
Get non-interpolating version of the instance.
getNonInterpolatingProvider() - Method in interface org.orekit.frames.EOPBasedTransformProvider
Get a version of the provider that does not cache tidal corrections.
getNonInterpolatingProvider() - Method in class org.orekit.frames.GTODProvider
Get a version of the provider that does not cache tidal corrections.
getNonInterpolatingTransform(Frame, Frame, AbsoluteDate) - Static method in class org.orekit.frames.FramesFactory
Get the transform between two frames, suppressing all interpolation.
getNonInterpolatingTransform(Frame, Frame, FieldAbsoluteDate<T>) - Static method in class org.orekit.frames.FramesFactory
Get the transform between two frames, suppressing all interpolation.
getNonPolynomialSize() - Method in class org.orekit.data.PoissonSeries
Get the number of different terms in the non-polynomial part.
getNonRotatinOriginNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for Non-Rotating Origin paradigm.
getNonRotatinOriginNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for Non-Rotating Origin paradigm.
getNoradID() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the NORAD Catalog Number ("Satellite Number").
getNoradId() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the satellite NORAD ID (i.e.
getNormal() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
Get unit normal vector.
getNormal(AbsoluteDate, Frame, Vector3D, Rotation) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get solar array normal in spacecraft frame.
getNormal(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get solar array normal in spacecraft frame.
getNormalGravity(double) - Method in class org.orekit.models.earth.ReferenceEllipsoid
Gets the normal gravity, that is gravity just due to the reference ellipsoid's potential.
getNormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics
Get a spherical harmonic cosine coefficient.
getNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the gravity field coefficients provider from the first supported file.
getNormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Create a time-independent NormalizedSphericalHarmonicsProvider from canonical coefficients.
getNormalizedProvider(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
getNormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get a gravity field normalized coefficients provider.
getNormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get a gravity field normalized coefficients provider.
getNormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics
Get a spherical harmonic sine coefficient.
getNormalizedValue() - Method in class org.orekit.utils.ParameterDriver
Get normalized value.
getNorth() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the north of point, expressed in parent shape frame.
getNorth() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the north of point, expressed in parent shape frame.
getNorth() - Method in class org.orekit.frames.TopocentricFrame
Get the north direction of topocentric frame, expressed in parent shape frame.
getNorthOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station position along North axis.
getNt() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the current date.
getNtripFlags() - Method in class org.orekit.gnss.metric.ntrip.SourceTable
Get the flags set by server.
getNumber() - Method in interface org.orekit.estimation.measurements.EstimationsProvider
Get the number of evaluations available.
getNumber() - Method in enum org.orekit.time.Month
Get the month number.
getNumberOfBiasesProcessed() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
Get the number of biases processed for the current satellite.
getNumberOfBiasesProcessed() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Get the number of biases processed for the current satellite.
getNumberOfClockDataTypes() - Method in class org.orekit.gnss.clock.RinexClock
Get the number of different clock data types in the file.
getNumberOfConstraints() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the number of constraints.
getNumberOfEpochs() - Method in class org.orekit.files.sp3.SP3
Returns the number of epochs contained in this orbit file.
getNumberOfFreeEpoch() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the number of free epoch.
getNumberOfFreeVariables() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the number of free variables.
getNumberOfIonosphericLayers() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
Get the number of ionospheric layers.
getNumberOfLeapSeconds() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the number of leap seconds.
getNumberOfLeapSeconds() - Method in class org.orekit.gnss.navigation.RinexNavigation
Getter for the current number of leap seconds.
getNumberOfLeapSecondsGNSS() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the number of leap second for GNSS time scales.
getNumberOfReceivers() - Method in class org.orekit.gnss.clock.RinexClock
Get the number of receivers that are considered in the file.
getNumberOfSatellites() - Method in class org.orekit.gnss.clock.RinexClock
Get the number of satellites that are considered in the file.
getNumberOfSatellites() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader
Get the number of satellites for the current IGM message.
getNumberOfValues() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
Getter for the number of values to follow.
getNutation() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the nutation angle of spin axis (rad).
getNutationArguments(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the fundamental nutation arguments.
getNutationArguments(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the fundamental nutation arguments.
getNutationArguments(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the fundamental nutation arguments.
getNutationCorrectionConverter() - Method in enum org.orekit.utils.IERSConventions
Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.
getNutationCorrectionConverter(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.
getNutationFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing the nutation angles.
getNutationFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the nutation angles.
getNutationPeriod() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the body nutation period of the spin axis (s).
getNutationPhase() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the inertial nutation phase (rad).
getNutationReferenceEpoch() - Method in enum org.orekit.utils.IERSConventions
Get the reference epoch for fundamental nutation arguments.
getNutationReferenceEpoch(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the reference epoch for fundamental nutation arguments.
getNutLn() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the nutation correction in longitude.
getNutOb() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the nutation correction in obliquity.
getNutX() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the nutation correction X.
getNutY() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the nutation correction Y.
getObject() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the object name for which metadata are given.
getObjectDesignator() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the object satellite catalog designator for which metadata are given.
getObjectDesignator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the unique satellite identification designator for the object.
getObjectID() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Get the spacecraft ID for which the attitude data are provided.
getObjectID() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Get the spacecraft ID for which the orbit state is provided.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the function computing position/velocity at sample points.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter
Get the function computing position/velocity at sample points.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter
Get the function computing position/velocity at sample points.
getObjectName() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Get the spacecraft name for which the attitude data are provided.
getObjectName() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the spacecraft name for the object.
getObjectName() - Method in class org.orekit.files.ccsds.ndm.odm.OdmMetadata
Get the spacecraft name for which the orbit state is provided.
getObjectType() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the type of object.
getObjectType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the type of object.
getOblateFlattening() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get central body oblate spheroid oblateness.
getObsAvailable() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the number of observations available for the OD of the object.
getObsAvailable() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get number of observations available within the actual OD span.
getObservationCode() - Method in class org.orekit.gnss.RinexObservationHeader
Get the observation code of the average phasecenter position w/r to antenna reference point.
getObservationData() - Method in class org.orekit.gnss.CombinedObservationDataSet
Get list of observation data.
getObservationData() - Method in class org.orekit.gnss.ObservationDataSet
Get list of observation data.
getObservationDataSets() - Method in class org.orekit.gnss.RinexObservationLoader
Get parsed rinex observations data sets.
getObservations() - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock
Get the list of Observations data lines.
getObservationType() - Method in class org.orekit.gnss.ObservationData
Get the observation type.
getObservedMeasurement() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the associated observed measurement.
getObservedMeasurement() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
Get the observed measurement.
getObservedValue() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the observed value.
getObservedValue() - Method in interface org.orekit.estimation.measurements.ComparableMeasurement
Get the observed value.
getObservedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the observed value.
getObserver() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the observer for Kalman Filter estimations.
getObserver() - Method in class org.orekit.propagation.events.AngularSeparationDetector
Get the observer for the spacecraft.
getObserverName() - Method in class org.orekit.gnss.RinexObservationHeader
Get name of the observer.
getObservers() - Method in class org.orekit.utils.ParameterDriver
Get the observers for this driver.
getObsUsed() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the number of observations accepted for the OD of the object.
getObsUsed() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get number of observations accepted within the actual OD span.
getOcculted() - Method in class org.orekit.propagation.events.EclipseDetector
Getter for the occulted body.
getOcculted() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the occulted body.
getOccultedRadius() - Method in class org.orekit.propagation.events.EclipseDetector
Getter for the occultedRadius.
getOccultedRadius() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the occulted body radius (m).
getOcculting() - Method in class org.orekit.propagation.events.EclipseDetector
Getter for the occulting body.
getOcculting() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the occulting body.
getOccultingRadius() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the occulting body radius (m).
getOceanLoadDeformationCoefficients() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the configured ocean load deformation coefficients.
getOceanLoadDeformationCoefficients() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get the configured ocean load deformation coefficients.
getOceanPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing ocean pole tide (ΔC₂₁, ΔS₂₁).
getOceanTidesModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get ocean tides model.
getOceanTidesWaves(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the ocean tides waves from the first supported file.
getOceanTidesWaves(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get the ocean tides waves.
getOceanTidesWaves(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get the ocean tides waves.
getOcmDataElements() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the list of elements of information data blocks included in this message.
getODParametersBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Get the OD parameters logical block.
getOebAreaAlongIntermediate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the cross-sectional area of Optimally Enclosing Box along Y-OEB.
getOebAreaAlongMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the cross-sectional area of Optimally Enclosing Box along X-OEB.
getOebAreaAlongMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the cross-sectional area of Optimally Enclosing Box along Z-OEB.
getOebIntermediate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
getOebMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the dimensions of Optimally Enclosing Box along X-OEB (i.e max).
getOebMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the dimensions of Optimally Enclosing Box along Z-OEB (i.e min).
getOebParentFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the Optimally Enclosing Box parent reference frame.
getOebParentFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the Optimally Enclosing Box parent reference frame epoch.
getOebQ() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the quaternion defining Optimally Enclosing Box.
getOffset(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Deprecated.
getOffset(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Deprecated.
as of 11.1, this method is only called by deprecated methods
getOffset() - Method in class org.orekit.time.OffsetModel
Offset at reference date in seconds (TAI minus UTC).
getOffset(AbsoluteDate) - Method in class org.orekit.time.UTCTAIOffset
Get the TAI - UTC offset in seconds.
getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCTAIOffset
Get the TAI - UTC offset in seconds.
getOffset(DateComponents, TimeComponents) - Method in class org.orekit.time.UTCTAIOffset
Get the TAI - UTC offset in seconds.
getOffsetGeodeticPoint(AbsoluteDate) - Method in class org.orekit.estimation.measurements.GroundStation
Get the geodetic point at the center of the offset frame.
getOffsetToInertial(Frame, AbsoluteDate) - Method in class org.orekit.estimation.measurements.GroundStation
Get the transform between offset frame and inertial frame.
getOffsetToInertial(Frame, AbsoluteDate, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation
Get the transform between offset frame and inertial frame with derivatives.
getOffsetToInertial(Frame, FieldAbsoluteDate<Gradient>, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation
Get the transform between offset frame and inertial frame with derivatives.
getOmega() - Method in class org.orekit.data.DelaunayArguments
Get the mean longitude of the ascending node of the Moon.
getOmega() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean longitude of the ascending node of the Moon.
getOmega0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the longitude of ascending node of orbit plane at weekly epoch.
getOmega0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Longitude of Ascending Node of Orbit Plane at Weekly Epoch.
getOmegaDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean longitude of the ascending node of the Moon time derivative.
getOmegaDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean longitude of the ascending node of the Moon time derivative.
getOmegaDot() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the rate of right ascension.
getOmegaDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Rate of Right Ascension.
getOOA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get ooA = 1 / A.
getOOA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get ooA = 1 / A.
getOOAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get ooAB = 1 / (A * B).
getOOAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get ooAB = 1 / (A * B).
getOoBpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get ooBpo = 1 / (B + 1).
getOoBpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get ooBpo = 1 / (B + 1).
getOoMU() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get ooMu = 1 / mu.
getOoMU() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get ooMu = 1 / mu.
getOON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get 1 / (n² * a²).
getOON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get 1 / (n² * a²).
getOpener() - Method in class org.orekit.data.DataSource
Get the data stream opener.
getOperator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the operator of the space object.
getOperator() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the institution/agency/company operating the caster.
getOperator() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Get the institution/agency/company operating the caster.
getOperatorContactPosition() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the contact position of the owner / operator of the object.
getOperatorEmail() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the email of the operator of the object.
getOperatorOrganization() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the contact organisation of the object.
getOperatorPhone() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the contact phone of the operator of the object.
getOpsStatus() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the operational status.
getOptimum() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the optimum found.
getOrbAveraging() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get type of averaging (Osculating, mean Brouwer, other.
getOrbit() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the current orbit.
getOrbit() - Method in class org.orekit.propagation.SpacecraftState
Get the current orbit.
getOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Get the underlying GNSS orbital elements.
getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the orbital parameters supported by this estimator.
getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the orbital parameters supported by this estimator.
getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
Get the orbital parameters supported by this estimator.
getOrbitalParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the drivers for the configurable orbital parameters.
getOrbitalParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the drivers for the configurable orbital parameters.
getOrbitalPeriod() - Method in class org.orekit.orbits.CR3BPDifferentialCorrection
Get the orbital period of the required orbit.
getOrbitalPeriod() - Method in class org.orekit.orbits.LibrationOrbit
Return the orbital period of the libration orbit.
getOrbitCategory() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the orbit category.
getOrbitCenter() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the central body for object 1 and 2.
getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
Get the orbit correction data.
getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
Get the orbit correction data.
getOrbitDeterminationBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Get orbit determination logical block.
getOrbitPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get the Keplerian period.
getOrbitPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get the Keplerian period.
getOrbitType() - Method in class org.orekit.files.sp3.SP3
Returns the SP3.SP3OrbitType for this SP3 file.
getOrbitType() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getOrbitType() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getOrbitType() - Method in class org.orekit.propagation.events.PositionAngleDetector
Get the orbit type defining the angle type.
getOrbitType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.integration.StateMapper
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get propagation parameter type.
getOrbitTypeKey() - Method in class org.orekit.files.sp3.SP3
Returns the orbit type key for this SP3 file.
getOrbRevNum() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get the integer orbit revolution number.
getOrbRevNumBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get the basis for orbit revolution number.
getOrdinateGrid() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the ordinate grid for the interpolation function.
getOrientation() - Method in class org.orekit.attitudes.Attitude
Get the complete orientation including spin.
getOrientation() - Method in class org.orekit.attitudes.FieldAttitude
Get the complete orientation including spin.
getOrigin() - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Get the origin ITRF.
getOrigin() - Method in class org.orekit.frames.ITRFVersion.Converter
Get the origin ITRF.
getOriginal() - Method in class org.orekit.propagation.events.NegateDetector
Get the delegate event detector.
getOriginator() - Method in class org.orekit.files.ccsds.section.Header
Get the file originator.
getOriginatorAddress() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the address of Programmatic Point Of Contact at originator.
getOriginatorEmail() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the email address of Programmatic Point Of Contact at originator.
getOriginatorPhone() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the phone number of Programmatic Point Of Contact at originator.
getOriginatorPOC() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the programmatic Point Of Contact at originator.
getOriginatorPosition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the position of Programmatic Point Of Contact at originator.
getOriginIndicator() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the angle origin indicator.
getOtherOccultingBodies() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Getter for other occulting bodies to consider.
getOTrajectoryBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Get trajectory state histories logical blocks.
getOutputName() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Get the name of the output (for error messages).
getOutputName() - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Get the name of the output (for error messages).
getOutputPulseType() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the output pulse type.
getOutputPulseWidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the output pulse width.
getOwner() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the owner of the space object.
getP() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS P Word.
getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the y component of inclination vector.
getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the y component of inclination vector.
getP1() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS P1 Word.
getP2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS P2 Word.
getP3() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS P3 Word.
getP4() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS P4 Word.
getPa() - Method in class org.orekit.data.BodiesElements
Get the general accumulated precession in longitude.
getPa() - Method in class org.orekit.data.FieldBodiesElements
Get the general accumulated precession in longitude.
getPa() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the orbit argument of pericenter.
getPa() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the argument of perigee.
getPa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getPa() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the Argument of Perigee.
getPa() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Argument of Perigee.
getPaDot() - Method in class org.orekit.data.BodiesElements
Get the general accumulated precession in longitude time derivative.
getPaDot() - Method in class org.orekit.data.FieldBodiesElements
Get the general accumulated precession in longitude time derivative.
getParameterDerivatives(ParameterDriver) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the partial derivatives of the simulated measurement with respect to a parameter.
getParameterDriver(String) - Method in class org.orekit.forces.AbstractForceModel
Get parameter value from its name.
getParameterDriver(String) - Method in interface org.orekit.forces.ForceModel
Get parameter value from its name.
getParameterDriver(String) - Method in class org.orekit.forces.inertia.InertialForces
Get parameter value from its name.
getParameterDriver(String) - Method in class org.orekit.propagation.analytical.tle.TLE
Get parameter driver from its name.
getParameters() - Method in class org.orekit.files.ccsds.ndm.odm.UserDefined
Get all user defined parameters.
getParameters() - Method in interface org.orekit.forces.ForceModel
Get force model parameters.
getParameters(Field<T>) - Method in interface org.orekit.forces.ForceModel
Get force model parameters.
getParameters() - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel
Get ionospheric model parameters.
getParameters(Field<T>) - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel
Get ionospheric model parameters.
getParameters() - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel
Get tropospheric model parameters.
getParameters(Field<T>) - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel
Get tropospheric model parameters.
getParameters(FieldSpacecraftState<Gradient>) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter
Get the model parameters.
getParameters(Field<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get model parameters.
getParameters(Field<T>) - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get model parameters.
getParameters(FieldSpacecraftState<Gradient>, ParametersDriversProvider) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Get the parametric model parameters.
getParameters() - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Get the number of parameters.
getParameters() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Get force model parameters.
getParameters(Field<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Get force model parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the drivers for this measurement parameters, including its modifiers parameters.
getParametersDrivers() - Method in interface org.orekit.estimation.measurements.EstimationModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.gnss.WindUp
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.Bias
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesPhaseModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSPhaseModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaPhaseModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesPhaseModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSPhaseModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockPhaseModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeRateModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesPhaseModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSPhaseModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockPhaseModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TDOAIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TDOATroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the drivers for this measurement parameters, including its modifiers parameters.
getParametersDrivers() - Method in class org.orekit.forces.drag.DragForce
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.drag.TimeSpanDragForce
Get the drivers for parameters.
getParametersDrivers() - Method in interface org.orekit.forces.empirical.AccelerationModel
Get the drivers for acceleration model parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel
Get the drivers for acceleration model parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.ParametricAcceleration
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel
Get the drivers for acceleration model parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.DeSitterRelativity
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.LenseThirringRelativity
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.OceanTides
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.Relativity
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.SolidTides
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.inertia.InertialForces
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.Maneuver
 
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the propulsion model parameter drivers.
getParametersDrivers() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the propulsion model parameter drivers.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the propulsion model parameter drivers.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Get the maneuver triggers parameter drivers.
getParametersDrivers() - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Get the maneuver triggers parameter drivers.
getParametersDrivers() - Method in class org.orekit.forces.radiation.ECOM2
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter
Get the parameter drivers related to the analytical propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the drivers for TLE propagation SGP4 and SDP4.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the drivers for TLE propagation SGP4 and SDP4.
getParametersDrivers() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Get the drivers for parameters.
getParametersDrivers() - Method in interface org.orekit.utils.ParametersDriversProvider
Get the drivers for parameters.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester
Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.analytical.tle.TLEJacobiansMapper
Get the Jacobian with respect to parameters from a one-dimensional additional state array.
getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Get the Jacobian with respect to parameters from a one-dimensional additional state array.
getParametersJacobian(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester
Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get the Jacobian with respect to parameters from a one-dimensional additional state array.
getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
Get the Jacobian with respect to parameters from a one-dimensional additional state array.
getParent() - Method in class org.orekit.frames.Frame
Get the parent frame.
getParentShape() - Method in class org.orekit.frames.TopocentricFrame
Get the body shape on which the local point is defined.
getParsedEop() - Method in class org.orekit.files.sinex.SinexLoader
Get the parsed EOP data.
getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Get the behavior to adopt for handling parsed units.
getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get the behavior to adopt for handling parsed units.
getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Get the behavior to adopt for handling parsed units.
getParser(List<Integer>) - Method in enum org.orekit.gnss.metric.ntrip.Type
Get the message parser associated to the SSR type.
getParticipants() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the coordinates of the measurements participants in signal travel order.
getParticipants() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the participants.
getParts() - Method in interface org.orekit.errors.LocalizedException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitIllegalStateException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitInternalError
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitIOException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitParseException
Get the variable parts of the error message.
getPastInfinity() - Method in class org.orekit.time.AbstractTimeScales
 
getPastInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Dummy date at infinity in the past direction.
getPastInfinity() - Method in interface org.orekit.time.TimeScales
Dummy date at infinity in the past direction.
getPatchedSpacecraftState() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the list of patched spacecraft states.
getPatchPoint(int) - Method in class org.orekit.utils.AbstractMultipleShooting
Get a patch point.
getPath() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the path.
getPath1() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the path1.
getPath2() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the path2.
getPattern() - Method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
Get the message number.
getPattern() - Method in enum org.orekit.gnss.metric.parser.RtcmMessageType
Get the message number.
getPdop() - Method in class org.orekit.gnss.DOP
Gets the position dilution of precision.
getPendingEvent() - Method in class org.orekit.propagation.events.FieldEventState
Get PendingEvent.
getPerigeeArgument() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the perigee argument.
getPerigeeArgument() - Method in class org.orekit.orbits.KeplerianOrbit
Get the perigee argument.
getPerigeeArgument() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the argument of perigee.
getPerigeeArgument() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the argument of perigee.
getPerigeeArgumentDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the perigee argument derivative.
getPerigeeArgumentDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the perigee argument derivative.
getPermanentTide() - Method in enum org.orekit.utils.IERSConventions
Get the permanent tide to be removed from ΔC₂₀ when zero-tide potentials are used.
getPerturbationsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Get perturbations logical block.
getPhase(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide
Get the phase of the tide.
getPhaseBias() - Method in class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias
Get the phase bias associated to the signal ID.
getPhaseBias(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Get the phase bias for a given signal ID.
getPhaseBiases() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Get the phase biases for the current satellite.
getPhaseCenterVariation(Frequency, Vector3D) - Method in class org.orekit.gnss.antenna.Antenna
Get the value of the phase center variation in a signal direction.
getPhaseCenterVariation(Vector3D) - Method in class org.orekit.gnss.antenna.FrequencyPattern
Get the value of the phase center variation in a signal direction.
getPhaseMinusCodeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the phase minus code combination of measurements.
getPhaseShiftCorrections() - Method in class org.orekit.gnss.RinexObservationHeader
Get the list of phase shift correction used to generate phases consistent w/r to cycle shifts.
getPhysicalCovariances(double) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the covariances matrix in space flight dynamics physical units.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the "physical" estimated state (i.e.
getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the physical innovation covariance matrix.
getPhysicalInnovationCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the physical innovation covariance matrix.
getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the physical innovation covariance matrix.
getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the physical Kalman gain matrix.
getPhysicalKalmanGain() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the physical Kalman gain matrix.
getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the physical Kalman gain matrix.
getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the physical Jacobian of the measurement with respect to the state (H matrix).
getPhysicalMeasurementJacobian() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the physical Jacobian of the measurement with respect to the state (H matrix).
getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the physical Jacobian of the measurement with respect to the state (H matrix).
getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
getPhysicalStateTransitionMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
getPhysicBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Get physical properties logical block.
getPlaneSection(Vector3D, Vector3D) - Method in class org.orekit.bodies.Ellipsoid
Compute the 2D ellipse at the intersection of the 3D ellipsoid and a plane.
getPlus(int, int) - Method in class org.orekit.utils.LoveNumbers
Get the real part of a nominal Love numbers.
getPluto() - Method in interface org.orekit.bodies.CelestialBodies
Get the Pluto singleton body.
getPluto() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Pluto singleton body.
getPluto() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getPnm(int, int) - Method in class org.orekit.utils.FieldLegendrePolynomials
Return the coefficient Pnm.
getPnm(int, int) - Method in class org.orekit.utils.LegendrePolynomials
Return the coefficient Pnm.
getPoint() - Method in class org.orekit.frames.TopocentricFrame
Get the surface point defining the origin of the frame.
getPoint(Field<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the surface point defining the origin of the frame.
getPolarDriftXDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a polar drift along X.
getPolarDriftXDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a polar drift along X.
getPolarDriftYDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a polar drift along Y.
getPolarDriftYDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a polar drift along Y.
getPolarOffsetXDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a polar offset along X.
getPolarOffsetXDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a polar offset along X.
getPolarOffsetYDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a polar offset along Y.
getPolarOffsetYDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a polar offset along Y.
getPolarRadius() - Method in class org.orekit.models.earth.ReferenceEllipsoid
Get the radius of this ellipsoid at the poles.
getPole(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole
Get the body North pole direction in ICRF frame.
getPole(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole
Get the body North pole direction in ICRF frame.
getPoleCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the pole IERS Reference Pole correction.
getPoleCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the pole IERS Reference Pole correction.
getPolynomial() - Method in class org.orekit.data.PoissonSeries
Get the polynomial part of the series.
getPort() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the port number.
getPort() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Get the port to use for connection.
getPosition() - Method in class org.orekit.estimation.measurements.Position
Get the position.
getPosition() - Method in class org.orekit.estimation.measurements.PV
Get the position.
getPosition() - Method in class org.orekit.files.sinex.Station
Get the station position.
getPosition() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the position.
getPosition() - Method in class org.orekit.utils.PVCoordinates
Gets the position.
getPositionAngle() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the positionAngle.
getPositionAngle() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getPositionAngle() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getPositionAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector
Get the type of position angle.
getPositionAngleType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.StateMapper
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get propagation parameter type.
getPositionScale() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the position scale.
getPositionVector() - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Get object Position Vector.
getPotential(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Calculate spacecraft potential.
getPotential(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Calculate spacecraft potential.
getPrecessionFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing the precession angles.
getPrecessionFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the precession angles.
getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the predicted measurement.
getPredictedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the predicted measurement.
getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the predicted measurement.
getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Get the predicted spacecraft states.
getPredictedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the predicted spacecraft states.
getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Get the predicted spacecraft states.
getPredictionProvider() - Method in class org.orekit.files.ilrs.CRDHeader
Get the prediction provider.
getPredictionType() - Method in class org.orekit.files.ilrs.CRDHeader
Get the prediction type (CPF or TLE).
getPressSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the pressure sensor manufacturer.
getPressSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the pressure sensor model.
getPressSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the pressure sensor serial number.
getPressure() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
Get the surface pressure.
getPressure() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Get the local pressure at the evaluation location.
getPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Returns the pressure at the station [hPa].
getPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
Get the atmospheric pressure of the station depending its position.
getPrevId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get identification of previous orbit determination.
getPreviousMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the creation date of previous message from a given originator.
getPreviousMessageID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the unique ID identifying previous message from a given originator.
getPreviousState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Get the state at previous grid point date.
getPreviousState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the state at previous grid point date.
getPrf() - Method in class org.orekit.files.ilrs.CPFHeader
Get the Pulse Repetition Frequency (PRF).
getPrimary() - Method in class org.orekit.bodies.CR3BPSystem
Get the primary CelestialBody.
getPrimaryObject() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Get the primaryObject, at the center of the proximity zone.
getPrimaryStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange
Get the primary ground station from which measurement is performed.
getPrimaryWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the primary wavelength.
getPrimeMeridianAngle(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole
Get the prime meridian angle.
getPrimeMeridianAngle(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole
Get the prime meridian angle.
getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a prime meridian rotation rate.
getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a prime meridian rotation rate.
getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a prime meridian rotation.
getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a prime meridian rotation.
getPrimeStation() - Method in class org.orekit.estimation.measurements.TDOA
Get the prime ground station, the one that gives the date of the measurement.
getPrmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the Unique identifier of Pointing Request Message linked to this Orbit Data Message.
getPRN() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the PRN number of the satellite.
getPRN() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the PRN number of the satellite.
getPRN() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the PRN number of the GNSS satellite.
getPRN() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Gets the PRN number of the SBAS satellite.
getPrnNumber() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get PRN number.
getPrnNumber() - Method in class org.orekit.gnss.CombinedObservationDataSet
Get PRN number.
getPrnNumber() - Method in class org.orekit.gnss.ObservationDataSet
Get PRN number.
getPRNNumbers() - Method in class org.orekit.gnss.SEMParser
Gets the PRN numbers of all the GPS almanacs read from the file.
getPRNNumbers() - Method in class org.orekit.gnss.YUMAParser
Gets the PRN numbers of all the GPS almanacs read from the file.
getProcessingSoftwares() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Get the processing softwares.
getProcessingSoftwareVersions() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Get the processing software versions.
getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in class org.orekit.estimation.sequential.ConstantProcessNoise
Get the process noise matrix between previous and current states.
getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider
Get the process noise matrix between previous and current states.
getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Get the process noise matrix between previous and current states.
getProductionEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the date component of the ephemeris production.
getProductionHour() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the hour of ephemeris production (UTC).
getProgDCBS() - Method in class org.orekit.gnss.AppliedDCBS
Get the program name used to apply DCBs.
getProgPCVS() - Method in class org.orekit.gnss.AppliedPCVS
Get the program name used to apply PCVs.
getProgramName() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the program name.
getProgramName() - Method in class org.orekit.gnss.navigation.RinexNavigation
Getter for the program name.
getPropagationParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the propagator parameters supported by this estimator.
getPropagationParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
Get the propagator parameters supported by this estimator.
getPropagationParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the drivers for the configurable propagation parameters.
getPropagationParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the drivers for the configurable propagation parameters.
getPropagationParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the propagationParametersEvolution.
getPropagationType() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Get the type of the orbit used for the propagation (mean or osculating).
getPropagationType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the propagation type.
getPropagator(ObservableSatellite) - Method in class org.orekit.estimation.measurements.generation.Generator
Get a registered propagator.
getPropagator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get the orbit propagator used to generate this trajectory.
getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
View this ephemeris segment as a propagator.
getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
View this ephemeris as a propagator, combining data from all segments.
getPropagator() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
View this ephemeris as a propagator, combining data from all segments.
getPropagator() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
 
getPropagator(FieldSpacecraftState<Gradient>, Gradient[]) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter
Get the converted analytical orbit propagator.
getPropagator() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the reference propagator.
getPropagatorIndex() - Method in class org.orekit.estimation.measurements.ObservableSatellite
Get the index of the propagator related to this satellite.
getPropagatorList() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the list of propagators.
getPropagatorParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the propagator parameters supported by this estimator.
getPropagators() - Method in class org.orekit.propagation.PropagatorsParallelizer
Get an unmodifiable list of the underlying mono-satellite propagators.
getPropulsionModel() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the propulsion model.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Get the spherical harmonics provider.
getProviders() - Method in class org.orekit.data.DataProvidersManager
Get an unmodifiable view of the list of supported providers.
getProximityAngle() - Method in class org.orekit.propagation.events.AngularSeparationDetector
Get the proximity angle (rad).
getProximityAngle() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Get the proximity angle (rad).
getProxy() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Get proxy.
getPulseEnergy() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the pulse energy.
getPulseInOutgoingSemiTrain() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the number of pulses in outgoing semi-train.
getPulseWidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Get the pulse width (FWHM in ps).
getPVCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Get the position/velocity coordinates contained in the OPM.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame
Get the PVCoordinates of the topocentric frame origin in the selected frame.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.FieldOrbit
Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.orbits.FieldOrbit
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit
Get the TimeStampedPVCoordinates in definition frame.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.Orbit
Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.orbits.Orbit
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.orbits.Orbit
Get the TimeStampedPVCoordinates in definition frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.AbstractPropagator
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.Ephemeris
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Get the extrapolated position and velocity from an initial TLE.
getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the extrapolated position and velocity from an initial TLE.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the TimeStampedFieldPVCoordinates in orbit definition frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.FieldSpacecraftState
Get the TimeStampedFieldPVCoordinates in given output frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.propagation.SpacecraftState
Get the TimeStampedPVCoordinates in orbit definition frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.SpacecraftState
Get the TimeStampedPVCoordinates in given output frame.
getPVCoordinates() - Method in class org.orekit.utils.AbsolutePVCoordinates
Get the TimeStampedPVCoordinates.
getPVCoordinates(Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates
Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates
 
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get the TimeStampedFieldPVCoordinates.
getPVCoordinates(Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get the TimeStampedFieldPVCoordinates in a specified frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
 
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.FieldPVCoordinatesProvider
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider
Get the PVCoordinates of the body in the selected frame.
getPVCoordinatesProvider() - Method in class org.orekit.propagation.events.AlignmentDetector
Get the body to align.
getPvProvider() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get PV coordinates provider.
getPvProvider() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get PV coordinates provider.
getPVTarget() - Method in class org.orekit.propagation.events.FieldOfViewDetector
Get the position/velocity provider of the target .
getPZ9011(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getPZ9011(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the PZ-90.11 (Parametry Zemly – 1990.11) reference frame.
getPZ9011(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the PZ-90.11 (Parametry Zemly – 1990.11) reference frame.
getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the x component of inclination vector.
getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the x component of inclination vector.
getQns() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get the value of Qns coefficients.
getQns() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get the value of Qns coefficients.
getQualityIndicator() - Method in class org.orekit.files.ilrs.CRDHeader
Get the data quality indicator.
getQuantumEfficiency() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the quantum efficiency at applicable wavelength.
getQuaternion() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Get the quaternion.
getQuaternionBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the quaternion logical block.
getQuaternionDot() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Get the quaternion derivative.
getQZSS() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getQZSS() - Method in interface org.orekit.time.TimeScales
Get the Quasi-Zenith Satellite System time scale.
getQZSS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Quasi-Zenith Satellite System time scale.
getQzssCodeOnL2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Get the QZSS code on L2 Channel.
getQzssEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getQzssEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for QZSS weeks: 1980-01-06T00:00:00 QZSS time.
getQzssFitInterval() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Get the QZSS fit interval.
getQzssNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Get the QZSS navigation message corresponding to the current RTCM data.
getQzssNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Get the QZSS navigation message corresponding to the current RTCM data.
getQZSSNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation
Get all the QZSS navigation messages contained in the file.
getQZSSNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Get the QZSS navigation messages for the given satellite Id.
getQzssToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Get the QZSS time of clock.
getRaan() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Get the orbit right ascension of ascending node.
getRaan() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get Right Ascension of the Ascending node.
getRaan() - Method in class org.orekit.propagation.analytical.tle.TLE
Get Right Ascension of the Ascending node.
getRadiationParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention
Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention
Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in interface org.orekit.forces.radiation.RadiationSensitive
Get the drivers for supported parameters.
getRange(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the range of a point with regards to the topocentric frame center point.
getRange(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the range of a point with regards to the topocentric frame center point.
getRange1() - Method in class org.orekit.estimation.iod.IodGooding
Get the range for observation (1).
getRange2() - Method in class org.orekit.estimation.iod.IodGooding
Get the range for observation (2).
getRange3() - Method in class org.orekit.estimation.iod.IodGooding
Get the range for observation (3).
getRangeData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Get the range data for the data block.
getRangeMode() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the rangeMode.
getRangeModulus(RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the range modulus in meters.
getRangeRate(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the range rate of a point with regards to the topocentric frame center point.
getRangeRate(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the range rate of a point with regards to the topocentric frame center point.
getRangeType() - Method in class org.orekit.files.ilrs.CRDHeader
Get the range type.
getRangeType(int) - Static method in enum org.orekit.files.ilrs.CRDHeader.RangeType
Get the range type for the given indicator.
getRangeUnits() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the rangeUnits.
getRangeUnitsConverter() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Get the converter for Range Units.
getRate() - Method in class org.orekit.gnss.metric.ntrip.StreamedMessage
Get refresh rate.
getRate(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide
Get the angular rate of the tide.
getRatio() - Method in enum org.orekit.gnss.Frequency
Get the ratio f/f0, where f0 is the common frequency.
getRatio() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get the ratio of satellite period to central body rotation period.
getRatio() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get the ratio of satellite period to central body rotation period.
getRawCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics
Get a spherical harmonic cosine coefficient.
getRawContent() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the raw content of the entry.
getRawCorrectionRange() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the raw correction for range.
getRawDrivers() - Method in class org.orekit.utils.ParameterDriversList.DelegatingDriver
Get the raw drivers to which this one delegates.
getRawProvider() - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the underlying provider for raw (non-interpolated) transforms.
getRawProvider() - Method in class org.orekit.frames.ShiftingTransformProvider
Get the underlying provider for raw (non-interpolated) transforms.
getRawPV(AbsoluteDate) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider
Get the position-velocity at date.
getRawPV(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider
Get the position-velocity at date.
getRawRangeModulus() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the raw range modulus.
getRawSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics
Get a spherical harmonic sine coefficient.
getRbar() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the critical distance.
getRcs() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the typical (50th percentile) radar cross-section.
getRcvrClkOffset() - Method in class org.orekit.gnss.CombinedObservationDataSet
Get receiver clock offset.
getRcvrClkOffset() - Method in class org.orekit.gnss.ObservationDataSet
Get receiver clock offset.
getRdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the Unique identifier of Reentry Data Message linked to this Orbit Data Message.
getReal(int, int) - Method in class org.orekit.utils.LoveNumbers
Get the real part of a nominal Love numbers.
getRealAPV(AbsolutePVCoordinates, AbsoluteDate, Frame) - Method in class org.orekit.bodies.CR3BPSystem
Get the AbsolutePVCoordinates from normalized units to standard units in an output frame.
getReceiveBand() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the receiveBand.
getReceiveDelays() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for receiveDelays.
getReceiverIdentifier() - Method in class org.orekit.gnss.clock.RinexClock.Receiver
Getter for the receiver identifier.
getReceiverNumber() - Method in class org.orekit.gnss.RinexObservationHeader
Get the number of the receiver.
getReceivers() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the receivers.
getReceiversAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader
Get parsed receivers antennas.
getReceiverStation() - Method in class org.orekit.estimation.measurements.BistaticRange
 
getReceiverStation() - Method in class org.orekit.estimation.measurements.BistaticRangeRate
Get the receiver ground station.
getReceiverType() - Method in class org.orekit.gnss.RinexObservationHeader
Get the type of the receiver.
getReceiverVersion() - Method in class org.orekit.gnss.RinexObservationHeader
Get the version of the receiver.
getRecommendedOdSpan() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the recommended OD time span calculated for the object.
getRecommendedOdSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get time span of observation recommended for the OD of the object.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the type of record.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the type of record.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Get the type of record.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.Record
Get the type of record.
getReductionTheory() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get reduction theory used for precession and nutation modeling.
getReferenceAttitude() - Method in class org.orekit.attitudes.FixedRate
Get the reference attitude.
getReferenceClocks() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the reference clocks.
getReferenceDate() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get initial date.
getReferenceDate() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the reference date for the harmonics.
getReferenceDate() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the reference date for the harmonics.
getReferenceDate() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get reference date.
getReferenceDate() - Method in class org.orekit.propagation.integration.StateMapper
Get reference date.
getReferenceDate() - Method in class org.orekit.utils.ParameterDriver
Get current reference date.
getReferenceDate() - Method in class org.orekit.utils.SecularAndHarmonic
Get the reference date.
getReferenceFrame() - Method in class org.orekit.attitudes.Attitude
Get the reference frame.
getReferenceFrame() - Method in class org.orekit.attitudes.FieldAttitude
Get the reference frame.
getReferenceFrame() - Method in class org.orekit.estimation.measurements.AngularRaDec
Get the reference frame in which the right ascension - declination angles are given.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get the reference frame from which attitude is defined.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Get the reference frame.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Get the value of REF_FRAME as an Orekit Frame.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Get Coordinate system for velocity increment vector.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Get the the value of REFERENCE_FRAME as an Orekit Frame.
getReferenceFrame() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get the reference frame from which attitude is defined.
getReferenceFrame() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get the reference frame from which attitude is defined.
getReferenceName() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock
Getter for the name of the receiver/satellite embedding the reference clock.
getReferenceRadius() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Get the reference radius of the central body attraction model.
getReferenceRadius() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Get the reference radius of the central body attraction model.
getReferenceTrajectories() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Getter for the reference trajectories.
getReferenceValue() - Method in class org.orekit.utils.ParameterDriver
Get reference parameter value.
getRefFrame() - Method in class org.orekit.files.ccsds.definitions.ModifiedFrame
Get the CCSDS reference frame.
getRefFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the value of REF_FRAME as an Orekit Frame.
getRefFrame() - Method in class org.orekit.files.ilrs.CPFHeader
Get the reference frame.
getRefFrameId() - Method in class org.orekit.files.ilrs.CPFHeader
Get the reference frame identifier.
getRefFrameString() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Get Coordinate system for the torque vector, for absolute frames.
getReflectance() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the typical (50th percentile) coefficient of reflectance.
getRefraction(double) - Method in interface org.orekit.models.AtmosphericRefractionModel
Compute the refraction angle from the true (geometrical) elevation.
getRefraction(double) - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
 
getRefraction(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
 
getRefractionModel() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured refraction model.
getRefractionModel() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured refraction model.
getRegistrationAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Get the web or mail address for registration.
getRelativeMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm
Get the file metadata.
getRelativeMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get the relative metadata following header, they are the common metadata for the CDM.
getRelativePosition() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the Object2’s position vector relative to Object1's at TCA in RTN frame, getX for R component, getY for T component, getZ for N component.
getRelativeSpeed() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the norm of relative velocity vector at TCA.
getRelativeVelocity() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the Object2’s velocity vector relative to Object1's at TCA in RTN frame, getX for R component, getY for T component, getZ for N component.
getRemainingDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the total ΔV remaining for spacecraft.
getResidualsAccepted() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the percentage of residuals accepted in the OD of the object (from 0 to 100).
getResults() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Get on all the results computed by the detector (e.g.: dates of cycle-slip).
getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the retrograde factor.
getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the retrograde factor.
getRevAtEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Get the revolution rumber.
getReversedProvider(TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils
Reverse a transform provider.
getRevolutionNumberAtEpoch() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the revolution number.
getRevolutionNumberAtEpoch() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the revolution number.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.CircularOrbit
Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.KeplerianOrbit
Get the right ascension of the ascending node.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.CircularOrbit
Get the right ascension of the ascending node derivative.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the right ascension of the ascending node derivative.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the right ascension of the ascending node derivative.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the right ascension of the ascending node derivative.
getRinexVersion() - Method in class org.orekit.gnss.RinexObservationHeader
Get Rinex Version.
getRMS() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the Root Mean Square Deviation of the fitting.
getRnml(double, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Rεn,m,l(γ).
getRnml(T, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Rεn,m,l(γ).
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get roa = R / a.
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get roa = R / a.
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get roa = R / a.
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get roa = R / a.
getRolloverReference() - Static method in class org.orekit.time.GNSSDate
Get the reference date ensuring continuity across GNSS week rollover.
getRoot() - Static method in class org.orekit.frames.Frame
Get the unique root frame.
getRotatingFrame() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP Rotating Frame.
getRotation() - Method in class org.orekit.attitudes.Attitude
Get the attitude rotation.
getRotation() - Method in class org.orekit.attitudes.FieldAttitude
Get the attitude rotation.
getRotation() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary rotation.
getRotation() - Method in interface org.orekit.frames.StaticTransform
Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.frames.Transform
Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation.
getRotation() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the rotation.
getRotationAcceleration() - Method in class org.orekit.attitudes.Attitude
Get the satellite rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.attitudes.FieldAttitude
Get the satellite rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.frames.FieldTransform
Get the second time derivative of the rotation.
getRotationAcceleration() - Method in class org.orekit.frames.Transform
Get the second time derivative of the rotation.
getRotationAcceleration() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the rotation acceleration.
getRotationalAngleType() - Method in class org.orekit.files.ilrs.CPFHeader
Get the rotation angle type.
getRotationAngles() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Get the coordinates of the Euler angles (rad).
getRotationRate() - Method in class org.orekit.frames.FieldTransform
Get the first time derivative of the rotation.
getRotationRate() - Method in class org.orekit.frames.Transform
Get the first time derivative of the rotation.
getRotationRate() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation rate.
getRotationRate() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the rotation rate.
getRotationRates() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Get the rates of the Euler angles (rad/s).
getRTNCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Get the covariance matrix logical block.
getRTNCovarianceMatrix() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Get the RTN covariance matrix.
getS() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
Get s.
getS10(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the EUV index (26-34 nm) scaled to F10.
getS10() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the EUV index (26-34 nm) scaled to F10.
getS10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the EUV index (26-34 nm) scaled to F10.
getS10B(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the EUV 81-day averaged centered index.
getS10B() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the EUV 81-day averaged centered index.
getS10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the EUV 81-day averaged centered index.
getSample() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the states sample.
getSatConfiguration() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Gets the satellite configuration.
getSatelliteCode() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get satellite code.
getSatelliteCount() - Method in class org.orekit.files.sp3.SP3
Get the number of satellites contained in this orbit file.
getSatelliteID() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
Get the satellite ID.
getSatelliteID() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData
Get the satellite ID.
getSatelliteId(SatelliteSystem, int) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
Transform the satellite ID parsed from the IGS SSR message to the real ID.
getSatelliteName() - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
Get the satellite name.
getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get the satellite id.
getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the satellite id.
getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the number of satellite revolutions to use for converting osculating to mean elements.
getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get the number of satellite revolutions to use for converting osculating to mean elements.
getSatellites() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the satellites related to this measurement.
getSatellites() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the satellites related to this measurement.
getSatellites() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the satellites related to this measurement.
getSatellites() - Method in class org.orekit.files.ccsds.ndm.adm.aem.Aem
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.ccsds.ndm.odm.oem.Oem
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in interface org.orekit.files.general.AttitudeEphemerisFile
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in interface org.orekit.files.general.EphemerisFile
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.general.OrekitEphemerisFile
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.ilrs.CPF
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.sp3.SP3
 
getSatellites() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the satellites.
getSatellitesAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader
Get parsed satellites antennas.
getSatelliteSystem() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get satellite system.
getSatelliteSystem() - Method in class org.orekit.gnss.AppliedDCBS
Get the satellite system.
getSatelliteSystem() - Method in class org.orekit.gnss.AppliedPCVS
Get the satellite system.
getSatelliteSystem() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the satellite system.
getSatelliteSystem() - Method in class org.orekit.gnss.CombinedObservationDataSet
Get Satellite System.
getSatelliteSystem() - Method in enum org.orekit.gnss.Frequency
Get the satellite system for which this frequency is defined.
getSatelliteSystem() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmMessage
Get the satellite system associated to the message.
getSatelliteSystem() - Method in class org.orekit.gnss.navigation.RinexNavigation
Getter for the satellite system.
getSatelliteSystem() - Method in class org.orekit.gnss.ObservationDataSet
Get Satellite System.
getSatelliteSystem() - Method in class org.orekit.gnss.RinexObservationHeader
Get Satellite System.
getSatelliteSystem() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.PhaseShiftCorrection
Get the Satellite System.
getSatelliteSystem() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.ScaleFactorCorrection
Get the Satellite System.
getSatelliteType() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get satellite type.
getSatsCorrected() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.PhaseShiftCorrection
Get the list of satellites involved.
getSaturn() - Method in interface org.orekit.bodies.CelestialBodies
Get the Saturn singleton body.
getSaturn() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Saturn singleton body.
getSaturn() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getSBASNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation
Get all the SBAS navigation messages contained in the file.
getSBASNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Get the SBAS navigation messages for the given satellite Id.
getSBASOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Get the underlying SBAS orbital elements.
getScale() - Method in class org.orekit.utils.ParameterDriver
Get scale.
getScale() - Method in class org.orekit.utils.units.PowerTerm
Get the scaling factor.
getScale() - Method in class org.orekit.utils.units.Unit
Get the scaling factor to SI units.
getScaleFactor() - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockModifier
Get the scale factor used to compute relativistic effect.
getSclkOffsetAtEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the spacecraft clock count at OcmMetadata.getEpochT0().
getSclkSecPerSISec() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the number of spacecraft clock seconds occurring during one SI second.
getScreenEntryTime() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the time in UTC when Object2 enters the screening volume.
getScreenExitTime() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the time in UTC when Object2 exits the screening volume.
getScreenVolumeFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the name of the Object1 centered reference frame in which the screening volume data are given.
getScreenVolumeShape() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the shape of the screening volume.
getScreenVolumeX() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the R or T (depending on if RTN or TVN is selected) component size of the screening volume in the corresponding frame.
getScreenVolumeY() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the T or V (depending on if RTN or TVN is selected) component size of the screening volume in the corresponding frame.
getScreenVolumeZ() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the N component size of the screening volume in the corresponding frame.
getSecInDay() - Method in class org.orekit.time.GLONASSDate
Get the number of seconds since Na start.
getSecond() - Method in class org.orekit.time.TimeComponents
Get the seconds number.
getSecondary() - Method in class org.orekit.bodies.CR3BPSystem
Get the secondary CelestialBody.
getSecondary() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
Get the provider for the secondary satellite.
getSecondaryObject() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Get the secondaryObject.
getSecondaryStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange
Get the secondary ground station reflecting the signal.
getSecondFrequencyPhaseHistory() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter
Get the history of phase values of the second frequency.
getSecondsInLocalDay() - Method in class org.orekit.time.TimeComponents
Get the second number within the local day, without applying the offset from UTC.
getSecondsInUTCDay() - Method in class org.orekit.time.TimeComponents
Get the second number within the UTC day, applying the offset from UTC.
getSecondsOfWeek() - Method in class org.orekit.files.sp3.SP3
Returns the seconds of the GPS week as contained in the SP3 file.
getSecondStation() - Method in class org.orekit.estimation.measurements.TDOA
Get the second ground station, the one that gives the measurement.
getSedr() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the amount of energy being removed from the object’s orbit by atmospheric drag.
getSegments() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
Get the segments of the attitude ephemeris.
getSegments() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
Get the segments.
getSegments() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
Get the segments of the ephemeris.
getSegments() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
Get the segments of the ephemeris.
getSegments() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
Get the segments of the attitude ephemeris.
getSegments() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the segments of the ephemeris.
getSegments() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Get the segments of the attitude ephemeris.
getSegments() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Get the segments of the ephemeris.
getSegments() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Returns a list containing only this.
getSegments() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
Returns a list containing only this.
getSelectedCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the selected short periodic coefficients that must be stored as additional states.
getSelectedCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get the selected short periodic coefficients that must be stored as additional states.
getSelectedMu() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
Select the gravitational coefficient to use.
getSelectedNormalizedParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the current value of selected normalized parameters.
getSelectedNormalizedParameters() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the current value of selected normalized parameters.
getSelectedOrbitalParametersDriversForBuilder(int) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Get the selected orbital drivers for a propagatorBuilder.
getSelectedParameters() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Get the selected parameters, in Jacobian matrix column order.
getSelectedParameters() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Deprecated.
Get the selected parameters, in Jacobian matrix column order.
getSelectedPropagationDriversForBuilder(int) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Get the selected propagation drivers for a propagatorBuilder.
getSelector() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler
Get the dates selector.
getSensors() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get description of sensors used.
getSensorsN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get number of sensors used.
getSequenceNumber() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the ephemeris sequence number.
getSerialNumber() - Method in class org.orekit.gnss.antenna.ReceiverAntenna
Get the serial number.
getShadowBodies() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get celestial bodies casting shadows.
getShadowModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get shadow model used for solar radiation pressure.
getShortPeriodTerms() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the short periodic terms.
getShortPeriodTermsValue(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the short period terms value.
getSic() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the SIC ID.
getSigma() - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
Get the current value of sigma.
getSignalCode() - Method in enum org.orekit.gnss.ObservationType
Get the signal code.
getSignalID() - Method in class org.orekit.gnss.metric.messages.ssr.igm.CodeBias
Get the GNSS signal and tracking mode identifier.
getSignalID() - Method in class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias
Get the GNSS signal and tracking mode identifier.
getSignalStrength() - Method in class org.orekit.gnss.ObservationData
Get the signal strength.
getSignalStrengthUnit() - Method in class org.orekit.gnss.RinexObservationHeader
Get the unit of the carrier to noise ratio observables.
getSignalWideLaneIntegerIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias
Get the signal Wide-Lane integer indicator.
getSij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldFourierCjSjCoefficients
Get the coefficient Sij.
getSij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FourierCjSjCoefficients
Get the coefficient Sij.
getSinexCode() - Method in class org.orekit.gnss.antenna.Antenna
Get the sinex code of the antenna.
getSingularPoints() - Method in class org.orekit.models.earth.tessellation.AlongTrackAiming
Get points at which aiming direction cannot be computed.
getSingularPoints() - Method in class org.orekit.models.earth.tessellation.ConstantAzimuthAiming
Get points at which aiming direction cannot be computed.
getSingularPoints() - Method in class org.orekit.models.earth.tessellation.DivertedSingularityAiming
Get points at which aiming direction cannot be computed.
getSingularPoints() - Method in interface org.orekit.models.earth.tessellation.TileAiming
Get points at which aiming direction cannot be computed.
getSisa() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Getter for the signal in space accuracy (m).
getSiteCode() - Method in class org.orekit.files.sinex.Station
Get the site code (station identifier).
getSiteLocation() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the site location.
getSiteName() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the site name.
getSites() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Get the list of sites for which we have found coefficients, in lexicographic order ignoring case.
getSize() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the size of the problem.
getSize() - Method in class org.orekit.utils.LoveNumbers
Get the size of the arrays.
getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the Sj coefficient.
getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the Sj coefficient.
getSlope() - Method in class org.orekit.time.OffsetModel
Offset slope in seconds per UTC day (TAI minus UTC / dUTC).
getSlots() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of slots in use.
getSlotsEvictions() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of slots evictions.
getSma() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the semi-major axis.
getSma() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Semi-Major Axis.
getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the semi-major axis.
getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the semi-major axis.
getSmoothedData() - Method in class org.orekit.estimation.measurements.filtering.SmoothedObservationDataSet
Get the smoothed observation data.
getSnm() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Get the sine parameters of spherical harmonics expansion of degree N and order M.
getSnr() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement
Get the signal to noise ratio.
getSoftwareId() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Get the software configuration ID.
getSoftwareRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the software configuration record.
getSolarRadArea() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Get the solar radiation pressure area.
getSolarRadCoeff() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Get the solar radiation pressure coefficient.
getSolarRadiationPressure() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Get boolean that indicates if Solar Radiation Pressure is taken into account or not.
getSolarSystemBarycenter() - Method in interface org.orekit.bodies.CelestialBodies
Get the solar system barycenter aggregated body.
getSolarSystemBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the solar system barycenter aggregated body.
getSolarSystemBarycenter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getSolidPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing solid pole tide (ΔC₂₁, ΔS₂₁).
getSolidTidesModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get solid tides model.
getSolution() - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution
Get the solution array.
getSolutionsSize() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the number of solutions found.
getSolveN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get number of solved-for states.
getSolveStates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get description of state elements solved-for.
getSource() - Method in class org.orekit.files.ilrs.CPFHeader
Get the ephemeris source.
getSource() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Gets the source of this GPS almanac.
getSource() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
Gets the source of this QZSS almanac.
getSourceDCBS() - Method in class org.orekit.gnss.AppliedDCBS
Get the source of corrections.
getSourceIdentifier() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Get the source identifier.
getSourceIdentifier() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Get the source identifier.
getSourcePCVS() - Method in class org.orekit.gnss.AppliedPCVS
Get the source of corrections.
getSourceString() - Method in enum org.orekit.errors.OrekitMessages
getSourceTable() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Get a sourcetable.
getSouth() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the south of point, expressed in parent shape frame.
getSouth() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the south of point, expressed in parent shape frame.
getSouth() - Method in class org.orekit.frames.TopocentricFrame
Get the south direction of topocentric frame, expressed in parent shape frame.
getSouthAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the amplitude along South axis.
getSouthPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the phase along South axis.
getSpacecraft() - Method in class org.orekit.forces.drag.DragForce
Get spacecraft that are sensitive to atmospheric drag forces.
getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get spacecraft shape.
getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get spacecraft shape.
getSpacecraftBodyFrame() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Get the spacecraft body frame.
getSpacecraftClockAndDriftApplied() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the spacecraft clock offset and drift applied indicator.
getSpacecraftEpochTimeScale() - Method in class org.orekit.files.ilrs.CRDHeader
Get the spacecraft epoch time scale.
getSpacecraftParametersBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the spacecraft parameters logical block.
getSpacecraftParametersBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Get the spacecraft parameters logical block.
getSpacecraftParametersBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get the spacecraft parameters logical block.
getSpaceWeatherEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get epoch of the Space Weather data.
getSpaceWeatherSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get Space Weather data source.
getSpan(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Get the time span containing a specified date.
getSpanAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the TimeSpanMap.Span valid after transition.
getSpanBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the TimeSpanMap.Span valid before transition.
getSpansNumber() - Method in class org.orekit.utils.TimeSpanMap
Get the number of spans.
getSpatialFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the spatial filter.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.adm.AdmParser
Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.NdmParser
Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Get the non-default token builders for special XML elements.
getSpecifier() - Method in interface org.orekit.errors.LocalizedException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitIllegalStateException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitInternalError
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitIOException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitParseException
Get the localizable specifier of the error message.
getSpectralFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the spectral filter.
getSphericalHarmonicsDegree() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Get the degree of spherical harmonic expansion.
getSphericalHarmonicsOrder() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Get the order of spherical harmonic expansion.
getSpin() - Method in class org.orekit.attitudes.Attitude
Get the satellite spin.
getSpin() - Method in class org.orekit.attitudes.FieldAttitude
Get the satellite spin.
getSpin() - Method in class org.orekit.models.earth.ReferenceEllipsoid
Gets the rotation of the ellipsoid about its axis.
getSpinAlpha() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the right ascension of spin axis vector (rad).
getSpinAngle() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the phase of the satellite about the spin axis (rad).
getSpinAngleVel() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the angular velocity of satellite around spin axis (rad/s).
getSpinDelta() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Get the declination of the spin axis vector (rad).
getSpinStabilizedBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get the spin-stabilized logical block.
getSquaredDistance() - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution
Get the squared distance to the corresponding float solution.
getSrpCoefficient() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the nominal SRP coefficient.
getSrpConstantArea() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the attitude-independent SRP area, not already into attitude-dependent area along OEB.
getSrpModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Get Solar Radiation Pressure model.
getSrpUncertainty() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the SRP coefficient 1σ uncertainty.
getSsrEpoch1s() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Get the SSR Epoch Time 1s.
getSsrIgm01Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01
Get the SSR IGM01 data parsed in the SSR message.
getSsrIgm02Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02
Get the SSR IGM02 data parsed in the SSR message.
getSsrIgm03Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03
Get the SSR IGM03 data parsed in the SSR message.
getSsrIgm04Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04
Get the SSR IGM04 data parsed in the SSR message.
getSsrIgm05Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05
Get the SSR IGM05 data parsed in the SSR message.
getSsrIgm06Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06
Get the SSR IGM06 data parsed in the SSR message.
getSsrIgm07Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07
Get the SSR IGM07 data parsed in the SSR message.
getSsrMultipleMessageIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Get the SSR Multiple Message Indicator.
getSsrProviderId() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Get the SSR Provider ID.
getSsrSolutionId() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Get the SSR Solution ID.
getSsrUpdateInterval() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Get the SSR Update Interval.
getSsrUra() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data
Get the SSR User Range Accuracy (URA).
getStandardModel(double) - Static method in class org.orekit.models.earth.troposphere.MariniMurrayModel
Create a new Marini-Murray model using a standard atmosphere model.
getStandardModel(double) - Static method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Create a new Mendes-Pavlis model using a standard atmosphere model.
getStandardModel() - Static method in class org.orekit.models.earth.troposphere.SaastamoinenModel
Create a new Saastamoinen model using a standard atmosphere model.
getStart() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the start of the measurements time span.
getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get the start date of this ephemeris segment.
getStart() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get the start date of this ephemeris segment.
getStart() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
Get the start date of the ephemeris.
getStart() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the start date of this ephemeris segment.
getStart() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
 
getStart() - Method in class org.orekit.time.OffsetModel
Get the date of the offset start.
getStart() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the start of this time span.
getStartDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the start date.
getStartDate() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Get the start date.
getStartDate() - Method in class org.orekit.frames.EOPHistory
Get the date of the first available Earth Orientation Parameters.
getStartDate() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock
Getter for the validity period start date.
getStartDate() - Method in class org.orekit.propagation.AbstractPropagator
Get the start date.
getStartDate() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the start date.
getStartDetector() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Getter for the firing start detector.
getStartDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Get the driver for start date.
getStartDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Get the driver for start date.
getStartEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the starting epoch (UTC).
getStartFiringDetector() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Getter for the start firing detector.
getStartScreenPeriod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the start time in UTC of the screening period for the conjunction assessment.
getStartTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get start of total time span covered by attitude data.
getStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the time of the earliest data contained in the OCM.
getStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Get start of total time span covered by ephemerides data and covariance data.
getStartTime() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the startTime.
getStartTransition() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the transition at start of this time span.
getState() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter
Get the state with the number of parameters consistent with the propagation model.
getState() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the triggering state.
getState() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
Get the triggering state.
getState() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event
Get the spacecraft's state at the event.
getState() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
Get the spacecraft's state at the event.
getState(ParametersDriversProvider) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Get the state with the number of parameters consistent with parametric model.
getStateDerivatives(int) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the partial derivatives of the simulated measurement with respect to state Cartesian coordinates.
getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.analytical.tle.TLEJacobiansMapper
Get the Jacobian with respect to state from a one-dimensional additional state array.
getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Get the Jacobian with respect to state from a one-dimensional additional state array.
getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get the Jacobian with respect to state from a one-dimensional additional state array.
getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
Get the Jacobian with respect to state from a one-dimensional additional state array.
getStates() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the states of the spacecrafts.
getStateSize() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get state size.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester
Extract state transition matrix from state.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Extract state transition matrix from state.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Extract state transition matrix from state.
getStateTransitionMatrix(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester
Extract state transition matrix from state.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Method returning the State Transition Matrix.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Extract state transition matrix from state.
getStateType() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Get the type of the elements used to define the orbital state (mean or osculating).
getStateVectorBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Get the state vector logical block.
getStateVectorBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get the state vector logical block.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation
Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter
 
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.L1TransformProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.ShiftingTransformProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider
Get a transform for only rotations and translations on the specified date.
getStaticTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame
Get the static portion of the transform from the instance to another frame.
getStation() - Method in class org.orekit.estimation.measurements.AngularAzEl
Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.AngularRaDec
Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.gnss.Phase
Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.Range
Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.RangeRate
Get the ground station from which measurement is performed.
getStation(String) - Method in class org.orekit.files.sinex.SinexLoader
Get the station corresponding to the given site code.
getStationClockAndDriftApplied() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the station clock offset and drift applied indicator.
getStationIdentifier() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the station identifier.
getStationName() - Method in class org.orekit.files.ilrs.CRDHeader
Get the station name from official list.
getStationName() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the station name.
getStationNetword() - Method in class org.orekit.files.ilrs.CRDHeader
Get the station network.
getStationOscDrift() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the estimated station oscillator drift in parts in 10¹⁵.
getStations() - Method in class org.orekit.files.sinex.SinexLoader
Get the parsed station data.
getStationUTCOffset() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the estimated station UTC offset.
getStatus() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the status.
getStep() - Method in class org.orekit.files.ilrs.CPFHeader
Get the time between table entries.
getStep() - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the grid points time step.
getStep() - Method in class org.orekit.frames.ShiftingTransformProvider
Get the grid points time step.
getStmName() - Method in class org.orekit.propagation.AbstractMatricesHarvester
Get the State Transition Matrix state name.
getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Get the end date of this ephemeris segment.
getStop() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
Get the end date of this ephemeris segment.
getStop() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
Get the end date of the ephemeris.
getStop() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the end date of this ephemeris segment.
getStop() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
 
getStopDate() - Method in class org.orekit.propagation.events.EventState.EventOccurrence
Get the new time for a stop action.
getStopDate() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence
Get the new time for a stop action.
getStopDetector() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Getter for the firing stop detector.
getStopDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Get the driver for stop date.
getStopDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Get the driver for stop date.
getStopFiringDetector() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Getter for the stop firing detector.
getStopScreenPeriod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the stop time in UTC of the screening period for the conjunction assessment.
getStopTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get end of total time span covered by attitude data.
getStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the time of the latest data contained in the OCM.
getStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Get end of total time span covered by ephemerides data and covariance data.
getStopTime() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the stopTime.
getStream(T) - Method in class org.orekit.data.AbstractListCrawler
Get the stream to read from an input.
getStream(File) - Method in class org.orekit.data.FilesListCrawler
Get the stream to read from an input.
getStream(URL) - Method in class org.orekit.data.NetworkCrawler
Get the stream to read from an input.
getStreamInfoAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Get the web address for stream information.
getStrengthLevel() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the strength level for activity.
getStuffReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Get the stuff (all the things needed for, the detector).
getSubDailySequenceNumber() - Method in class org.orekit.files.ilrs.CPFHeader
Get the sub-daily ephemeris sequence number.
getSun() - Method in interface org.orekit.bodies.CelestialBodies
Get the Sun singleton body.
getSun() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Sun singleton body.
getSun() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getSun() - Method in class org.orekit.forces.gravity.DeSitterRelativity
Get the sun model used to compute De Sitter effect.
getSunEarthCR3BP(AbsoluteDate, TimeScale) - Static method in class org.orekit.bodies.CR3BPFactory
Get the Sun-Earth CR3BP singleton bodies pair.
getSunJupiterCR3BP(AbsoluteDate, TimeScale) - Static method in class org.orekit.bodies.CR3BPFactory
Get the Sun-Jupiter CR3BP singleton bodies pair.
getSupportedNames() - Method in class org.orekit.data.AbstractSelfFeedingLoader
Get the supported names regular expression.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.gnss.SEMParser
 
getSupportedNames() - Method in class org.orekit.gnss.YUMAParser
 
getSupportedNames() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
 
getSupportedNames() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
 
getSupportedNames() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
 
getSupportedNames() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
 
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
Getter for the user SV accuray (meters).
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
Getter for the user SV accuray (meters).
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
Getter for the user SV accuray (meters).
getSvHealth() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Get the satellite health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Getter for the SV health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
Getter for the satellite health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Getter for the satellite health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
Getter for the satellite health status.
getSVN() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Gets the satellite "SVN" reference number.
getSystem(CelestialBody, CelestialBody, double) - Static method in class org.orekit.bodies.CR3BPFactory
Get the corresponding CR3BP System.
getSystemId() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
Get the system configuration ID.
getSystemIdentifier() - Method in class org.orekit.files.ilrs.CRDHeader
Get the system identifier.
getSystemNumber() - Method in class org.orekit.files.ilrs.CRDHeader
Get the system number.
getSystemObservationTypes() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the different observation type for each satellite system.
getSystemOccupancy() - Method in class org.orekit.files.ilrs.CRDHeader
Get the system occupancy.
getSystemRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the system configuration record.
getTabDensity() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the current density table.
getTable() - Method in class org.orekit.attitudes.TabulatedLofOffset
Get an unmodifiable view of the tabulated attitudes.
getTAI() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTAI() - Method in interface org.orekit.time.TimeScales
Get the International Atomic Time scale.
getTAI() - Static method in class org.orekit.time.TimeScalesFactory
Get the International Atomic Time scale.
getTaimutcT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the difference (TAI – UTC) in seconds at epoch OcmMetadata.getEpochT0().
getTargetClass() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the target class.
getTargetLocation() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the target location.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.NadirPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.NadirPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TargetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TargetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the target point position/velocity in specified frame.
getTargetSize() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the size of the target.
getTauC() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS time scale correction to UTC time.
getTauGps() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the correction to GPS time relative to GLONASS time.
getTauMultiplier() - Method in class org.orekit.models.earth.displacement.Tide
Get the multiplier for the τ Doodson argument.
getTC() - Method in class org.orekit.data.DelaunayArguments
Get the offset in Julian centuries.
getTC() - Method in class org.orekit.data.FieldDelaunayArguments
Get the offset in Julian centuries.
getTca() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the date and time in UTC of the closest approach.
getTCB() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTCB() - Method in interface org.orekit.time.TimeScales
Get the Barycentric Coordinate Time scale.
getTCB() - Static method in class org.orekit.time.TimeScalesFactory
Get the Barycentric Coordinate Time scale.
getTCG() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTCG() - Method in interface org.orekit.time.TimeScales
Get the Geocentric Coordinate Time scale.
getTCG() - Static method in class org.orekit.time.TimeScalesFactory
Get the Geocentric Coordinate Time scale.
getTDB() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTDB() - Method in interface org.orekit.time.TimeScales
Get the Barycentric Dynamic Time scale.
getTDB() - Static method in class org.orekit.time.TimeScalesFactory
Get the Barycentric Dynamic Time scale.
getTdim() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP orbital period of m2 around m1.
getTdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the Unique identifier of Tracking Data Message linked to this Orbit Data Message.
getTdop() - Method in class org.orekit.gnss.DOP
Gets the time dilution of precision.
getTEC(AbsoluteDate, GeodeticPoint) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
Computes the Total Electron Content (TEC) at a given date by performing a temporal interpolation with the two closest date in the IONEX file.
getTEC(FieldAbsoluteDate<T>, GeodeticPoint) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
Computes the Total Electron Content (TEC) at a given date by performing a temporal interpolation with the two closest date in the IONEX file.
getTechAddress() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the address of Technical Point Of Contact at originator.
getTechEmail() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the email address of Technical Point Of Contact at originator.
getTechOrg() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the creating agency or operator.
getTechPhone() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the phone number of Technical Point Of Contact at originator.
getTechPOC() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the Technical Point Of Contact at originator.
getTechPosition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the position of Technical Point Of Contact at originator.
getTEME() - Method in class org.orekit.frames.AbstractFrames
 
getTEME() - Method in interface org.orekit.frames.Frames
Get the TEME reference frame.
getTEME() - Static method in class org.orekit.frames.FramesFactory
Get the TEME reference frame.
getTemperature() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
Get the surface temperature.
getTemperature() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Get the local temperature at the evaluation location.
getTemperature() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Returns the temperature at the station [K].
getTemperature() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
Get the atmospheric temperature of the station depending its position.
getTemplateTLE() - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
Getter for the template TLE.
getTempSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the temperature sensor manufacturer.
getTempSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the temperature sensor model.
getTempSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Get the temperature sensor serial number.
getTFirstObs() - Method in class org.orekit.gnss.RinexObservationHeader
Get the time of First observation record.
getTGD() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
Gets the estimated group delay differential TGD for L1-L2 correction.
getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Gets for the Group Delay Differential (s).
getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
Getter for the Group Delay Differential (s).
getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Getter for the estimated group delay differential TGD for L5-S correction.
getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
Getter for the Group Delay Differential (s).
getTGD1() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
Getter for the estimated group delay differential TGD1 for B1I signal.
getTGD2() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
Getter for the estimated group delay differential TGD for B2I signal.
getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the theoretical standard deviation.
getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the theoretical standard deviation.
getTheoreticalStandardDeviation() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the theoretical standard deviation.
getTheta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
Get Central body rotation angle θ.
getTheta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
Get Central body rotation angle θ.
getTheta0() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
Get the station elevation angle under free-space propagation .
getThetaMin() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
Get the station minimal elevation angle.
getThreeHourlyAp() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the array of the eight three-hourly Ap indices for the current entry.
getThreeHourlyAp(int) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the three-hourly Ap index at index i from the threeHourlyAp array.
getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the 3 hours geomagnetic index.
getThreeHourlyKp() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the array of the eight three-hourly Kp indices for the current entry.
getThreeHourlyKp(int) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the three-hourly Kp index at index i from the threeHourlyKp array.
getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the 3 hours geomagnetic index.
getThreeHourlyKP(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Get the value of the 3 hours geomagnetic index.
getThreshold() - Method in class org.orekit.propagation.events.AbstractDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.AdapterDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in interface org.orekit.propagation.events.EventDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in interface org.orekit.propagation.events.FieldEventDetector
Get the convergence threshold in the event time search.
getThrust() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get thrust.
getThrust() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Get the thrust.
getThrust() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the thrust.
getThrust() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust value (N).
getThrust(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the thrust norm (N).
getThrustAcceleration() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Get the object’s acceleration due to in-track thrust used to propagate the state vector and covariance to TCA.
getThrustDirectionProvider() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Getter on Thrust direction and spaceraft attitude provided by an external object.
getThrustDirectionSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get one σ angular off-nominal thrust direction.
getThrustEfficiency() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get thrust efficiency η.
getThrusterAxisInSatelliteFrame() - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Thruster axis in satellite frame.
getThrustInterpolation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get interpolation mode between current and next thrust line.
getThrustIsp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get thrust specific impulse.
getThrustMagnitudeSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Get one σ percent error on thrust magnitude.
getThrustVector() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the thrust vector (N) in S/C frame.
getThrustVector(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getTidalDisplacementFrequencyCorrectionDiurnal() - Method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for diurnal tides.
getTidalDisplacementFrequencyCorrectionDiurnal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for diurnal tides.
getTidalDisplacementFrequencyCorrectionZonal() - Method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for zonal tides.
getTidalDisplacementFrequencyCorrectionZonal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for zonal tides.
getTide(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the tide.
getTideFrequencyDependenceFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).
getTideFrequencyDependenceFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).
getTideSystem() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the TideSystem used in the gravity field.
getTideSystem() - Method in interface org.orekit.forces.gravity.potential.TideSystemProvider
Get the TideSystem used in the gravity field.
getTime() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the reference time of the GNSS orbit as a duration from week start.
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
 
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Get the Reference Time.
getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the Reference Time.
getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Reference Time of the GNSS orbit as a duration from week start.
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Gets the Reference Time of the SBAS orbit in GPS seconds of the week.
getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Gets the Reference Time of the SBAS orbit in GPS seconds of the week.
getTime() - Method in class org.orekit.time.DateTimeComponents
Get the time component.
getTime() - Method in class org.orekit.utils.units.Unit
Get the time exponent.
getTimeConverter() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Get the current time converter.
getTimeConverter() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Get the current time converter.
getTimeLastObsEnd() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the start of a time interval (UTC) that contains the time of the last accepted observation.
getTimeLastObsStart() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the start of a time interval (UTC) that contains the time of the last accepted observation.
getTimeOfFlight() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement
Get the time-of-flight.
getTimeOffset() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the time offset from first state date to measurement date.
getTimer() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Get the timer name.
getTimerSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Get the timer serial number.
getTimeScale() - Method in class org.orekit.files.ccsds.definitions.TimeConverter
Get the base time scale.
getTimeScale() - Method in class org.orekit.files.ilrs.CPF
Get the time scale used in CPF file.
getTimeScale() - Method in class org.orekit.files.ilrs.CRDParser
Get the time scale used to read the file.
getTimeScale() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the data time scale.
getTimeScale(TimeScales) - Method in enum org.orekit.gnss.TimeSystem
Get the time scale corresponding to time system.
getTimeScales() - Method in class org.orekit.data.CompositeDataContext
 
getTimeScales() - Method in interface org.orekit.data.DataContext
Get a factory for constructing TimeScales based on the auxiliary data in this context.
getTimeScales() - Method in class org.orekit.data.ExceptionalDataContext
 
getTimeScales() - Method in class org.orekit.data.LazyLoadedDataContext
 
getTimeScales() - Method in class org.orekit.frames.AbstractFrames
Get the time scales.
getTimeScales() - Method in class org.orekit.frames.EOPHistory
Get the time scales used in computing EOP corrections.
getTimeScales() - Static method in class org.orekit.time.TimeScalesFactory
Get the instance of TimeScales that is called by all of the static methods in this class.
getTimeSinceFirstObservation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get time elapsed between first accepted observation on epoch.
getTimeSinceLastObservation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get time elapsed between last accepted observation on epoch.
getTimeSource() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Get the time source.
getTimeSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the span of time in seconds that the OCM covers.
getTimeSystem() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Get the Time System that: for CDM, is used for relative metadata, metadata, OD parameters, state vector.
getTimeSystem() - Method in class org.orekit.files.ccsds.section.Metadata
Get the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.
getTimeSystem() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get the time system.
getTimeSystem() - Method in class org.orekit.files.sp3.SP3
Returns the TimeSystem used to time-stamp position entries.
getTimeSystem() - Method in class org.orekit.gnss.clock.RinexClock
Getter for the file time system.
getTimeSystemCorrectionA0() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection
Getter for the A0 coefficient of the time system correction.
getTimeSystemCorrectionA1() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection
Getter for the A1 coefficient of the time system correction.
getTimeSystemCorrections() - Method in class org.orekit.gnss.navigation.RinexNavigation
Getter for the time system corrections contained in the file header.
getTimeSystemCorrectionSecOfWeek() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection
Getter for the reference time of the time system correction polynomial.
getTimeSystemCorrectionType() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection
Getter for the time system correction type.
getTimeSystemCorrectionWeekNumber() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection
Getter for the reference week number of the time system correction polynomial.
getTimetagRef() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the timetagRef.
getTimingRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the timing system configuration record.
getTIRF(IERSConventions) - Method in class org.orekit.frames.AbstractFrames
 
getTIRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getTIRF(IERSConventions) - Method in interface org.orekit.frames.Frames
Get the TIRF reference frame, ignoring tidal effects.
getTIRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the TIRF reference frame.
getTIRF(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the TIRF reference frame, ignoring tidal effects.
getTIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TIRF reference frame.
getTk() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the time referenced to the beginning of the frame within the current day.
getTLastObs() - Method in class org.orekit.gnss.RinexObservationHeader
Get the time of last observation record.
getTLE() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Get the underlying TLE.
getTLE() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the underlying TLE.
getTLEBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Get the TLE logical block.
getTN() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Get the correction to the satellite time relative to GLONASS system time.
getTN() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the correction to the satellite time relative to GLONASS system time.
getTo() - Method in class org.orekit.utils.units.UnitsConverter
Get the destination unit.
getToc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
Gets the clock correction reference time toc.
getToc() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Gets the clock correction reference time toc.
getTOD(boolean) - Method in class org.orekit.frames.AbstractFrames
 
getTOD(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getTOD(boolean) - Method in interface org.orekit.frames.Frames
Get the TOD reference frame.
getTOD(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the TOD reference frame.
getTOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TOD reference frame.
getTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TOD reference frame.
getTon2a() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
Get ton2a = 2 / (n² * a).
getTon2a() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
Get ton2a = 2 / (n² * a).
getTool() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade
Get the tool used for OD.
getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured topocentric frame definitions.
getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Returns the topocentric frame centered on ground point.
getTopocentricFrame() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured topocentric frame definitions.
getTorque() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Get the torque vector (N.m).
getTotalEclipse() - Method in class org.orekit.propagation.events.EclipseDetector
Get the total eclipse detection flag.
getTotalEclipse() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the total eclipse detection flag.
getTotalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the total intensity of the magnetic field (= norm of the field vector).
getTotalLightingRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the total lighting ratio ([0-1]).
getTotalLightingRatio(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the total lighting ratio ([0-1]).
getTotalNumberOfDataLines() - Method in class org.orekit.gnss.clock.RinexClock
Get the total number of complete data lines in the file.
getTrackId() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the tracking data identifier.
getTrackingSoftwares() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Get the tracking softwares.
getTrackingSoftwareVersions() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Get the tracking software versions.
getTracksAvailable() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the number of sensor tracks available for the OD of the object.
getTracksAvailable() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get number of sensors tracks available for the OD within the actual OD span.
getTracksUsed() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the number of sensor tracks used for the OD of the object.
getTracksUsed() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get number of sensors tracks accepted for the OD within the actual OD span.
getTrajBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get basis of this trajectory state time history data.
getTrajBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get identification number of the orbit determination or simulation upon which this trajectory is based.
getTrajectoryStates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
Get the trajectory states.
getTrajFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get epoch of the trajectory reference frame.
getTrajID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get trajectory identification number.
getTrajNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get identification number of next trajectory.
getTrajPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get identification number of previous trajectory.
getTrajReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get reference frame of the trajectory.
getTrajType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get trajectory element set type.
getTrajUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get trajectory element set units.
getTransform(AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<Gradient>, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the transform with derivatives.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.EclipticProvider
 
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EclipticProvider
 
getTransform(AbsoluteDate) - Method in class org.orekit.frames.FixedTransformProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.FixedTransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider
Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.HelmertTransformation
Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter
Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.L1TransformProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.L1TransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.ShiftingTransformProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ShiftingTransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in interface org.orekit.frames.TransformProvider
Get the FieldTransform corresponding to specified date.
getTransformation() - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Get the underlying HelmertTransformation.
getTransformation(TimeScale) - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Get the underlying HelmertTransformation.
getTransformProvider() - Method in class org.orekit.frames.Frame
Get the provider for transform from parent frame to instance.
getTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame
Get the transform from the instance to another frame.
getTransformTo(Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.Frame
Get the transform from the instance to another frame.
getTransitions() - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
as of 11.1, replaced by TimeSpanDragForce.getFirstSpan()
getTransitions() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Deprecated.
getTransitions() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
getTransitions() - Method in class org.orekit.utils.FieldTimeSpanMap
Get an unmodifiable view of the sorted transitions.
getTransitions() - Method in class org.orekit.utils.TimeSpanMap
getTranslation() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary translation.
getTranslation() - Method in interface org.orekit.frames.StaticTransform
Get the underlying elementary translation.
getTranslation() - Method in class org.orekit.frames.Transform
Get the underlying elementary translation.
getTransmissionOfSpectralFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Get the percentage of transmission of spectral filter.
getTransmitBand() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the transmitBand.
getTransmitDelays() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the transmitDelays.
getTranspClkRef() - Method in class org.orekit.files.ilrs.CPFHeader
Get the transponder Clock Reference Time.
getTranspClkRefTime() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the transponder clock reference time.
getTransponderId() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the transponder configuration ID.
getTransponderRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
Get the transponder configuration record.
getTranspOscDrift() - Method in class org.orekit.files.ilrs.CPFHeader
Get the transponder Oscillator Drift in parts in 10^15.
getTranspOscDrift() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the estimated transponder oscillator drift in parts in 10¹⁵.
getTranspTransmitDelay() - Method in class org.orekit.files.ilrs.CPFHeader
Get the transponder transmit delay.
getTranspUtcOffset() - Method in class org.orekit.files.ilrs.CPFHeader
Get the transponder UTC offset.
getTranspUTCOffset() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the estimated transponder UTC offset.
getTrigger() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the triggering event.
getTriggeredEnd() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Getter for the triggered date of engine stop.
getTriggeredIncreasing() - Method in enum org.orekit.propagation.events.FilterType
Get the increasing status of triggered events.
getTriggeredStart() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Getter triggered date of engine start.
getTropoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier
Get the tropospheric delay model.
getTropoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier
Get the tropospheric delay model.
getTroposphericModel(AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Get the EstimatedTroposphericModel model valid at a date.
getTrueAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true anomaly.
getTrueAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true anomaly.
getTrueAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true anomaly derivative.
getTrueAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true anomaly derivative.
getTT() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTT() - Method in interface org.orekit.time.TimeScales
Get the Terrestrial Time scale.
getTT() - Static method in class org.orekit.time.TimeScalesFactory
Get the Terrestrial Time scale.
getTurnaroundDenominator() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the turnaroundDenominator.
getTurnaroundNumerator() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Getter for the turnaroundNumerator.
getTypAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.
getType() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade
Get the method type.
getType() - Method in class org.orekit.files.ccsds.definitions.PocMethodFacade
Get the method type.
getType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Covariance
Get the type of the elements.
getType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
Get the type of the elements.
getType() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation
Get the type of observation.
getType() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the type of the token.
getType() - Method in class org.orekit.files.sp3.SP3
Returns the SP3.SP3FileType associated with this SP3 file.
getType() - Method in class org.orekit.gnss.antenna.Antenna
Get the type of the antenna.
getType() - Method in class org.orekit.orbits.CartesianOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.CircularOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.KeplerianOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.Orbit
Get the orbit type.
getTypeCode() - Method in class org.orekit.gnss.metric.messages.ParsedMessage
Get the code for the message type.
getTypeObs() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.PhaseShiftCorrection
Get the Carrier Phase Observation Code.
getTypesObsScaled() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.ScaleFactorCorrection
Get the list of Observation Types scaled.
getU() - Method in class org.orekit.bodies.Ellipse
Get the unit vector along the major axis.
getU1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients
Get the coefficient U₁j for Fourier index i.
getU1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients
Get the coefficient U₁j for Fourier index i.
getU2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients
Get the coefficient U₂j for Fourier index = 1 (i == 0).
getU2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients
Get the coefficient U₂j for Fourier index = 1 (i == 0).
getUnderlyingAttitudeProvider() - Method in interface org.orekit.attitudes.AttitudeProviderModifier
Get the underlying attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.SpinStabilized
Get the underlying attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawCompensation
Get the underlying (ground pointing) attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawSteering
Get the underlying (ground pointing) attitude provider.
getUndulation(double, double, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
Gets the Undulation of the Geoid, N at the given position.
getUnit() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Get the field unit.
getUnits() - Method in enum org.orekit.files.ccsds.definitions.ElementsType
Get the elements units.
getUnits() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Get the units.
getUnits(String) - Method in class org.orekit.utils.units.UnitsCache
Get units from a string specification.
getUnnormalizationFactors(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get a un-normalization factors array.
getUnnormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics
Get a spherical harmonic cosine coefficient.
getUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the gravity field coefficients provider from the first supported file.
getUnnormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Create a time-independent UnnormalizedSphericalHarmonicsProvider from canonical coefficients.
getUnnormalizedProvider(NormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
getUnnormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get a gravity field unnormalized coefficients provider.
getUnnormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get a gravity field unnormalized coefficients provider.
getUnnormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics
Get a spherical harmonic sine coefficient.
getUpperCaseAbbreviation() - Method in enum org.orekit.time.Month
Get the upper case three letters abbreviation.
getUpperCaseName() - Method in enum org.orekit.time.Month
Get the upper case full name.
getURA() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Gets the average URA number.
getURA() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Getter for the user range accuray (meters).
getURA() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Getter for the user range accuray (meters).
getUranus() - Method in interface org.orekit.bodies.CelestialBodies
Get the Uranus singleton body.
getUranus() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Uranus singleton body.
getUranus() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get start of useable time span covered by attitude data.
getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Get start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get end of useable time span covered by ephemerides data.
getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Get end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Get end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUsedObservationData() - Method in class org.orekit.gnss.CombinedObservationData
Get the list of observation data used to perform the combination of measurements.
getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Get user defined parameters logical block.
getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Get the user defined parameters logical block.
getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get the user defined parameters logical block.
getUT1(EOPHistory) - Method in class org.orekit.time.AbstractTimeScales
Get the Universal Time 1 scale.
getUT1(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
 
getUT1(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
 
getUT1(EOPHistory) - Method in class org.orekit.time.LazyLoadedTimeScales
Get the Universal Time 1 scale.
getUT1(IERSConventions, boolean) - Method in interface org.orekit.time.TimeScales
Get the Universal Time 1 scale.
getUT1(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time 1 scale.
getUT1(EOPHistory) - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time 1 scale.
getUt1MinusUtc() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the UT1-UTC offset.
getUT1MinusUTC() - Method in class org.orekit.frames.EOPEntry
Get the UT1-UTC value.
getUT1MinusUTC(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the UT1-UTC value.
getUT1MinusUTC(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the UT1-UTC value.
getUt1mutcT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Get the difference (UT1 – UTC) in seconds at epoch OcmMetadata.getEpochT0().
getUtc() - Method in class org.orekit.frames.AbstractEopLoader
Get the UTC time scale.
getUtc() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the UTC time scale used to create this TLE.
getUTC() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getUTC() - Method in interface org.orekit.time.TimeScales
Get the Universal Time Coordinate scale.
getUTC() - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time Coordinate scale.
getUTCScale() - Method in class org.orekit.time.UT1Scale
Get the associated UTC scale.
getUTCTAIOffsets() - Method in class org.orekit.time.UTCScale
Returns the UTC-TAI offsets underlying this UTC scale.
getV() - Method in class org.orekit.bodies.Ellipse
Get the unit vector along the minor axis.
getV1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients
Get the coefficient V₁j for Fourier index i.
getV1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients
Get the coefficient V₁j for Fourier index i.
getV2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients
Get the coefficient V₂j for Fourier index = 1 (i == 0).
getV2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients
Get the coefficient V₂j for Fourier index = 1 (i == 0).
getValidFrom() - Method in class org.orekit.files.sinex.Station
Get start of validity.
getValidFrom() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get start of validity.
getValidityStart() - Method in class org.orekit.time.UTCTAIOffset
Get the start time of validity for this offset.
getValidUntil() - Method in class org.orekit.files.sinex.Station
Get end of validity.
getValidUntil() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get end of validity.
getValue() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
getValue() - Method in class org.orekit.gnss.CombinedObservationData
Get the combined observed value.
getValue() - Method in class org.orekit.gnss.ObservationData
Get the observed value.
getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction
Get Γ function value.
getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Get Γ function value.
getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear
Compute the value of the Hansen coefficient Kj-n-1, s.
getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear
Compute the value of the Hansen coefficient K₀n, s.
getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
Get the K₀-n-1,s coefficient value.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Compute the value of the Hansen coefficient Kj-n-1, s.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the value of the Hansen coefficient K₀n, s.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Get the K₀-n-1,s coefficient value.
getValue(int, int, int, Gradient) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials
Returns the value and derivatives of the Jacobi polynomial Plv,w evaluated at γ.
getValue(int, int, int, FieldGradient<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials
Returns the value and derivatives of the Jacobi polynomial Plv,w evaluated at γ.
getValue(int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.NewcombOperators
Get the Newcomb operator evaluated at n, s, ρ, σ.
getValue() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
Get the value.
getValue() - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Get the value.
getValue() - Method in class org.orekit.utils.ParameterDriver
Get current parameter value.
getValue(int, Map<String, Integer>) - Method in class org.orekit.utils.ParameterDriver
Get the value as a gradient.
getValuesSamples() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the values samples for the interpolation function.
getVdim() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP orbital velocity of m2.
getVdop() - Method in class org.orekit.gnss.DOP
Gets the vertical dilution of precision.
getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector f.
getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get equinoctial frame vector f.
getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector g.
getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get equinoctial frame vector g.
getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector w.
getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get equinoctial frame vector w.
getVeis1950() - Method in class org.orekit.frames.AbstractFrames
 
getVeis1950() - Method in interface org.orekit.frames.Frames
Get the VEIS 1950 reference frame.
getVeis1950() - Static method in class org.orekit.frames.FramesFactory
Get the VEIS 1950 reference frame.
getVelocity() - Method in class org.orekit.estimation.measurements.PV
Get the velocity.
getVelocity() - Method in class org.orekit.files.sinex.Station
Get the station velocity.
getVelocity() - Method in class org.orekit.frames.FieldTransform
Get the first time derivative of the translation.
getVelocity() - Method in class org.orekit.frames.Transform
Get the first time derivative of the translation.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the inertial velocity of atmosphere molecules.
getVelocity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the inertial velocity of atmosphere molecules.
getVelocity() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the velocity.
getVelocity() - Method in class org.orekit.utils.PVCoordinates
Gets the velocity.
getVelocityVector() - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Get object Velocity Vector.
getVenus() - Method in interface org.orekit.bodies.CelestialBodies
Get the Venus singleton body.
getVenus() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Venus singleton body.
getVenus() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getVersion() - Method in class org.orekit.files.ilrs.ILRSHeader
Get the format version.
getVersion() - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration
Get ITRF version.
getVertices() - Method in class org.orekit.models.earth.tessellation.Tile
Get the four vertices.
getVmAbsolute() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the typical (50th percentile) visual magnitude.
getVmApparent() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the typical (50th percentile) apparent visual magnitude.
getVmApparentMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the maximum apparent visual magnitude.
getVmApparentMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the minimum apparent visual magnitude.
getVmns(int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Get the Vn,sm coefficient from Vn,s.
getVtecQualityIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
Get the VTEC quality indicator.
getWarmup() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
Get the value of warmup iterations.
getWaterVaporPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Returns the water vapor pressure at the station [hPa].
getWavelength() - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
Get the wavelength.
getWavelength() - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
Get the wavelength.
getWavelength() - Method in class org.orekit.estimation.measurements.gnss.Phase
Get the wavelength.
getWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
Get the transmit wavelength.
getWavelength() - Method in enum org.orekit.gnss.Frequency
Get the wavelength in meters.
getWaves() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the loaded waves.
getWeek() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Getter for the reference week of the GNSS orbit.
getWeek() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
Gets the Reference Week of the GNSS orbit.
getWeek() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Gets the Reference Week of the SBAS orbit.
getWeek() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Gets the Reference Week of the SBAS orbit.
getWeekNumber() - Method in class org.orekit.time.GNSSDate
Get the week number since the GNSS reference epoch.
getWeightedRMS() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Get the weighted Root Mean Square (RMS) of the residuals from a batch least squares OD.
getWeightedRms() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Get weighted RMS residual ratio.
getWest() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the west of point, expressed in parent shape frame.
getWest() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the west of point, expressed in parent shape frame.
getWest() - Method in class org.orekit.frames.TopocentricFrame
Get the west direction of topocentric frame, expressed in parent shape frame.
getWestAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the amplitude along west axis.
getWestPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the phase along West axis.
getWetMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the total mass at T₀.
getWgs84(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the WGS84 ellipsoid, attached to the given body frame.
getWideLaneCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Wide-Lane combination of measurements.
getWindUp(SatelliteSystem, int, String) - Method in class org.orekit.estimation.measurements.gnss.WindUpFactory
Get a modifier for a satellite/receiver pair.
getWMM(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the WMM model for the given year.
getWMM(double) - Method in interface org.orekit.models.earth.GeoMagneticFields
Get the WMM model for the given year.
getWMM(double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
 
getX() - Method in class org.orekit.frames.EOPEntry
Get the X component of the pole motion.
getX() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get the X axis defining FoV boundary.
getX() - Method in class org.orekit.gnss.clock.RinexClock.Receiver
Getter for the X coordinate in meters in considered Earth centered frame.
getX() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite X position.
getX() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getX() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the ECEF-X component of satellite coordinates in PZ-90 datum.
getX() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-X component of satellite coordinates.
getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getX2ON2A2XP1() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get (χ²) / (n² * a² * (χ + 1 ) ).
getX2ON2A2XP1() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get (χ²) / (n² * a² * (χ + 1 ) ).
getX3ON2A() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get χ³ / (n² * a).
getX3ON2A() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get χ³ / (n² * a).
getXDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite X velocity.
getXDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getXDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the ECEF-X component of satellite velocity vector in PZ-90 datum.
getXDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-X component of satellite velocity vector.
getXDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite X acceleration.
getXDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getXDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the GLONASS ECEF-X component of satellite acceleration vector in PZ-90 datum.
getXDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-X component of satellite acceleration vector.
getXM10(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the MG2 index scaled to F10.
getXM10() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the MG2 index scaled to F10.
getXM10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the MG2 index scaled to F10.
getXM10B(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the MG2 81-day average centered index.
getXM10B() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the MG2 81-day average centered index.
getXM10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the MG2 81-day average centered index.
getXON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get χ / (n² * a²).
getXON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get χ / (n² * a²).
getXp() - Method in class org.orekit.frames.FieldPoleCorrection
Get the xp parameter.
getXp() - Method in class org.orekit.frames.PoleCorrection
Get the xp parameter.
getXPo() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the X polar motion.
getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get Χ².
getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get Χ².
getXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
Get Χ³.
getXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
Get Χ³.
getXYSpXY2Function() - Method in enum org.orekit.utils.IERSConventions
Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.
getXYSpXY2Function(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.
getY() - Method in class org.orekit.frames.EOPEntry
Get the Y component of the pole motion.
getY() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get the Y axis defining FoV boundary.
getY() - Method in class org.orekit.gnss.clock.RinexClock.Receiver
Getter for the Y coordinate in meters in considered Earth centered frame.
getY() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite Y position.
getY() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getY() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the ECEF-Y component of satellite coordinates in PZ-90 datum.
getY() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-Y component of satellite coordinates.
getY10(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the Solar X-Ray & Lya index scaled to F10.
getY10() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the Solar X-Ray & Lya index scaled to F10.
getY10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the Solar X-Ray & Lya index scaled to F10.
getY10B(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Get the Solar X-Ray & Lya 81-day ave.
getY10B() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Get the Solar X-Ray & Lya 81-day ave.
getY10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the Solar X-Ray & Lya 81-day ave.
getYawAngle(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the yaw compensation angle at date.
getYawAngle(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the yaw compensation angle at date.
getYawAngle() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Get the yaw angle used for computation of phase wind-up correction.
getYawRate() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Get the yaw rate.
getYDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite Y velocity.
getYDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getYDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the ECEF-Y component of satellite velocity vector in PZ-90 datum.
getYDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-Y component of satellite velocity vector.
getYDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite Y acceleration.
getYDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getYDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the GLONASS ECEF-Y component of satellite acceleration vector in PZ-90 datum.
getYDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-Y component of satellite acceleration vector.
getYear() - Method in enum org.orekit.frames.ITRFVersion
Get the reference year of the frame version.
getYear() - Method in class org.orekit.time.DateComponents
Get the year number.
getYearOfCentury() - Method in class org.orekit.files.ilrs.CRDHeader
Get the year of century from CPF or TLE.
getYp() - Method in class org.orekit.frames.FieldPoleCorrection
Get the yp parameter.
getYp() - Method in class org.orekit.frames.PoleCorrection
Get the yp parameter.
getYPo() - Method in class org.orekit.files.sinex.SinexEopEntry
Get the Y polar motion.
getZ() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get the Z axis defining FoV boundary.
getZ() - Method in class org.orekit.gnss.clock.RinexClock.Receiver
Getter for the Z coordinate in meters in considered Earth centered frame.
getZ() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite Z position.
getZ() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getZ() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the ECEF-Z component of satellite coordinates in PZ-90 datum.
getZ() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-Z component of satellite coordinates.
getZDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite Z velocity.
getZDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getZDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the ECEF-Z component of satellite velocity vector in PZ-90 datum.
getZDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-Z component of satellite velocity vector.
getZDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Getter for the satellite Z acceleration.
getZDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
 
getZDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
Get the GLONASS ECEF-Z component of satellite acceleration vector in PZ-90 datum.
getZDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
Get the ECEF-Z component of satellite acceleration vector.
getZenith() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction above the point, expressed in parent shape frame.
getZenith() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction above the point, expressed in parent shape frame.
getZenith() - Method in class org.orekit.frames.TopocentricFrame
Get the zenith direction of topocentric frame, expressed in parent shape frame.
getZenithAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the amplitude along zenith axis.
getZenithDelay() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Returns the zenith delay array.
getZenithOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station position along Zenith axis.
getZenithPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the phase along zenith axis.
getZero(Field<T>) - Static method in class org.orekit.utils.FieldPVCoordinates
Get fixed position/velocity at origin (both p, v and a are zero vectors).
getZInverseTransformationReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get a reference to the Z inverse transformation matrix.
getZipJarCrawler(T) - Method in class org.orekit.data.AbstractListCrawler
Get a zip/jar crawler for an input.
getZipJarCrawler(File) - Method in class org.orekit.data.FilesListCrawler
Get a zip/jar crawler for an input.
getZipJarCrawler(URL) - Method in class org.orekit.data.NetworkCrawler
Get a zip/jar crawler for an input.
getZone() - Method in class org.orekit.geometry.fov.PolygonalFieldOfView
Get the interior zone.
getZone() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Get the geographic zone triggering the events.
getZone() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the geographic zone.
GHIJjsPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Gjs, Hjs, Ijs and Jjs polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
GHIJjsPolynomials(double, double, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Create a set of Gjs, Hjs, Ijs and Jjs polynomials.
GHmsjPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Gmsj and the Hmsj polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
GHmsjPolynomials(double, double, double, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Create a set of Gmsj and Hmsj polynomials.
GillIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for GillIntegrator.
GillIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.GillIntegratorBuilder
Build a new instance.
GlobalIonosphereMapModel - Class in org.orekit.models.earth.ionosphere
Global Ionosphere Map (GIM) model.
GlobalIonosphereMapModel(String) - Constructor for class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
Constructor with supported names given by user.
GlobalIonosphereMapModel(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
Constructor that uses user defined supported names and data context.
GlobalMappingFunctionModel - Class in org.orekit.models.earth.troposphere
The Global Mapping Function model for radio techniques.
GlobalMappingFunctionModel() - Constructor for class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
Build a new instance.
GlobalMappingFunctionModel(TimeScale) - Constructor for class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
Build a new instance.
GlobalPressureTemperature2Model - Class in org.orekit.models.earth.weather
The Global Pressure and Temperature 2 (GPT2) model.
GlobalPressureTemperature2Model(String, double, double, Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Constructor with supported names given by user.
GlobalPressureTemperature2Model(String, double, double, Geoid, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Constructor with supported names and source of GPT2 auxiliary data given by user.
GlobalPressureTemperature2Model(double, double, Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Constructor with default supported names.
GlobalPressureTemperatureModel - Class in org.orekit.models.earth.weather
The Global Pressure and Temperature model.
GlobalPressureTemperatureModel(double, double, Frame) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
Build a new instance.
GlobalPressureTemperatureModel(double, double, Frame, DataContext) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
Build a new instance.
Glonass - Class in org.orekit.gnss.attitude
Attitude providers for Glonass navigation satellites.
Glonass(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Glonass
Simple constructor.
GLONASS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for GLONASS four-year interval number: 1996-01-01T00:00:00 GLONASS time.
GLONASS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for GLONASS four-year interval number: 1996-01-01.
GLONASS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of the Earth's universal gravitational parameter for GLONASS user in m³/s².
GLONASS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of Pi for conversion from semicircles to radian.
GLONASSAlmanac - Class in org.orekit.propagation.analytical.gnss.data
This class holds a GLONASS almanac as read from .agl files.
GLONASSAlmanac(int, int, int, int, int, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Constructor.
GLONASSAlmanac(int, int, int, int, int, double, double, double, double, double, double, double, double, double, double, TimeScale) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
Constructor.
GLONASSAnalyticalPropagator - Class in org.orekit.propagation.analytical.gnss
This class aims at propagating a GLONASS orbit from GLONASSOrbitalElements.
GLONASSAnalyticalPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss
This nested class aims at building a GLONASSAnalyticalPropagator.
GLONASSAnalyticalPropagatorBuilder(GLONASSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Initializes the builder.
GLONASSAnalyticalPropagatorBuilder(GLONASSOrbitalElements, DataContext) - Constructor for class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Initializes the builder.
GLONASSDate - Class in org.orekit.time
Container for date in GLONASS form.
GLONASSDate(int, int, double) - Constructor for class org.orekit.time.GLONASSDate
Build an instance corresponding to a GLONASS date.
GLONASSDate(int, int, double, TimeScale) - Constructor for class org.orekit.time.GLONASSDate
Build an instance corresponding to a GLONASS date.
GLONASSDate(AbsoluteDate) - Constructor for class org.orekit.time.GLONASSDate
Build an instance from an absolute date.
GLONASSDate(AbsoluteDate, TimeScale) - Constructor for class org.orekit.time.GLONASSDate
Build an instance from an absolute date.
GLONASSEphemeris - Class in org.orekit.propagation.analytical.gnss.data
Class for GLONASS ephemeris used by the GLONASSNumericalPropagator.
GLONASSEphemeris(int, int, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
Build a new instance.
GLONASSEphemeris(int, int, double, double, double, double, double, double, double, double, double, double, AbsoluteDate) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
Build a new instance.
GLONASSNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a Glonass navigation message.
GLONASSNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Constructor.
GLONASSNumericalPropagator - Class in org.orekit.propagation.numerical
This class propagates GLONASS orbits using numerical integration.
GLONASSNumericalPropagator(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, Frame, AttitudeProvider, double, DataContext, boolean) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagator
Private constructor.
GLONASSNumericalPropagatorBuilder - Class in org.orekit.propagation.numerical
This nested class aims at building a GLONASSNumericalPropagator.
GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, boolean) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
Initializes the builder.
GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, boolean, DataContext) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
Initializes the builder.
GLONASSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data
This interface provides the minimal set of orbital elements needed by the GLONASSAnalyticalPropagator and the GLONASSNumericalPropagator.
GLONASSScale - Class in org.orekit.time
GLONASS time scale.
GlonassUserRangeAccuracy - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris.utils
Enumerate for GLONASS User Range Accuracy.
GlonassUserRangeAccuracy(int) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.GlonassUserRangeAccuracy
Simple constructor.
GMSTScale - Class in org.orekit.time
Greenwich Mean Sidereal Time.
GNSS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of Pi for conversion from semicircles to radians in GNSS.
GNSS_WEEK_IN_SECONDS - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Duration of the GNSS week in seconds.
GNSSAttitudeProvider - Interface in org.orekit.gnss.attitude
Attitude providers for navigation satellites.
GNSSClockElements - Interface in org.orekit.propagation.analytical.gnss.data
This interface provides the minimal set of orbital elements needed by the ClockCorrectionsProvider.
GNSSConstants - Interface in org.orekit.propagation.analytical.gnss.data
Set of useful physical constants used in Global Navigation Satellite Systems (GNSS).
GnssData - Class in org.orekit.gnss.metric.ntrip
GNSS data retrieved from Ntrip caster.
GnssData(byte[], int) - Constructor for class org.orekit.gnss.metric.ntrip.GnssData
Build a GNSS data bloc.
GNSSDate - Class in org.orekit.time
Container for date in GNSS form.
GNSSDate(int, double, SatelliteSystem) - Constructor for class org.orekit.time.GNSSDate
Build an instance corresponding to a GNSS date.
GNSSDate(int, double, SatelliteSystem, TimeScales) - Constructor for class org.orekit.time.GNSSDate
Build an instance corresponding to a GNSS date.
GNSSDate(AbsoluteDate, SatelliteSystem) - Constructor for class org.orekit.time.GNSSDate
Build an instance from an absolute date.
GNSSDate(AbsoluteDate, SatelliteSystem, TimeScales) - Constructor for class org.orekit.time.GNSSDate
Build an instance from an absolute date.
GNSSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data
This interface provides the minimal set of orbital elements needed by the GNSSPropagator.
GNSSPropagator - Class in org.orekit.propagation.analytical.gnss
Common handling of AbstractAnalyticalPropagator methods for GNSS propagators.
GNSSPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss
This nested class aims at building a GNSSPropagator.
GNSSPropagatorBuilder(GNSSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Initializes the builder.
GNSSPropagatorBuilder(GNSSOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Initializes the builder.
GPS_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of the earth's rotation rate in rad/s for GPS user.
GPS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
GPS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for GPS weeks: 1980-01-06.
GPS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
WGS 84 value of the Earth's universal gravitational parameter for GPS user in m³/s².
GPS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Number of weeks in the GPS cycle.
GPSAlmanac - Class in org.orekit.propagation.analytical.gnss.data
This class holds a GPS almanac as read from SEM or YUMA files.
GPSAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Constructor.
GPSBlockIIA - Class in org.orekit.gnss.attitude
Attitude providers for GPS block IIA navigation satellites.
GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIA
Simple constructor.
GPSBlockIIF - Class in org.orekit.gnss.attitude
Attitude providers for GPS block IIF navigation satellites.
GPSBlockIIF(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIF
Simple constructor.
GPSBlockIIR - Class in org.orekit.gnss.attitude
Attitude providers for GPS block IIR navigation satellites.
GPSBlockIIR(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIR
Simple constructor.
GPSNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a GPS navigation message.
GPSNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
Constructor.
GPSScale - Class in org.orekit.time
GPS time scale.
gradient(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the gradient of the non-central part of the gravity field.
gradient(FieldAbsoluteDate<T>, FieldVector3D<T>, T) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the gradient of the non-central part of the gravity field.
GraggBulirschStoerIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for GraggBulirschStoerIntegrator.
GraggBulirschStoerIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder
Build a new instance.
GRAM - Static variable in class org.orekit.utils.units.Unit
Gram unit.
GRAPHICCombination - Class in org.orekit.estimation.measurements.gnss
GRoup And Phase Ionospheric Calibration (GRAPHIC) combination.
GravityFieldFactory - Class in org.orekit.forces.gravity.potential
Factory used to read gravity field files in several supported formats.
GravityFields - Interface in org.orekit.forces.gravity.potential
Defines methods for obtaining gravity fields.
GRGS_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for GRGS files.
GRGSFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the GRGS gravity field format.
GRGSFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader
Simple constructor.
GRGSFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader
Simple constructor.
GRIM5C1_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from GRIM5C1 model: 7.292115e-5 rad/s.
GRIM5C1_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from GRIM5C1 model: -1.082626110612609e-3.
GRIM5C1_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from GRIM5C1 model: 2.536150841690056e-6.
GRIM5C1_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from GRIM5C1 model: 1.61936352497151e-6.
GRIM5C1_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from GRIM5C1 model: 2.231013736607540e-7.
GRIM5C1_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from GRIM5C1 model: -5.402895357302363e-7.
GRIM5C1_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from GRIM5C1 model: 6378136.46 m.
GRIM5C1_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from GRIM5C1 model: 1.0 / 298.25765.
GRIM5C1_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from GRIM5C1 model: 3.986004415e14 m³/s².
GroundAtNightDetector - Class in org.orekit.propagation.events
Detector for ground location being at night.
GroundAtNightDetector(TopocentricFrame, PVCoordinatesProvider, double, AtmosphericRefractionModel) - Constructor for class org.orekit.propagation.events.GroundAtNightDetector
Simple constructor.
GroundFieldOfViewDetector - Class in org.orekit.propagation.events
Finder for satellite entry/exit events with respect to a sensor Field Of View attached to an arbitrary frame.
GroundFieldOfViewDetector(Frame, FieldOfView) - Constructor for class org.orekit.propagation.events.GroundFieldOfViewDetector
Build a new instance.
GroundPointing - Class in org.orekit.attitudes
Base class for ground pointing attitude providers.
GroundPointing(Frame, Frame) - Constructor for class org.orekit.attitudes.GroundPointing
Default constructor.
GroundStation - Class in org.orekit.estimation.measurements
Class modeling a ground station that can perform some measurements.
GroundStation(TopocentricFrame) - Constructor for class org.orekit.estimation.measurements.GroundStation
Build a ground station ignoring station displacements.
GroundStation(TopocentricFrame, EOPHistory, StationDisplacement...) - Constructor for class org.orekit.estimation.measurements.GroundStation
Simple constructor.
GRS80_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from GRS80 model: 7.292115e-5 rad/s.
GRS80_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from GRS80 model: -1.08263e-3.
GRS80_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from GRS80 model: 6378137.0 m.
GRS80_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from GRS80 model: 1.0 / 298.257222101.
GRS80_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from GRS80 model: 3.986005e14 m³/s².
GTODProvider - Class in org.orekit.frames
Greenwich True Of Date Frame, also known as True of Date Rotating frame (TDR) or Greenwich Rotating Coordinate frame (GCR).
GTODProvider(IERSConventions, EOPHistory, TimeScales) - Constructor for class org.orekit.frames.GTODProvider
Simple constructor.
guessCenter(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CenterName
Guess the name of the center of the reference frame.
guessFrame(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
Guesses names from ODM Table 5-3 and Annex A.
GzipFilter - Class in org.orekit.data
Filter for gzip compressed data.
GzipFilter() - Constructor for class org.orekit.data.GzipFilter
 

H

H00 - Static variable in class org.orekit.time.TimeComponents
Constant for commonly used hour 00:00:00.
H12 - Static variable in class org.orekit.time.TimeComponents
Constant for commonly used hour 12:00:00.
H_X - Static variable in enum org.orekit.orbits.OrbitType
Name for inclination vector first component.
H_Y - Static variable in enum org.orekit.orbits.OrbitType
Name for inclination vector second component .
HaloOrbit - Class in org.orekit.orbits
Class calculating different parameters of a Halo Orbit.
HaloOrbit(CR3BPSystem, PVCoordinates, double) - Constructor for class org.orekit.orbits.HaloOrbit
Simple Constructor.
HaloOrbit(RichardsonExpansion, double, LibrationOrbitFamily) - Constructor for class org.orekit.orbits.HaloOrbit
Simple Constructor.
HaloXZPlaneCrossingDetector - Class in org.orekit.propagation.events
Detector for XZ Plane crossing.
HaloXZPlaneCrossingDetector(double, double) - Constructor for class org.orekit.propagation.events.HaloXZPlaneCrossingDetector
Simple Constructor.
handleStep(OrekitStepInterpolator) - Method in class org.orekit.estimation.sequential.EskfMeasurementHandler
Handle the current step.
handleStep(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter
Handle the current step.
handleStep(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter
Handle the current step.
handleStep(SpacecraftState) - Method in class org.orekit.files.ilrs.StreamingCpfWriter.Segment
Handle the current step.
handleStep(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler
Handle the current step.
handleStep(FieldOrekitStepInterpolator<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler
Handle the current step.
handleStep(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Handle the current step.
handleStep(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Handle the current step.
handleStep(List<OrekitStepInterpolator>) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler
Handle the current step.
handleStep(SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler
Handle the current step.
handleStep(OrekitStepInterpolator) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Handle the current step.
handleStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Handle the last accepted step.
handleStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Handle the current step.
HansenTesseralLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t!=0 and n < 0.
HansenTesseralLinear(int, int, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Constructor.
HansenThirdBodyLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n > 0.
HansenThirdBodyLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Constructor.
HansenUtilities - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Utilities class.
HansenZonalLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n < 0.
HansenZonalLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Constructor.
HarmonicAccelerationModel - Class in org.orekit.forces.empirical
Harmonic acceleration model.
HarmonicAccelerationModel(String, AbsoluteDate, double, int) - Constructor for class org.orekit.forces.empirical.HarmonicAccelerationModel
Simple constructor.
HarrisPriester - Class in org.orekit.models.earth.atmosphere
This atmosphere model is the realization of the Modified Harris-Priester model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester
Simple constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester
Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][]) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester
Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][], double) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester
Constructor for Modified Harris-Priester atmosphere model.
hasAcceleration() - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
Check if state contains acceleration data.
hasAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState
Check if an additional state is available.
hasAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState
Check if an additional state is available.
hasAdditionalStateDerivative(String) - Method in class org.orekit.propagation.FieldSpacecraftState
Check if an additional state derivative is available.
hasAdditionalStateDerivative(String) - Method in class org.orekit.propagation.SpacecraftState
Check if an additional state derivative is available.
hasDataFor(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Check if the cache has data for the given date using EOPHistory.getStartDate() and EOPHistory.getEndDate().
hasDerivatives() - Method in class org.orekit.orbits.CartesianOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldCartesianOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldCircularOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.Orbit
Check if orbit includes derivatives.
hasDopplerCountRollover() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Check if there is a Doppler count rollover.
hashCode() - Method in class org.orekit.bodies.FieldGeodeticPoint
 
hashCode() - Method in class org.orekit.bodies.GeodeticPoint
 
hashCode() - Method in class org.orekit.models.earth.displacement.Tide
 
hashCode() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get a hashcode for this tle.
hashCode() - Method in class org.orekit.propagation.analytical.tle.TLE
Get a hashcode for this tle.
hashCode() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
hashCode() - Method in class org.orekit.time.AbsoluteDate
Get a hashcode for this date.
hashCode() - Method in class org.orekit.time.DateComponents
hashCode() - Method in class org.orekit.time.DateTimeComponents
hashCode() - Method in class org.orekit.time.FieldAbsoluteDate
Get a hashcode for this date.
hashCode() - Method in class org.orekit.time.TimeComponents
hashCode() - Method in class org.orekit.utils.units.Unit
Get a hashcode for this unit.
hasManeuvers() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Get boolean testing whether the APM contains at least one maneuver.
hasManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
check whether the OPM contains at least one maneuver.
hasManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Get boolean testing whether the APM contains at least one maneuver.
hasNonKeplerianAcceleration(FieldPVCoordinates<T>, T) - Static method in class org.orekit.orbits.FieldOrbit
Check if Cartesian coordinates include non-Keplerian acceleration.
hasNonKeplerianAcceleration(PVCoordinates, double) - Static method in class org.orekit.orbits.Orbit
Check if Cartesian coordinates include non-Keplerian acceleration.
hasRates() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Check if the logical block includes rates.
hasRates() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Check if the logical block includes rates.
HatanakaCompressFilter - Class in org.orekit.gnss
Decompression filter for Hatanaka compressed RINEX files.
HatanakaCompressFilter() - Constructor for class org.orekit.gnss.HatanakaCompressFilter
 
Header - Class in org.orekit.files.ccsds.section
Header of a CCSDS Navigation Data Message.
Header(double) - Constructor for class org.orekit.files.ccsds.section.Header
Constructor.
HeaderKey - Enum in org.orekit.files.ccsds.section
Keywords allowed in Header.
HeaderProcessingState - Class in org.orekit.files.ccsds.section
HeaderProcessingState(AbstractConstituentParser<?, ?>) - Constructor for class org.orekit.files.ccsds.section.HeaderProcessingState
Simple constructor.
HECTO_PASCAL - Static variable in class org.orekit.files.ccsds.definitions.Units
HectoPascal unit.
HELIUM - Static variable in class org.orekit.models.earth.atmosphere.DTM2000
Identifier for helium.
HelmertTransformation - Class in org.orekit.frames
Transformation class for geodetic systems.
HelmertTransformation(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.frames.HelmertTransformation
Build a transform from its primitive operations.
HelmertTransformation.Predefined - Enum in org.orekit.frames
Enumerate for predefined Helmert transformations.
HERTZ - Static variable in class org.orekit.utils.units.Unit
Hertz unit.
HighamHall54IntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for HighamHall54Integrator.
HighamHall54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder
Build a new instance.
HolmesFeatherstoneAttractionModel - Class in org.orekit.forces.gravity
This class represents the gravitational field of a celestial body.
HolmesFeatherstoneAttractionModel(Frame, NormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Creates a new instance.
HOUR - Static variable in class org.orekit.utils.units.Unit
Hour unit.
HYDROGEN - Static variable in class org.orekit.models.earth.atmosphere.DTM2000
Identifier for hydrogen.
hyperbolicEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the mean anomaly from the hyperbolic eccentric anomaly.
hyperbolicEccentricToMean(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the mean anomaly from the hyperbolic eccentric anomaly.
hyperbolicEccentricToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the true anomaly from the hyperbolic eccentric anomaly.
hyperbolicEccentricToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the true anomaly from the hyperbolic eccentric anomaly.
HZ_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Hertz per second unit.

I

i - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
final inclination.
i - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final inclination.
IAU_2012_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants
Astronomical unit as a conventional unit of length since IAU 2012 resolution B2: 149597870700.0 m.
IAU_2015_NOMINAL_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius as defined by IAU 2015 resolution B3: 6.3781e6 (m).
IAU_2015_NOMINAL_EARTH_GM - Static variable in interface org.orekit.utils.Constants
Earth attraction coefficient as defined by IAU 2015 resolution B3: 3.986004e14 (m³/s²).
IAU_2015_NOMINAL_EARTH_POLAR_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth polar radius as defined by IAU 2015 resolution B3: 6.3568e6 (m).
IAU_2015_NOMINAL_JUPITER_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Jupiter equatorial radius as defined by IAU 2015 resolution B3: 7.1492e7 (m).
IAU_2015_NOMINAL_JUPITER_GM - Static variable in interface org.orekit.utils.Constants
Jupiter attraction coefficient as defined by IAU 2015 resolution B3: 1.2668653e17 (m³/s²).
IAU_2015_NOMINAL_JUPITER_POLAR_RADIUS - Static variable in interface org.orekit.utils.Constants
Jupiter polar radius as defined by IAU 2015 resolution B3: 6.6854e7 (m).
IAU_2015_NOMINAL_SOLAR_RADIUS - Static variable in interface org.orekit.utils.Constants
Solar radius as defined by IAU 2015 resolution B3: 695700000.0 m.
IAU_2015_NOMINAL_SUN_GM - Static variable in interface org.orekit.utils.Constants
Sun attraction coefficient as defined by IAU 2015 resolution B3: 1.3271244e20 (m³/s²).
IAUPole - Interface in org.orekit.bodies
Interface for IAU pole and prime meridian orientations.
ICGEM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for ICGEM files.
ICGEMFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the ICGEM gravity field format.
ICGEMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader
Simple constructor.
ICGEMFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader
Simple constructor.
IDENTITY - Static variable in class org.orekit.frames.Transform
Identity transform.
IDENTITY - Static variable in class org.orekit.utils.AngularCoordinates
Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).
IDENTITY - Static variable in class org.orekit.utils.units.UnitsConverter
Identity converter.
IDENTITY_PROVIDER - Static variable in class org.orekit.frames.TransformProviderUtils
Identity provider.
IdentityConverter - Class in org.orekit.files.ccsds.ndm.tdm
Identity converter for Range Units.
IdentityConverter() - Constructor for class org.orekit.files.ccsds.ndm.tdm.IdentityConverter
 
IERS2003_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from IERS2003 model: 7.292115e-5 rad/s.
IERS2003_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from IERS2003 model: -1.0826359e-3.
IERS2003_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from IERS2003 model: 6378136.6 m.
IERS2003_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from IERS2003 model: 1.0 / 298.25642.
IERS2003_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from IERS2003 model: 3.986004418e14 m³/s².
IERS2010_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from IERS2010 model: 7.292115e-5 rad/s.
IERS2010_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from IERS2010 model: -1.0826359e-3.
IERS2010_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from IERS2010 model: 6378136.6 m.
IERS2010_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from IERS2010 model: 1.0 / 298.25642.
IERS2010_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from IERS2010 model: 3.986004418e14 m³/s².
IERS96_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from IERS96 model: 7.292115e-5 rad/s.
IERS96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from IERS96 model: -1.0826359e-3.
IERS96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from IERS96 model: 6378136.49 m.
IERS96_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from IERS96 model: 1.0 / 298.25642.
IERS96_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from IERS96 model: 3.986004418e14 m³/s².
IERSConventions - Enum in org.orekit.utils
Supported IERS conventions.
IERSConventions.NutationCorrectionConverter - Interface in org.orekit.utils
Interface for functions converting nutation corrections between δΔψ/δΔε to δX/δY.
IgsSsrDataField - Enum in org.orekit.gnss.metric.parser
Enum containing all intermediate level data fields that can be parsed to build an IGS SSR message.
IgsSsrMessagesParser - Class in org.orekit.gnss.metric.parser
Parser for SSR encoded messages.
IgsSsrMessagesParser(List<Integer>) - Constructor for class org.orekit.gnss.metric.parser.IgsSsrMessagesParser
Constructor.
IgsSsrMessageType - Enum in org.orekit.gnss.metric.parser
Enum containing the supported IGS SSR messages types.
ILRSHeader - Class in org.orekit.files.ilrs
Container for common data contains in International Laser Ranging Service (ILRS) files header.
ILRSHeader() - Constructor for class org.orekit.files.ilrs.ILRSHeader
 
ImmutableTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils
A cache of TimeStamped data that provides concurrency through immutability.
ImmutableTimeStampedCache(int, Collection<? extends T>) - Constructor for class org.orekit.utils.ImmutableTimeStampedCache
Create a new cache with the given neighbors size and data.
ImpulseManeuver<T extends EventDetector> - Class in org.orekit.forces.maneuvers
Impulse maneuver model.
ImpulseManeuver(T, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
ImpulseManeuver(T, AttitudeProvider, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
INC - Static variable in enum org.orekit.orbits.OrbitType
Name for inclination.
increment(double[]) - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
Increment the value.
increment(T[]) - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Increment the value.
increment(double[]) - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Increment the value.
inData() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Acknowledge data parsing has started.
InertialForces - Class in org.orekit.forces.inertia
Inertial force model.
InertialForces(Frame) - Constructor for class org.orekit.forces.inertia.InertialForces
Simple constructor.
InertialProvider - Class in org.orekit.attitudes
This class handles an attitude provider aligned with a frame or a fixed offset to it.
InertialProvider(Rotation) - Constructor for class org.orekit.attitudes.InertialProvider
Creates new instance.
InertialProvider(Frame) - Constructor for class org.orekit.attitudes.InertialProvider
Creates new instance aligned with the given frame.
InertialProvider(Rotation, Frame) - Constructor for class org.orekit.attitudes.InertialProvider
Creates new instance with a fixed attitude in the given frame.
inHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Acknowledge header parsing has started.
init(JavacTask, String...) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
 
init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Initialize builder at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler
Initialize scheduler at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Initialize builder at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.estimation.measurements.generation.Scheduler
Initialize scheduler at the start of a measurements generation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.estimation.sequential.EskfMeasurementHandler
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.empirical.AccelerationModel
Initialize the acceleration model at the start of the propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel
Initialize the acceleration model at the start of the propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.ParametricAcceleration
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel
Initialize the acceleration model at the start of the propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.ForceModel
Initialize the force model at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.ForceModel
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
Initialize the additional state provider at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.Maneuver
Initialize the force model at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.Maneuver
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Initialization method.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Initialization method.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Initialization method called at propagation start.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Initialization method called at propagation start.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Initialization method called at propagation start.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.maneuvers.trigger.FieldManeuverTriggersResetter
Initialization method called at propagation start.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Initialization method called at propagation start.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Initialization method called at propagation start.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter
Initialization method called at propagation start.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.AdditionalStateProvider
Initialize the additional state provider at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AbstractDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AdapterDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.BooleanDetector
 
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.events.EventDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventShifter
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventSlopeFilter
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventState
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldEventState
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, T) - Method in interface org.orekit.propagation.events.handlers.EventHandler
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, D) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>, KK) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.MagneticFieldDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.NegateDetector
 
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.PositionAngleDetector
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
Initialize the additional state provider at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations
Initialize the equations at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.integration.AdditionalEquations
Deprecated.
Initialize the equations at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.integration.AdditionalEquationsAdapter
Deprecated.
Initialize the generator at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations
Initialize the equations at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
Initialize the generator at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations
Deprecated.
Initialize the equations at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAdditionalEquationsAdapter
Deprecated.
Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Deprecated.
Initialize the generator at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>, T) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler
Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler
Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Initialize step handler at the start of a propagation.
init(List<SpacecraftState>, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, double) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Deprecated.
Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Initialize the force model at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Initialize the force model at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Initialize the force model at the start of propagation.
initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Check if the initial state is provided in osculating elements.
initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Check if the initial state is provided in osculating elements.
initializeAdditionalStates(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator
Initialize the additional state providers at the start of propagation.
initializeAdditionalStates(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Initialize the additional state providers at the start of propagation.
initializeFieldShortPeriodTerms(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Initialize the short periodic terms for the "field" elements.
initializePropagation() - Method in class org.orekit.propagation.AbstractPropagator
Initialize propagation.
initializePropagation() - Method in class org.orekit.propagation.FieldAbstractPropagator
Initialize propagation.
initializeResetters(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Initialize resetters.
initializeResetters(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Initialize resetters.
initializeShortPeriodicTerms(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Initialize the short periodic terms for the Kalman Filter.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Computes the highest power of the eccentricity and the highest power of a/R3 to appear in the truncated analytical power series expansion.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Performs initialization prior to propagation for the current force model.
initMapper() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Initialize the mapper.
initMapper(Field<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Initialize the mapper.
initPVCoordinates() - Method in class org.orekit.orbits.CartesianOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.CircularOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldCartesianOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.Orbit
Compute the position/velocity coordinates from the canonical parameters.
initStates(FieldSpacecraftState<Gradient>) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Initialize first state with 0 parameters.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Acknowledge metada parsing has started.
InputStreamEncodedMessages - Class in org.orekit.gnss.metric.parser
Encoded message from an input stream.
InputStreamEncodedMessages(InputStream) - Constructor for class org.orekit.gnss.metric.parser.InputStreamEncodedMessages
Simple constructor.
insideLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
Check if date is within a leap second introduction in this time scale.
insideLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
Check if date is within a leap second introduction in this time scale.
insideLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Check if date is within a leap second introduction in this time scale.
insideLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
Check if date is within a leap second introduction in this time scale.
insideLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Check if date is within a leap second introduction in this time scale.
insideLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
Check if date is within a leap second introduction in this time scale.
intArrayToString(int[]) - Method in class org.orekit.files.ccsds.section.AbstractWriter
Convert an array of integer to a comma-separated list.
IntegerBootstrapping - Class in org.orekit.estimation.measurements.gnss
Bootstrapping engine for ILS problem solving.
IntegerBootstrapping(double) - Constructor for class org.orekit.estimation.measurements.gnss.IntegerBootstrapping
Constructor for the bootstrapping ambiguity estimator.
integerGaussTransformation(int, int) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Perform one integer Gauss transformation.
IntegerLeastSquareComparator - Class in org.orekit.estimation.measurements.gnss
Comparator for IntegerLeastSquareSolution instance.
IntegerLeastSquareComparator() - Constructor for class org.orekit.estimation.measurements.gnss.IntegerLeastSquareComparator
Simple constructor.
IntegerLeastSquareSolution - Class in org.orekit.estimation.measurements.gnss
Class holding a solution to an Integer Least Square problem.
IntegerLeastSquareSolution(long[], double) - Constructor for class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution
Simple constructor.
IntegerLeastSquareSolver - Interface in org.orekit.estimation.measurements.gnss
Interface for algorithms solving integer least square problems.
integrate(UnivariateVectorFunction, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussQuadrature
Integrates a given function on the given interval.
integrate(CalculusFieldUnivariateVectorFunction<T>, T, T, Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussQuadrature
Integrates a given function on the given interval.
IntegratedEphemeris - Class in org.orekit.propagation.integration
This class stores sequentially generated orbital parameters for later retrieval.
IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, PropagationType, DenseOutputModel, Map<String, double[]>, List<AdditionalStateProvider>, String[]) - Constructor for class org.orekit.propagation.integration.IntegratedEphemeris
IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, PropagationType, DenseOutputModel, DoubleArrayDictionary, List<AdditionalStateProvider>, String[]) - Constructor for class org.orekit.propagation.integration.IntegratedEphemeris
IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, PropagationType, DenseOutputModel, DoubleArrayDictionary, List<AdditionalStateProvider>, String[], int[]) - Constructor for class org.orekit.propagation.integration.IntegratedEphemeris
Creates a new instance of IntegratedEphemeris.
IntegrationReference - Enum in org.orekit.files.ccsds.ndm.tdm
Relationship between time tag and integration interval.
INTERMEDIATE_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation
Suffix for ground station intermediate frame name.
interpolate(AbsoluteDate, Stream<Attitude>) - Method in class org.orekit.attitudes.Attitude
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldAttitude<T>>) - Method in class org.orekit.attitudes.FieldAttitude
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Collection<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform
Interpolate a transform from a sample set of existing transforms.
interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform
Interpolate a transform from a sample set of existing transforms.
interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, AngularDerivativesFilter, Stream<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform
Interpolate a transform from a sample set of existing transforms.
interpolate(AbsoluteDate, Stream<Transform>) - Method in class org.orekit.frames.Transform
Get an interpolated instance.
interpolate(AbsoluteDate, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<Transform>) - Static method in class org.orekit.frames.Transform
Interpolate a transform from a sample set of existing transforms.
interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.CartesianOrbit
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.CircularOrbit
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.EquinoctialOrbit
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldCartesianOrbit
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldCircularOrbit
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.KeplerianOrbit
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldSpacecraftState<T>>) - Method in class org.orekit.propagation.FieldSpacecraftState
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<SpacecraftState>) - Method in class org.orekit.propagation.SpacecraftState
Get an interpolated instance.
interpolate(FieldAbsoluteDate<KK>, Collection<T>) - Method in interface org.orekit.time.FieldTimeInterpolable
Get an interpolated instance.
interpolate(FieldAbsoluteDate<KK>, Stream<T>) - Method in interface org.orekit.time.FieldTimeInterpolable
Get an interpolated instance.
interpolate(AbsoluteDate, Collection<T>) - Method in interface org.orekit.time.TimeInterpolable
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<T>) - Method in interface org.orekit.time.TimeInterpolable
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<AbsolutePVCoordinates>) - Method in class org.orekit.utils.AbsolutePVCoordinates
 
interpolate(Frame, AbsoluteDate, CartesianDerivativesFilter, Stream<AbsolutePVCoordinates>) - Static method in class org.orekit.utils.AbsolutePVCoordinates
Interpolate position-velocity.
interpolate(FieldAbsoluteDate<T>, Stream<FieldAbsolutePVCoordinates<T>>) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
 
interpolate(Frame, FieldAbsoluteDate<T>, CartesianDerivativesFilter, Stream<FieldAbsolutePVCoordinates<T>>) - Static method in class org.orekit.utils.FieldAbsolutePVCoordinates
Interpolate position-velocity.
interpolate(AbsoluteDate, AngularDerivativesFilter, Collection<TimeStampedAngularCoordinates>) - Static method in class org.orekit.utils.TimeStampedAngularCoordinates
Interpolate angular coordinates.
interpolate(AbsoluteDate, AngularDerivativesFilter, Collection<TimeStampedFieldAngularCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Interpolate angular coordinates.
interpolate(FieldAbsoluteDate<T>, AngularDerivativesFilter, Collection<TimeStampedFieldAngularCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Interpolate angular coordinates.
interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, Collection<TimeStampedFieldPVCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Interpolate position-velocity.
interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, Stream<TimeStampedFieldPVCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Interpolate position-velocity.
interpolate(AbsoluteDate, CartesianDerivativesFilter, Collection<? extends TimeStampedPVCoordinates>) - Static method in class org.orekit.utils.TimeStampedPVCoordinates
Interpolate position-velocity.
interpolate(AbsoluteDate, CartesianDerivativesFilter, Stream<? extends TimeStampedPVCoordinates>) - Static method in class org.orekit.utils.TimeStampedPVCoordinates
Interpolate position-velocity.
InterpolatingTransformProvider - Class in org.orekit.frames
Transform provider using thread-safe interpolation on transforms sample.
InterpolatingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double) - Constructor for class org.orekit.frames.InterpolatingTransformProvider
Simple constructor.
InterpolationGrid - Interface in org.orekit.propagation.semianalytical.dsst.utilities
Interface for interpolation grids.
InterpolationMethod - Enum in org.orekit.files.ccsds.ndm.odm.oem
OEM interpolation method.
InterpolationTableLoader - Class in org.orekit.utils
Used to read an interpolation table from a data file.
InterpolationTableLoader() - Constructor for class org.orekit.utils.InterpolationTableLoader
 
InterSatDirectViewDetector - Class in org.orekit.propagation.events
Detector for inter-satellites direct view (i.e.
InterSatDirectViewDetector(OneAxisEllipsoid, PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.InterSatDirectViewDetector
simple constructor.
InterSatellitesPhase - Class in org.orekit.estimation.measurements.gnss
Phase measurement between two satellites.
InterSatellitesPhase(ObservableSatellite, ObservableSatellite, AbsoluteDate, double, double, double, double) - Constructor for class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
Constructor.
InterSatellitesPhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical inter-satellites phase measurement with ambiguity.
InterSatellitesPhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier
Constructor.
InterSatellitesPhaseBuilder - Class in org.orekit.estimation.measurements.generation
Builder for InterSatellitesPhase measurements.
InterSatellitesPhaseBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, double, double, double) - Constructor for class org.orekit.estimation.measurements.generation.InterSatellitesPhaseBuilder
Simple constructor.
InterSatellitesRange - Class in org.orekit.estimation.measurements
One-way or two-way range measurements between two satellites.
InterSatellitesRange(ObservableSatellite, ObservableSatellite, boolean, AbsoluteDate, double, double, double) - Constructor for class org.orekit.estimation.measurements.InterSatellitesRange
Simple constructor.
InterSatellitesRangeBuilder - Class in org.orekit.estimation.measurements.generation
Builder for InterSatellitesRange measurements.
InterSatellitesRangeBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, boolean, double, double) - Constructor for class org.orekit.estimation.measurements.generation.InterSatellitesRangeBuilder
Simple constructor.
IntervalEventTrigger<T extends AbstractDetector<T>> - Class in org.orekit.forces.maneuvers.trigger
Maneuver triggers based on a single event detector that defines firing intervals.
IntervalEventTrigger(T) - Constructor for class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Simple constructor.
intValue(EncodedMessage) - Method in interface org.orekit.gnss.metric.parser.DataField
Get the value of the field as an integer.
inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Inverse the decomposition.
inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod
Inverse the decomposition.
inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Inverse the decomposition.
IodGibbs - Class in org.orekit.estimation.iod
Gibbs initial orbit determination.
IodGibbs(double) - Constructor for class org.orekit.estimation.iod.IodGibbs
Creator.
IodGooding - Class in org.orekit.estimation.iod
Gooding angles only initial orbit determination, assuming Keplerian motion.
IodGooding(double) - Constructor for class org.orekit.estimation.iod.IodGooding
Creator.
IodLambert - Class in org.orekit.estimation.iod
Lambert initial orbit determination, assuming Keplerian motion.
IodLambert(double) - Constructor for class org.orekit.estimation.iod.IodLambert
Creator.
IodLaplace - Class in org.orekit.estimation.iod
Laplace angles-only initial orbit determination, assuming Keplerian motion.
IodLaplace(double) - Constructor for class org.orekit.estimation.iod.IodLaplace
Constructor.
IonosphereFreeCombination - Class in org.orekit.estimation.measurements.gnss
Ionosphere-free combination.
IonosphericGradientConverter - Class in org.orekit.estimation.measurements.modifiers
Deprecated.
as of 11.2, replaced by ModifierGradientConverter
IonosphericGradientConverter(SpacecraftState, int, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.IonosphericGradientConverter
Deprecated.
Simple constructor.
IonosphericMappingFunction - Interface in org.orekit.models.earth.ionosphere
Interface for mapping functions used in the ionospheric delay computation.
IonosphericModel - Interface in org.orekit.models.earth.ionosphere
Defines a ionospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.
IRNSS_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of the earth's rotation rate in rad/s for IRNSS user.
IRNSS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for IRNSS weeks: 1999-08-22T00:00:00 IRNSS time.
IRNSS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for IRNSS weeks: 1999-08-22.
IRNSS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
WGS 84 value of the Earth's universal gravitational parameter for IRNSS user in m³/s².
IRNSS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Number of weeks in the IRNSS cycle.
IRNSSAlmanac - Class in org.orekit.propagation.analytical.gnss.data
Class for IRNSS almanac.
IRNSSAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.IRNSSAlmanac
Constructor.
IRNSSNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in an IRNSS navigation message.
IRNSSNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Constructor.
IRNSSScale - Class in org.orekit.time
IRNSS time scale (also called IRNWT for IRNSS NetWork Time).
isA2b() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Check if rotation direction is from frame A to frame B.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.AbstractPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.analytical.Ephemeris
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.FieldAbstractPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.FieldPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.Propagator
Check if an additional state is managed.
isAfter(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is strictly after another.
isAfter(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is strictly after another.
isAfterOrEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is after or equal to another.
isAfterOrEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is after or equal to another.
isBefore(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is strictly before another.
isBefore(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is strictly before another.
isBeforeOrEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is before or equal to another.
isBeforeOrEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is before or equal to another.
isBetween(TimeStamped, TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is strictly between two others representing the boundaries of a time span.
isBetween(FieldTimeStamped<T>, FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is strictly between two others representing the boundaries of a time span.
isBetweenOrEqualTo(TimeStamped, TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is between two others representing the boundaries of a time span, or equal to one of them.
isBetweenOrEqualTo(FieldTimeStamped<T>, FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is between two others representing the boundaries of a time span, or equal to one of them.
isCenterOfMassCorrectionApplied() - Method in class org.orekit.files.ilrs.CPFHeader
Get the flag telling if the center of mass correction is applied.
isCenterOfMassCorrectionApplied() - Method in class org.orekit.files.ilrs.CRDHeader
Get the center of mass correction applied indicator.
isChildOf(Frame) - Method in class org.orekit.frames.Frame
Determine if a Frame is a child of another one.
isClosedOrbit() - Method in class org.orekit.utils.AbstractMultipleShooting
Get he flag representing if the orbit is closed.
isCloseTo(TimeStamped, double) - Method in class org.orekit.time.AbsoluteDate
Check if the instance time is close to another.
isCloseTo(FieldTimeStamped<T>, double) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance time is close to another.
isCompatibleWith(AttitudeEndoints) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Check if a endpoint is compatible with another one.
isCompatibleWithTIVs() - Method in class org.orekit.files.ilrs.CPFHeader
Get the flag for compatibility with TIVs.
isConsistencyMaintained() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header
Get the flag indicating if phase biases maintain consistency between non-dispersive and all original dispersive phase signals.
isCurrentStateInterpolated() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Determines if the current state is computed directly by the integrator, or if it is calculated using interpolation.
isDSStateDerivative(FieldSpacecraftState<T>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Check if a field state corresponds to derivatives with respect to state.
isEnabled() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Check if a measurement is enabled.
isEnabled() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Check if a measurement is enabled.
isEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents the same time as another.
isEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents the same time as another.
isExternal2SpacecraftBody() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Check if attitude is from external frame to spacecraft body frame.
isFiring(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Check if maneuvering is on.
isFiring(FieldSpacecraftState<T>) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Check if maneuvering is on.
isFiring(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Check if maneuvering is on.
isFiring(AbsoluteDate, double[]) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Find out if the maneuver is firing or not.
isFiring(FieldAbsoluteDate<S>, S[]) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Find out if the maneuver is firing or not.
isFiring(AbsoluteDate, double[]) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Find out if the maneuver is firing or not.
isFiring(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Find out if the maneuver is firing or not.
isFiring(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Check if maneuvering is on.
isFiring(AbsoluteDate, double[]) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Find out if the maneuver is firing or not.
isFiring(FieldAbsoluteDate<T>, T[]) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Find out if the maneuver is firing or not.
isFiringOnInitialState(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Method to check if the thruster is firing on initialization.
isFiringOnInitialState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Method to check if the thruster is firing on initialization.
isFiringOnInitialState(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Method to check if the thruster is firing on initialization.
isFiringOnInitialState(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Method to check if the thruster is firing on initialization.
isFirst() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Get the flag for the placement of the quaternion QC in the attitude data.
isFormatOK(String, String) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE
Check the lines format validity.
isFormatOK(String, String) - Static method in class org.orekit.propagation.analytical.tle.TLE
Check the lines format validity.
isForward() - Method in class org.orekit.propagation.events.AbstractDetector
Check if the current propagation is forward or backward.
isForward() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Check if the current propagation is forward or backward.
isForward() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Check is integration direction is forward in date.
isForward() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Check is integration direction is forward in date.
isForwardPropagation() - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Return the forward propagation flag.
isGradientStateDerivative(FieldSpacecraftState<T>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Check if a field state corresponds to derivatives with respect to state.
isHealthAvailable() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the flag indicating if GLONASS almanac health is available.
isIncreasing() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the Increasing/decreasing status of the event.
isIncreasing() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
Get the Increasing/decreasing status of the event.
isIncreasing() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event
Is the g() function increasing?
isIncreasing() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
Is the g() function increasing?
isInitialize() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Deprecated.
Get the flag for the initialization of the state jacobian.
isInside(Vector3D) - Method in class org.orekit.bodies.Ellipsoid
Check if a point is inside the ellipsoid.
isMeanOrbit() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Deprecated.
isMeanOrbit() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Check if only the mean elements should be used in a semianalitical propagation.
isMelbourneWubbenaConsistencyMaintained() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header
Get the flag indicating if consistency between code and phase biases is maintained for the MW combinations.
isNetworked() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Check if the stream is generated from a network of stations.
isNMEARequired() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Check if NMEA message must be sent to caster.
isOn() - Method in enum org.orekit.files.ccsds.definitions.OnOff
Check if status is "on".
isOnlyPosition() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Check if fitting uses only sample positions.
isOrbitDefined() - Method in class org.orekit.propagation.FieldSpacecraftState
Check if the state contains an orbit part.
isOrbitDefined() - Method in class org.orekit.propagation.SpacecraftState
Check if the state contains an orbit part.
IsotropicDrag - Class in org.orekit.forces.drag
This class models isotropic drag effects.
IsotropicDrag(double, double) - Constructor for class org.orekit.forces.drag.IsotropicDrag
Constructor with drag coefficient min/max set to ±∞.
IsotropicDrag(double, double, double, double) - Constructor for class org.orekit.forces.drag.IsotropicDrag
Constructor with drag coefficient min/max set by user.
IsotropicRadiationClassicalConvention - Class in org.orekit.forces.radiation
This class represents the features of a simplified spacecraft.
IsotropicRadiationClassicalConvention(double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention
Simple constructor.
IsotropicRadiationCNES95Convention - Class in org.orekit.forces.radiation
This class represents the features of a simplified spacecraft.
IsotropicRadiationCNES95Convention(double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention
Simple constructor.
IsotropicRadiationSingleCoefficient - Class in org.orekit.forces.radiation
This class represents the features of a simplified spacecraft.
IsotropicRadiationSingleCoefficient(double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Constructor with reflection coefficient min/max set to ±∞.
IsotropicRadiationSingleCoefficient(double, double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Constructor with reflection coefficient min/max set by user.
isPreviousStateInterpolated() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Determines if the previous state is computed directly by the integrator, or if it is calculated using interpolation.
isPseudoInertial() - Method in class org.orekit.frames.Frame
Check if the frame is pseudo-inertial.
isQuasiInertial() - Method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Check if frame should be treated as inertial.
isReceiveAmplitudeCorrectionApplied() - Method in class org.orekit.files.ilrs.CRDHeader
Get the receive amplitude correction applied indicator.
isRefractionCorrected() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
Get the flag indicating if the refraction is corrected.
isSelected() - Method in class org.orekit.utils.ParameterDriver
Check if parameter is selected.
isSignalInteger() - Method in class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias
Get the flag indicating is signal has integer property.
isSimpleEOP() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Check if tidal effects are ignored when interpolating EOP.
isSimpleEOP() - Method in class org.orekit.files.ccsds.utils.ContextBinding
Get EOP interpolation method.
isSimpleEOP() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Get EOP interpolation method.
isSimpleEop() - Method in class org.orekit.frames.EOPHistory
Determine if this history uses simplified EOP corrections.
isSpacecraftBodyRate() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Check if rates are specified in spacecraft body frame.
isSpacecraftBodyRate() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Check if rates are specified in spacecraft body frame.
isSpacecraftTimeSimplified() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Get the spacecraft time simplified flag.
isStart() - Method in class org.orekit.utils.DateDriver
Check if driver corresponds to a start date.
isStationSystemDelayApplied() - Method in class org.orekit.files.ilrs.CRDHeader
Get the station system delay applied indicator.
isSupported(DataProvider) - Method in class org.orekit.data.DataProvidersManager
Check if some provider is supported.
isSupported(String) - Method in class org.orekit.forces.AbstractForceModel
Check if a parameter is supported.
isSupported(String) - Method in interface org.orekit.forces.ForceModel
Check if a parameter is supported.
isTime() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Check if a field is a time field.
isTransponderDelayApplied() - Method in class org.orekit.files.ilrs.CRDHeader
Get the spacecraft system delay applied (transponders) indicator.
isTroposphericRefractionApplied() - Method in class org.orekit.files.ilrs.CRDHeader
Get the tropospheric refraction correction applied indicator.
isTwoWay() - Method in class org.orekit.estimation.measurements.InterSatellitesRange
Check if the instance represents a two-way measurement.
isTwoWay() - Method in class org.orekit.estimation.measurements.Range
Check if the instance represents a two-way measurement.
isTwoWay() - Method in class org.orekit.estimation.measurements.RangeRate
Check if the instance represents a two-way measurement.
isValid(int) - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration
Check if configuration entry is valid for a date.
isVariable(DerivativeStructure, int) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Check if a derivative represents a specified variable.
isVariable(Gradient, int) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Check if a derivative represents a specified variable.
ITRFVersion - Enum in org.orekit.frames
Enumerate for ITRF versions.
ITRFVersion.Converter - Class in org.orekit.frames
Specialized transform provider between ITRF frames.
ITRFVersionConfiguration(String, ITRFVersion, int, int) - Constructor for class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration
Simple constructor.
ITRFVersionLoader - Class in org.orekit.frames
Loader for ITRF version configuration file.
ITRFVersionLoader(String) - Constructor for class org.orekit.frames.ITRFVersionLoader
Build a loader for ITRF version configuration file.
ITRFVersionLoader(String, DataProvidersManager) - Constructor for class org.orekit.frames.ITRFVersionLoader
Build a loader for ITRF version configuration file.
ITRFVersionLoader() - Constructor for class org.orekit.frames.ITRFVersionLoader
Build a loader for ITRF version configuration file using the default name.
ITRFVersionLoader.ITRFVersionConfiguration - Class in org.orekit.frames
ITRF version configuration entry.
ItrfVersionProvider - Interface in org.orekit.frames
Interface for retrieving the ITRF version for a given set of EOP data.

J

J2000_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
J2000_EPOCH - Static variable in class org.orekit.time.DateComponents
J2000.0 Reference epoch: 2000-01-01.
J2DifferentialEffect - Class in org.orekit.propagation.analytical
Analytical model for J2 effect.
J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(Orbit, Orbit, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(Orbit, Orbit, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
JacobianPropagatorConverter - Class in org.orekit.propagation.conversion
Propagator converter using the real Jacobian.
JacobianPropagatorConverter(NumericalPropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.JacobianPropagatorConverter
Simple constructor.
JacobiansMapper - Class in org.orekit.propagation.numerical
Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
JacobiPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
Provider of the Jacobi polynomials Plv,w.
JAVA_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
JAVA_EPOCH - Static variable in class org.orekit.time.DateComponents
Java Reference epoch: 1970-01-01.
JB2008 - Class in org.orekit.models.earth.atmosphere
This is the realization of the Jacchia-Bowman 2008 atmospheric model.
JB2008(JB2008InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.models.earth.atmosphere.JB2008
Constructor with space environment information for internal computation.
JB2008(JB2008InputParameters, PVCoordinatesProvider, BodyShape, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.JB2008
Constructor with space environment information for internal computation.
JB2008InputParameters - Interface in org.orekit.models.earth.atmosphere
Interface for solar activity and magnetic activity data.
JB2008SpaceEnvironmentData - Class in org.orekit.models.earth.atmosphere.data
This class provides a container for the solar indices data required by the JB2008 atmospheric model.
JB2008SpaceEnvironmentData(String, String) - Constructor for class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Simple constructor.
JB2008SpaceEnvironmentData(String, String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData
Constructor that allows specifying the source of the SOLFSMY space weather file.
JOULE - Static variable in class org.orekit.utils.units.Unit
Joule unit.
JPL_SSD_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants
Astronomical Unit: 149597870691 m.
JPL_SSD_EARTH_GM - Static variable in interface org.orekit.utils.Constants
Earth attraction coefficient (m³/s²).
JPL_SSD_EARTH_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Earth/Moon mass ratio: 81.30059.
JPL_SSD_EARTH_PLUS_MOON_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Earth + Moon) attraction coefficient (m³/s²).
JPL_SSD_GAUSSIAN_GRAVITATIONAL_CONSTANT - Static variable in interface org.orekit.utils.Constants
Gaussian gravitational constant: 0.01720209895 √(AU³/d²).
JPL_SSD_JUPITER_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Jupiter system) ttraction coefficient (m³/s²).
JPL_SSD_MARS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Mars system) attraction coefficient (m³/s²).
JPL_SSD_MERCURY_GM - Static variable in interface org.orekit.utils.Constants
Sun/Mercury attraction coefficient (m³/s²).
JPL_SSD_MOON_GM - Static variable in interface org.orekit.utils.Constants
Moon attraction coefficient (m³/s²).
JPL_SSD_NEPTUNE_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Neptune system) attraction coefficient (m³/s²).
JPL_SSD_PLUTO_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Pluto system) ttraction coefficient (m³/s²).
JPL_SSD_SATURN_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Saturn system) attraction coefficient (m³/s²).
JPL_SSD_SUN_EARTH_PLUS_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Earth + Moon) mass ratio: 328900.56.
JPL_SSD_SUN_GM - Static variable in interface org.orekit.utils.Constants
Sun attraction coefficient (m³/s²).
JPL_SSD_SUN_JUPITER_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Jupiter system) mass ratio: 1047.3486.
JPL_SSD_SUN_MARS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Mars system) mass ratio: 3098708.0.
JPL_SSD_SUN_MERCURY_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/Mercury mass ratio: 6023600.
JPL_SSD_SUN_NEPTUNE_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Neptune system) mass ratio: 19412.24.
JPL_SSD_SUN_PLUTO_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Pluto system) mass ratio: 1.35e8.
JPL_SSD_SUN_SATURN_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Saturn system) mass ratio: 3497.898.
JPL_SSD_SUN_URANUS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Uranus system) mass ratio: 22902.98.
JPL_SSD_SUN_VENUS_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/Venus mass ratio: 408523.71.
JPL_SSD_URANUS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Uranus system) attraction coefficient (m³/s²).
JPL_SSD_VENUS_GM - Static variable in interface org.orekit.utils.Constants
Sun/Venus attraction coefficient (m³/s²).
JPLEphemeridesLoader - Class in org.orekit.bodies
Loader for JPL ephemerides binary files (DE 4xx) and similar formats (INPOP 06/08/10).
JPLEphemeridesLoader(String, JPLEphemeridesLoader.EphemerisType) - Constructor for class org.orekit.bodies.JPLEphemeridesLoader
Create a loader for JPL ephemerides binary files.
JPLEphemeridesLoader(String, JPLEphemeridesLoader.EphemerisType, DataProvidersManager, TimeScales, Frame) - Constructor for class org.orekit.bodies.JPLEphemeridesLoader
Create a loader for JPL ephemerides binary files.
JPLEphemeridesLoader.EphemerisType - Enum in org.orekit.bodies
List of supported ephemerides types.
JPLEphemeridesLoader.RawPVProvider - Interface in org.orekit.bodies
Interface for raw position-velocity retrieval.
JULIAN_CENTURY - Static variable in interface org.orekit.utils.Constants
Duration of a Julian century: 36525 Constants.JULIAN_DAY.
JULIAN_DAY - Static variable in interface org.orekit.utils.Constants
Duration of a mean solar day: 86400.0 s.
JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for julian dates: -4712-01-01.
JULIAN_EPOCH - Static variable in class org.orekit.time.DateTimeComponents
The Julian Epoch.
JULIAN_YEAR - Static variable in interface org.orekit.utils.Constants
Duration of a Julian year: 365.25 Constants.JULIAN_DAY.
JUPITER - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Jupiter.

K

K1 - Static variable in class org.orekit.models.earth.displacement.Tide
K₁ tide.
K2 - Static variable in class org.orekit.models.earth.displacement.Tide
K₂ tide.
KalmanEstimation - Interface in org.orekit.estimation.sequential
Interface for accessing Kalman filter estimations.
KalmanEstimator - Class in org.orekit.estimation.sequential
Implementation of a Kalman filter to perform orbit determination.
KalmanEstimatorBuilder - Class in org.orekit.estimation.sequential
Builder for a Kalman filter estimator.
KalmanEstimatorBuilder() - Constructor for class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Default constructor.
KalmanModel - Class in org.orekit.estimation.sequential
Class defining the process model dynamics to use with a KalmanEstimator.
KalmanModel(List<OrbitDeterminationPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.KalmanModel
Kalman process model constructor.
KalmanObserver - Interface in org.orekit.estimation.sequential
Observer for Kalman filter estimations.
KeplerianElements - Class in org.orekit.files.ccsds.ndm.odm
Container for Keplerian elements.
KeplerianElements() - Constructor for class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Simple constructor.
KeplerianElementsKey - Enum in org.orekit.files.ccsds.ndm.odm
Keys for Keplerian elements entries.
KeplerianOrbit - Class in org.orekit.orbits
This class handles traditional Keplerian orbital parameters.
KeplerianOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Creates a new instance.
KeplerianOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Creates a new instance.
KeplerianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from Cartesian parameters.
KeplerianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from Cartesian parameters.
KeplerianOrbit(Orbit) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from any kind of orbital parameters.
KeplerianPropagator - Class in org.orekit.propagation.analytical
Simple Keplerian orbit propagator.
KeplerianPropagator(Orbit) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit only.
KeplerianPropagator(Orbit, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit and central attraction coefficient μ.
KeplerianPropagator(Orbit, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit and attitude provider.
KeplerianPropagator(Orbit, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit, attitude provider and central attraction coefficient μ.
KeplerianPropagator(Orbit, AttitudeProvider, double, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
KeplerianPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for Keplerian propagator.
KeplerianPropagatorBuilder(Orbit, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a new instance.
KeplerianPropagatorBuilder(Orbit, PositionAngle, double, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a new instance.
KG_M2 - Static variable in class org.orekit.files.ccsds.definitions.Units
kg.m² unit.
KILOGRAM - Static variable in class org.orekit.utils.units.Unit
Kilogram unit.
KILOMETRE - Static variable in class org.orekit.utils.units.Unit
Kilometre unit.
KILOMETRES_2_TO_METRES_2 - Static variable in class org.orekit.utils.units.UnitsConverter
Square kilometres to square metres converter.
KILOMETRES_TO_METRES - Static variable in class org.orekit.utils.units.UnitsConverter
Kilometres to metres converter.
KlobucharIonoCoefficientsLoader - Class in org.orekit.models.earth.ionosphere
Loads Klobuchar-Style ionospheric coefficients a given input stream.
KlobucharIonoCoefficientsLoader(String) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Constructor with supported names given by user.
KlobucharIonoCoefficientsLoader(String, DataProvidersManager) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Constructor that uses user defined supported names and data context.
KlobucharIonoCoefficientsLoader() - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Constructor with default supported names.
KlobucharIonoModel - Class in org.orekit.models.earth.ionosphere
Klobuchar ionospheric delay model.
KlobucharIonoModel(double[], double[]) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Create a new Klobuchar ionospheric delay model, when a single frequency system is used.
KlobucharIonoModel(double[], double[], TimeScale) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Create a new Klobuchar ionospheric delay model, when a single frequency system is used.
KM2 - Static variable in class org.orekit.files.ccsds.definitions.Units
Square kilometers units.
KM2_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Square kilometers per second units.
KM2_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units
Square kilometers per square second units.
KM3_P_S2_TO_M3_P_S2 - Static variable in class org.orekit.utils.units.UnitsConverter
km³/s² to m³/s² converter.
KM3_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units
km³/s² unit.
KM_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Kilometers per second units.
KM_PER_S - Static variable in class org.orekit.gnss.metric.parser.Units
Kilometers par second units.
KM_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units
Kilometers per square second units.
KM_PER_S2 - Static variable in class org.orekit.gnss.metric.parser.Units
Kilometers par square second units.
KnockeRediffusedForceModel - Class in org.orekit.forces.radiation
The Knocke Earth Albedo and IR emission force model.
KnockeRediffusedForceModel(ExtendedPVCoordinatesProvider, RadiationSensitive, double, double) - Constructor for class org.orekit.forces.radiation.KnockeRediffusedForceModel
Default Constructor.
KnockeRediffusedForceModel(ExtendedPVCoordinatesProvider, RadiationSensitive, double, double, TimeScale) - Constructor for class org.orekit.forces.radiation.KnockeRediffusedForceModel
General constructor.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.AemWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.cdm.CdmWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.OemWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.OpmWriter
Padding width for aligning the '=' sign.
KVN_PADDING_WIDTH - Static variable in class org.orekit.files.ccsds.ndm.tdm.TdmWriter
Padding width for aligning the '=' sign.
KvnGenerator - Class in org.orekit.files.ccsds.utils.generation
Generator for Key-Value Notation CCSDS messages.
KvnGenerator(Appendable, int, String, int) - Constructor for class org.orekit.files.ccsds.utils.generation.KvnGenerator
Simple constructor.
KvnLexicalAnalyzer - Class in org.orekit.files.ccsds.utils.lexical
Lexical analyzer for Key-Value Notation CCSDS messages.
KvnLexicalAnalyzer(DataSource) - Constructor for class org.orekit.files.ccsds.utils.lexical.KvnLexicalAnalyzer
Simple constructor.
KvnStructureKey - Enum in org.orekit.files.ccsds.section
Keys for FileFormat.KVN format structure.
KvnStructureProcessingState - Class in org.orekit.files.ccsds.section
ProcessingState for structure of FileFormat.KVN CCSDS Messages.
KvnStructureProcessingState(AbstractConstituentParser<?, ?>) - Constructor for class org.orekit.files.ccsds.section.KvnStructureProcessingState
Simple constructor.

L

L1Frame - Class in org.orekit.frames
Class to create a L1 centered frame with L1TransformProvider.
L1Frame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L1Frame
Simple constructor.
L1TransformProvider - Class in org.orekit.frames
L1 Transform provider for a frame on the L1 Lagrange point of two celestial bodies.
L1TransformProvider(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L1TransformProvider
Simple constructor.
L2Frame - Class in org.orekit.frames
Class to create a L2 centered frame with L2TransformProvider.
L2Frame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L2Frame
Simple constructor.
LagrangianPoints - Enum in org.orekit.utils
Enumerate for selecting which Lagrangian Point to consider in different classes.
LambdaMethod - Class in org.orekit.estimation.measurements.gnss
Decorrelation/reduction engine for LAMBDA method.
LambdaMethod() - Constructor for class org.orekit.estimation.measurements.gnss.LambdaMethod
 
LaserConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
 
LatitudeCrossingDetector - Class in org.orekit.propagation.events
Detector for geographic latitude crossing.
LatitudeCrossingDetector(OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LatitudeCrossingDetector
Build a new detector.
LatitudeCrossingDetector(double, double, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LatitudeCrossingDetector
Build a detector.
LatitudeExtremumDetector - Class in org.orekit.propagation.events
Detector for geographic latitude extremum.
LatitudeExtremumDetector(OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LatitudeExtremumDetector
Build a new detector.
LatitudeExtremumDetector(double, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LatitudeExtremumDetector
Build a detector.
LazyLoadedCelestialBodies - Class in org.orekit.bodies
This class lazily loads auxiliary data when it is needed by a requested body.
LazyLoadedCelestialBodies(DataProvidersManager, TimeScales, Frame) - Constructor for class org.orekit.bodies.LazyLoadedCelestialBodies
Create a celestial body factory with the given auxiliary data sources.
LazyLoadedDataContext - Class in org.orekit.data
A data context that aims to match the behavior of Orekit 10.0 regarding auxiliary data.
LazyLoadedDataContext() - Constructor for class org.orekit.data.LazyLoadedDataContext
Create a new data context that only loads auxiliary data when it is first accessed and allows configuration of the auxiliary data sources until then.
LazyLoadedEop - Class in org.orekit.frames
Loads Earth Orientation Parameters (EOP) from a configured set of EOPHistoryLoaders on demand.
LazyLoadedEop(DataProvidersManager) - Constructor for class org.orekit.frames.LazyLoadedEop
Create a new instance for loading EOP data from multiple EOPHistoryLoaders.
LazyLoadedFrames - Class in org.orekit.frames
This class lazily loads auxiliary data when it is needed by a requested frame.
LazyLoadedFrames(LazyLoadedEop, TimeScales, CelestialBodies) - Constructor for class org.orekit.frames.LazyLoadedFrames
Create a collection of frames from the given auxiliary data.
LazyLoadedGeoMagneticFields - Class in org.orekit.models.earth
Loads magnetic fields on request and can be configured after creation.
LazyLoadedGeoMagneticFields(DataProvidersManager) - Constructor for class org.orekit.models.earth.LazyLoadedGeoMagneticFields
Create a factory for magnetic fields that uses the given data manager to load magnetic field files.
LazyLoadedGravityFields - Class in org.orekit.forces.gravity.potential
Loads gravity fields when first requested and can be configured until then.
LazyLoadedGravityFields(DataProvidersManager, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Create a factory for gravity fields that uses the given data manager to load the gravity field files.
LazyLoadedTimeScales - Class in org.orekit.time
An implementation of TimeScales that loads auxiliary data, leap seconds and UT1-UTC, when it is first accessed.
LazyLoadedTimeScales(LazyLoadedEop) - Constructor for class org.orekit.time.LazyLoadedTimeScales
Create a new set of time scales with the given sources of auxiliary data.
LegendrePolynomials - Class in org.orekit.utils
Computes the Pnm(t) coefficients.
LegendrePolynomials(int, int, double) - Constructor for class org.orekit.utils.LegendrePolynomials
Create Legendre polynomials for the given degree and order.
LenseThirringRelativity - Class in org.orekit.forces.gravity
Lense-Thirring post-Newtonian correction force due to general relativity.
LenseThirringRelativity(double, Frame) - Constructor for class org.orekit.forces.gravity.LenseThirringRelativity
Constructor.
LexicalAnalyzer - Interface in org.orekit.files.ccsds.utils.lexical
Interface for CCSDS messages lexical analysis.
LexicalAnalyzerSelector - Class in org.orekit.files.ccsds.utils.lexical
Utility class for selecting either XmlLexicalAnalyzer or KvnLexicalAnalyzer depending on data first bytes.
LibrationOrbit - Class in org.orekit.orbits
Base class for libration orbits.
LibrationOrbit(CR3BPSystem, PVCoordinates, double) - Constructor for class org.orekit.orbits.LibrationOrbit
Constructor.
LibrationOrbitFamily - Enum in org.orekit.orbits
Enumerate for Libration Orbit family.
LibrationOrbitType - Enum in org.orekit.orbits
Enumerate for Libration Orbit type.
LIFT_RATIO - Static variable in interface org.orekit.forces.drag.DragSensitive
Parameter name for lift ration enabling Jacobian processing.
lIndex(int, int) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the index of an entry in the lower triangular matrix.
lineOfSight(double, double) - Static method in class org.orekit.estimation.iod.IodGooding
Calculates the line of sight vector.
lineOfSight(AngularRaDec) - Static method in class org.orekit.estimation.iod.IodGooding
Calculate the line of sight vector from an AngularRaDec measurement.
lineOfSight(double, double) - Static method in class org.orekit.estimation.iod.IodLaplace
Calculates the line of sight vector.
lineOfSight(AngularRaDec) - Static method in class org.orekit.estimation.iod.IodLaplace
Calculate the line of sight vector from an AngularRaDec measurement.
LineParameters(AbsoluteDate, double[], double, double[], double, double, int, double, double, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Constructor.
LineParameters(AbsoluteDate, double) - Constructor for class org.orekit.models.earth.atmosphere.data.DtcDataLoader.LineParameters
Constructor.
LineParameters(AbsoluteDate, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
Constructor.
LineReader(String, BufferedReader) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader
Deprecated.
Create a line reader.
LnsCoefficients - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Lns(γ).
LnsCoefficients(int, int, double[][], TreeMap<CoefficientsFactory.NSKey, Double>, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Create a set of Lns(γ) coefficients.
loadCelestialBody(String) - Method in interface org.orekit.bodies.CelestialBodyLoader
Load celestial body.
loadCelestialBody(String) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Load celestial body.
loadData(InputStream, String) - Method in interface org.orekit.data.DataLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCHatEpsilonReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCnmSnmReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.gnss.RinexObservationLoader.Parser
Load data from a stream.
loadData() - Method in class org.orekit.gnss.SEMParser
Loads almanacs.
loadData(InputStream, String) - Method in class org.orekit.gnss.SEMParser
 
loadData() - Method in class org.orekit.gnss.YUMAParser
Loads almanacs.
loadData(InputStream, String) - Method in class org.orekit.gnss.YUMAParser
 
loadData(InputStream, String) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.GeoMagneticModelLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Load Klobuchar-Style ionospheric coefficients read from some file.
loadData(InputStream, String) - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
 
loadData(InputStream, String) - Method in class org.orekit.utils.InterpolationTableLoader
Loads an bi-variate interpolation table from the given InputStream.
loadKlobucharIonosphericCoefficients() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Load the data using supported names .
loadKlobucharIonosphericCoefficients(DateComponents) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Load the data for a given day.
loadLoveNumbers(String) - Method in enum org.orekit.utils.IERSConventions
Load the Love numbers.
loadOffsets() - Method in class org.orekit.time.AGILeapSecondFilesLoader
Load UTC-TAI offsets entries.
loadOffsets() - Method in class org.orekit.time.TAIUTCDatFilesLoader
Load UTC-TAI offsets entries.
loadOffsets() - Method in class org.orekit.time.UTCTAIBulletinAFilesLoader
Load UTC-TAI offsets entries.
loadOffsets() - Method in class org.orekit.time.UTCTAIHistoryFilesLoader
Load UTC-TAI offsets entries.
loadOffsets() - Method in interface org.orekit.time.UTCTAIOffsetsLoader
Load UTC-TAI offsets entries.
loadViennaCoefficients() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Load the data using supported names .
loadViennaCoefficients(DateTimeComponents) - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Load the data for a given day.
LocalizedException - Interface in org.orekit.errors
This interface specified methods implemented by localized exception classes.
LocalOrbitalFrame - Class in org.orekit.frames
Class for frames moving with an orbiting satellite.
LocalOrbitalFrame(Frame, LOFType, PVCoordinatesProvider, String) - Constructor for class org.orekit.frames.LocalOrbitalFrame
Build a new instance.
LofOffset - Class in org.orekit.attitudes
Attitude law defined by fixed Roll, Pitch and Yaw angles (in any order) with respect to a local orbital frame.
LofOffset(Frame, LOFType) - Constructor for class org.orekit.attitudes.LofOffset
Create a LOF-aligned attitude.
LofOffset(Frame, LOFType, RotationOrder, double, double, double) - Constructor for class org.orekit.attitudes.LofOffset
Creates new instance.
LofOffsetPointing - Class in org.orekit.attitudes
This class provides a default attitude provider.
LofOffsetPointing(Frame, BodyShape, AttitudeProvider, Vector3D) - Constructor for class org.orekit.attitudes.LofOffsetPointing
Creates new instance.
LOFType - Enum in org.orekit.frames
Enumerate for different types of Local Orbital Frames.
LongitudeCrossingDetector - Class in org.orekit.propagation.events
Detector for geographic longitude crossing.
LongitudeCrossingDetector(OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LongitudeCrossingDetector
Build a new detector.
LongitudeCrossingDetector(double, double, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LongitudeCrossingDetector
Build a detector.
LongitudeExtremumDetector - Class in org.orekit.propagation.events
Detector for geographic longitude extremum.
LongitudeExtremumDetector(OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LongitudeExtremumDetector
Build a new detector.
LongitudeExtremumDetector(double, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LongitudeExtremumDetector
Build a detector.
LoveNumbers - Class in org.orekit.utils
Container for Love numbers.
LoveNumbers(double[][], double[][], double[][]) - Constructor for class org.orekit.utils.LoveNumbers
Simple constructor.
ltdlDecomposition() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Perform Lᵀ.D.L = Q decomposition of the covariance matrix.
ltdlDecomposition() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod
Perform Lᵀ.D.L = Q decomposition of the covariance matrix.
ltdlDecomposition() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Compute the LᵀDL factorization with symmetric pivoting decomposition of Q (symmetric definite positive matrix) with a minimum symmetric pivoting: Q = ZᵀLᵀDLZ.
luniSolarTermsComputation() - Method in class org.orekit.propagation.analytical.tle.DeepSDP4
Computes luni - solar terms from initial coordinates and epoch.
luniSolarTermsComputation() - Method in class org.orekit.propagation.analytical.tle.FieldDeepSDP4
Computes luni - solar terms from initial coordinates and epoch.
LutherIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for LutherIntegrator.
LutherIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.LutherIntegratorBuilder
Build a new instance.
LyapunovOrbit - Class in org.orekit.orbits
Class calculating different parameters of a Lyapunov Orbit.
LyapunovOrbit(CR3BPSystem, PVCoordinates, double) - Constructor for class org.orekit.orbits.LyapunovOrbit
Simple Constructor.
LyapunovOrbit(RichardsonExpansion, double) - Constructor for class org.orekit.orbits.LyapunovOrbit
Simple Constructor.

M

M2 - Static variable in class org.orekit.files.ccsds.definitions.Units
m² unit.
M2 - Static variable in class org.orekit.models.earth.displacement.Tide
M₂ tide.
M2 - Static variable in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Default value for M2 coefficient.
M2_NAME - Static variable in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Parameter name for M2 coefficient.
M2_PER_KG - Static variable in class org.orekit.files.ccsds.definitions.Units
m² per kilograms units.
M2_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Square meters per second units.
M2_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units
Square meters per square second units.
M2_PER_S3 - Static variable in class org.orekit.files.ccsds.definitions.Units
Square meters per cube second units.
M2_PER_S4 - Static variable in class org.orekit.files.ccsds.definitions.Units
Square meters per s⁴ units.
M3_PER_KG - Static variable in class org.orekit.files.ccsds.definitions.Units
m³ per kilograms units.
M3_PER_KGS - Static variable in class org.orekit.files.ccsds.definitions.Units
Cubic meters per kilograms second units.
M3_PER_KGS2 - Static variable in class org.orekit.files.ccsds.definitions.Units
Cubic meters per kilograms (square second) units.
M4 - Static variable in class org.orekit.files.ccsds.definitions.Units
m⁴ unit.
M4_PER_KG - Static variable in class org.orekit.files.ccsds.definitions.Units
m⁴ per kilograms units.
M4_PER_KG2 - Static variable in class org.orekit.files.ccsds.definitions.Units
m⁴ per square kilograms units.
M_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Meters per second units.
M_PER_S2 - Static variable in class org.orekit.files.ccsds.definitions.Units
Meters per square second units.
MagneticFieldDetector - Class in org.orekit.propagation.events
Detector for South-Atlantic anomaly frontier crossing.
MagneticFieldDetector(double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector
Build a new detector.
MagneticFieldDetector(double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector
Build a new detector.
MagneticFieldDetector(double, double, double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector
Build a detector.
MagneticFieldDetector(double, double, double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean, DataContext) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector
Build a detector.
MAN_LINE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Maneuver line element for XML messages.
manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
The method is in charge of collecting the measurements, manage them, and call the detection method.
manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCycleSlipDetector
The method is in charge of collecting the measurements, manage them, and call the detection method.
manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCycleSlipDetector
The method is in charge of collecting the measurements, manage them, and call the detection method.
ManBasis - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Basis of maneuver used in CCSDS Orbit Comprehensive Messages.
Maneuver - Class in org.orekit.files.ccsds.ndm.adm.apm
Maneuver in an APM file.
Maneuver() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Simple constructor.
Maneuver - Class in org.orekit.files.ccsds.ndm.odm.ocm
Maneuver entry.
Maneuver() - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Build an uninitialized maneuver.
Maneuver - Class in org.orekit.files.ccsds.ndm.odm.opm
Maneuver in an OPM file.
Maneuver() - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Simple constructor.
Maneuver - Class in org.orekit.forces.maneuvers
A generic model for maneuvers.
Maneuver(AttitudeProvider, ManeuverTriggers, PropulsionModel) - Constructor for class org.orekit.forces.maneuvers.Maneuver
Generic maneuver constructor.
ManeuverFieldType - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Maneuver field type used in CCSDS Orbit Comprehensive Messages.
ManeuverHistory - Class in org.orekit.files.ccsds.ndm.odm.ocm
Maneuver history.
ManeuverHistoryMetadata - Class in org.orekit.files.ccsds.ndm.odm.ocm
Metadata for maneuver history.
ManeuverHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Keys for maneuver history container entries.
ManeuverKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
Keys for APM maneuver entries.
ManeuverKey - Enum in org.orekit.files.ccsds.ndm.odm.opm
Keys for OPM maneuver entries.
maneuverTriggered(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
Observe a maneuver trigger.
maneuverTriggered(FieldSpacecraftState<T>, boolean) - Method in interface org.orekit.forces.maneuvers.trigger.FieldManeuverTriggersResetter
Observe a maneuver trigger.
maneuverTriggered(SpacecraftState, boolean) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter
Observe a maneuver trigger.
ManeuverTriggers - Interface in org.orekit.forces.maneuvers.trigger
Generic interface for the maneuver triggers used in a Maneuver.
ManeuverTriggersResetter - Interface in org.orekit.forces.maneuvers.trigger
Resetter for maneuver triggers.
Maneuvrable - Enum in org.orekit.files.ccsds.ndm.cdm
Maneuvrable possibilities used in CCSDS Conjunction Data Messages.
map(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
Map an Orekit frame to a CCSDS frame.
map(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CenterName
Map an Orekit frame to a CCSDS center.
map(Frame) - Static method in class org.orekit.files.ccsds.definitions.FrameFacade
Map an Orekit frame to a CCSDS frame facade.
mapArrayToOrbit(double[], double[], PositionAngle, AbsoluteDate, double, Frame) - Method in enum org.orekit.orbits.OrbitType
Convert state array to orbital parameters.
mapArrayToOrbit(T[], T[], PositionAngle, FieldAbsoluteDate<T>, T, Frame) - Method in enum org.orekit.orbits.OrbitType
Convert state array to orbital parameters.
mapArrayToState(T, T[], T[], PropagationType) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map the raw double components to a spacecraft state.
mapArrayToState(FieldAbsoluteDate<T>, T[], T[], PropagationType) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map the raw double components to a spacecraft state.
mapArrayToState(double, double[], double[], PropagationType) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double components to a spacecraft state.
mapArrayToState(AbsoluteDate, double[], double[], PropagationType) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double components to a spacecraft state.
mapDateToDouble(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map a date to a raw double time offset.
mapDateToDouble(AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper
Map a date to a raw double time offset.
mapDoubleToDate(T) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map the raw double time offset to a date.
mapDoubleToDate(T, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map the raw double time offset to a date.
mapDoubleToDate(double) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double time offset to a date.
mapDoubleToDate(double, AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double time offset to a date.
mapOrbitToArray(Orbit, PositionAngle, double[], double[]) - Method in enum org.orekit.orbits.OrbitType
Convert orbit to state array.
mapOrbitToArray(FieldOrbit<T>, PositionAngle, T[], T[]) - Method in enum org.orekit.orbits.OrbitType
Convert orbit to state array.
mappingFactor(double) - Method in interface org.orekit.models.earth.ionosphere.IonosphericMappingFunction
This method allows the computation of the ionospheric mapping factor.
mappingFactor(T) - Method in interface org.orekit.models.earth.ionosphere.IonosphericMappingFunction
This method allows the computation of the ionospheric mapping factor.
mappingFactor(double) - Method in class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction
This method allows the computation of the ionospheric mapping factor.
mappingFactor(T) - Method in class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction
This method allows the computation of the ionospheric mapping factor.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.MappingFunction
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.MappingFunction
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
With the Mendes Pavlis tropospheric model, the mapping function is not split into hydrostatic and wet component.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
With the Mendes Pavlis tropospheric model, the mapping function is not split into hydrostatic and wet component.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
This method allows the computation of the hydrostatic and wet mapping functions.
MappingFunction - Interface in org.orekit.models.earth.troposphere
Interface for mapping functions used in the tropospheric delay computation.
mappingFunction(double, double, double, double) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils
Compute the mapping function related to the coefficient values and the elevation.
mappingFunction(T, T, T, T) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils
Compute the mapping function related to the coefficient values and the elevation.
mapStateToArray(FieldSpacecraftState<T>, T[], T[]) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map a spacecraft state to raw double components.
mapStateToArray(SpacecraftState, double[], double[]) - Method in class org.orekit.propagation.integration.StateMapper
Map a spacecraft state to raw double components.
MariniMurrayModel - Class in org.orekit.models.earth.troposphere
The Marini-Murray tropospheric delay model for laser ranging.
MariniMurrayModel(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.MariniMurrayModel
Create a new Marini-Murray model for the troposphere using the given environmental conditions.
MARS - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Mars.
MarshallSolarActivityFutureEstimation - Class in org.orekit.models.earth.atmosphere.data
This class reads and provides solar activity data needed by atmospheric models: F107 solar flux, Ap and Kp indexes.
MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Simple constructor.
MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Constructor that allows specifying the source of the MSAFE auxiliary data files.
MarshallSolarActivityFutureEstimation.StrengthLevel - Enum in org.orekit.models.earth.atmosphere.data
Strength level of activity.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Sets the mass.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Sets the mass.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Sets the mass.
mass(double) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
Sets the mass.
MASS_RATIO_SUFFIX - Static variable in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Suffix for parameter name for Mass Ratio enabling Jacobian processing.
MassDepletionDelay - Class in org.orekit.forces.maneuvers.jacobians
Generator for effect of delaying mass depletion when delaying a maneuver.
MassDepletionDelay(String, boolean, Maneuver) - Constructor for class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
Simple constructor.
MatricesHarvester - Interface in org.orekit.propagation
Interface for extracting State Transition Matrices and Jacobians matrices from spacecraft state.
MAX_EPOCH - Static variable in class org.orekit.time.DateComponents
Maximum supported date.
MaxGapInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolation grid where points obey a maximum time gap.
MaxGapInterpolationGrid(double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid
Constructor.
maxValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter maximum value has been changed.
MEAN_ANOM - Static variable in enum org.orekit.orbits.OrbitType
Name for mean anomaly.
MEAN_LAT_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for mean argument of latitude.
MEAN_LON_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for mean argument of longitude.
meanDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic
Get mean derivative, truncated to first components.
meanSecondDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic
Get mean second derivative, truncated to first components.
meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit
Computes the eccentric latitude argument from the mean latitude argument.
meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit
Computes the eccentric longitude argument from the mean longitude argument.
meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit
Computes the eccentric latitude argument from the mean latitude argument.
meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
Computes the eccentric longitude argument from the mean longitude argument.
meanToEllipticEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the elliptic eccentric anomaly from the mean anomaly.
meanToEllipticEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the elliptic eccentric anomaly from the mean anomaly.
meanToHyperbolicEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the hyperbolic eccentric anomaly from the mean anomaly.
meanToHyperbolicEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the hyperbolic eccentric anomaly from the mean anomaly.
meanValue(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic
Get mean value, truncated to first components.
MeasurementBuilder<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.generation
Interface for generating individual measurements.
MeasurementCombination - Interface in org.orekit.estimation.measurements.gnss
Interface for combination of measurements.
MeasurementCombinationFactory - Class in org.orekit.estimation.measurements.gnss
Factory for predefined combination of measurements.
MeasurementDecorator - Class in org.orekit.estimation.sequential
Decorator adding Measurement API to an ObservedMeasurement.
MeasurementDecorator(ObservedMeasurement<?>, RealMatrix, AbsoluteDate) - Constructor for class org.orekit.estimation.sequential.MeasurementDecorator
Simple constructor.
MeasurementFilter<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.filtering
Interface for measurement pre-processing filter.
measurementIsFeasible(double) - Method in enum org.orekit.estimation.measurements.generation.SignSemantic
Check if measurement is feasible.
MeasurementType - Enum in org.orekit.gnss
Enumerate for measurement type.
MEDIAN_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Default suffix for median driver.
MEDIAN_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Default suffix for median driver.
MedianDate - Class in org.orekit.forces.maneuvers.jacobians
Generator for one column of a Jacobian matrix for special case of maneuver median date.
MedianDate(String, String, String) - Constructor for class org.orekit.forces.maneuvers.jacobians.MedianDate
Simple constructor.
MelbourneWubbenaCombination - Class in org.orekit.estimation.measurements.gnss
Melbourne-Wübbena combination.
MendesPavlisModel - Class in org.orekit.models.earth.troposphere
The Mendes - Pavlis tropospheric delay model for optical techniques.
MendesPavlisModel(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.MendesPavlisModel
Create a new Mendes-Pavlis model for the troposphere.
MERCURY - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Mercury.
messageAvailable(String, ParsedMessage) - Method in interface org.orekit.gnss.metric.ntrip.MessageObserver
Notify that an encoded message is available.
messageNumberToSatelliteSystem(int) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
Find the satellite system corresponding to the sub-type message number.
MessageObserver - Interface in org.orekit.gnss.metric.ntrip
Interface for objects that needs to be notified when new encoded messages are available.
MessageParser<T> - Interface in org.orekit.files.ccsds.utils.lexical
Parser for CCSDS messages.
MessagesParser - Class in org.orekit.gnss.metric.parser
Parser for IGS encoded messages.
MessagesParser(List<Integer>) - Constructor for class org.orekit.gnss.metric.parser.MessagesParser
Constructor.
MessageType - Interface in org.orekit.gnss.metric.parser
Interface for encoded message types.
MessageVersionXmlTokenBuilder - Class in org.orekit.files.ccsds.utils.lexical
Builder for the root element with CCSDS message version.
MessageVersionXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.utils.lexical.MessageVersionXmlTokenBuilder
 
MessageWriter<H extends Header,S extends Segment<?,?>,F extends NdmConstituent<H,S>> - Interface in org.orekit.files.ccsds.utils.generation
Interface for writing Navigation Data Message (NDM) files.
Metadata - Class in org.orekit.files.ccsds.section
This class gathers the meta-data present in the Navigation Data Message (ADM, ODM and TDM).
Metadata(TimeSystem) - Constructor for class org.orekit.files.ccsds.section.Metadata
Simple constructor.
MetadataKey - Enum in org.orekit.files.ccsds.section
Keys for NDM Metadata entries.
Meteo(SortedSet<CRD.MeteorologicalMeasurement>) - Constructor for class org.orekit.files.ilrs.CRD.Meteo
Constructor.
MeteorologicalConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
 
MeteorologicalMeasurement(AbsoluteDate, double, double, double) - Constructor for class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
Constructor.
metersToRu(TdmMetadata, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.tdm.IdentityConverter
Convert a range expressed in meters.
metersToRu(TdmMetadata, AbsoluteDate, double) - Method in interface org.orekit.files.ccsds.ndm.tdm.RangeUnitsConverter
Convert a range expressed in meters.
METRE - Static variable in class org.orekit.utils.units.Unit
Metre unit.
MF - Static variable in class org.orekit.models.earth.displacement.Tide
Mf tide.
MHZ_TO_HZ - Static variable in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Mega Hertz to Hertz converter.
MidpointIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for MidpointIntegrator.
MidpointIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.MidpointIntegratorBuilder
Build a new instance.
MILLI_ARC_SECONDS_TO_RADIANS - Static variable in class org.orekit.utils.units.UnitsConverter
Milli arcseconds to radians converter.
MILLI_SECONDS_TO_SECONDS - Static variable in class org.orekit.utils.units.UnitsConverter
Milli seconds to seconds converter.
MIN_EPOCH - Static variable in class org.orekit.time.DateComponents
Maximum supported date.
MINUTE - Static variable in class org.orekit.utils.units.Unit
Minute unit.
minuteDuration(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
Check length of the current minute in this time scale.
minuteDuration(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
Check length of the current minute in this time scale.
minuteDuration(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Check length of the current minute in this time scale.
minuteDuration(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
Check length of the current minute in this time scale.
minuteDuration(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Check length of the current minute in this time scale.
minuteDuration(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
Check length of the current minute in this time scale.
MINUTES_PER_DAY - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Time units per julian day.
minValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter minimum value has been changed.
missingCoefficientsAllowed() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Check if missing coefficients are allowed in the input data.
MM - Static variable in class org.orekit.gnss.metric.parser.Units
Millimetres units.
MM - Static variable in class org.orekit.models.earth.displacement.Tide
Mm tide.
MM_PER_S - Static variable in class org.orekit.gnss.metric.parser.Units
Millimetres per second units.
MM_PER_S2 - Static variable in class org.orekit.gnss.metric.parser.Units
Millimetres per square second units.
modelCalled(Orbit[], Map<ObservedMeasurement<?>, EstimatedMeasurement<?>>) - Method in interface org.orekit.estimation.leastsquares.ModelObserver
Notification callback for orbit changes.
ModelObserver - Interface in org.orekit.estimation.leastsquares
Observer for model calls.
MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for modified julian dates: 1858-11-17.
ModifiedFrame - Class in org.orekit.files.ccsds.definitions
A reference frame created from the REF_FRAME and CENTER_NAME is a CCSDS OPM, OMM, or OEM file.
ModifiedFrame(Frame, CelestialBodyFrame, CelestialBody, String) - Constructor for class org.orekit.files.ccsds.definitions.ModifiedFrame
Create a CCSDS reference frame by changing the origin of an existing frame.
ModifiedLambdaMethod - Class in org.orekit.estimation.measurements.gnss
Decorrelation/reduction engine for Modified LAMBDA method.
ModifiedLambdaMethod() - Constructor for class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
 
ModifierGradientConverter - Class in org.orekit.estimation.measurements.modifiers
Converter for states and parameters arrays.
ModifierGradientConverter(SpacecraftState, int, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.ModifierGradientConverter
Simple constructor.
modify(EstimatedMeasurement<T>) - Method in interface org.orekit.estimation.measurements.EstimationModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.gnss.WindUp
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier
 
modify(EstimatedMeasurement<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier
 
modify(EstimatedMeasurement<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
 
modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.Bias
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<BistaticRange>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeIonosphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<BistaticRangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeRateIonosphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<BistaticRangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeRateTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<BistaticRange>) - Method in class org.orekit.estimation.measurements.modifiers.BistaticRangeTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesPhaseModifier
 
modify(EstimatedMeasurement<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSPhaseModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaPhaseModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
 
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier
 
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>, ParametersDriversProvider, AbstractGradientConverter, GroundStation, ParametricModelEffect, ParametricModelEffectGradient) - Static method in class org.orekit.estimation.measurements.modifiers.RangeModifierUtil
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>, ParametersDriversProvider, AbstractGradientConverter, GroundStation, ParametricModelEffect, ParametricModelEffectGradient) - Static method in class org.orekit.estimation.measurements.modifiers.RangeRateModifierUtil
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesPhaseModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSPhaseModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockPhaseModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeRateModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesPhaseModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSPhaseModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockPhaseModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<TDOA>) - Method in class org.orekit.estimation.measurements.modifiers.TDOAIonosphericDelayModifier
 
modify(EstimatedMeasurement<TDOA>) - Method in class org.orekit.estimation.measurements.modifiers.TDOATroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier
 
modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier
Apply a modifier to an estimated measurement.
MOLECULAR_NITROGEN - Static variable in class org.orekit.models.earth.atmosphere.DTM2000
Identifier for molecular nitrogen.
MOLECULAR_OXYGEN - Static variable in class org.orekit.models.earth.atmosphere.DTM2000
Identifier for molecular oxygen.
monitorDetector(T) - Method in class org.orekit.propagation.events.EventsLogger
Monitor an event detector.
monitorDetector(D) - Method in class org.orekit.propagation.events.FieldEventsLogger
Monitor an event detector.
Month - Enum in org.orekit.time
Enumerate representing a calendar month.
MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Moon.
MOON_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Moon equatorial radius: 1737400 m.
mu(double) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Sets the Earth gravity coefficient.
MU - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Earth gravity coefficient in m³/s².
MultipleShooter - Class in org.orekit.utils
Multiple shooting method applicable for trajectories, in an ephemeris model.
MultipleShooter(List<SpacecraftState>, List<NumericalPropagator>, List<AdditionalEquations>, double, double) - Constructor for class org.orekit.utils.MultipleShooter
MultipleShooter(List<SpacecraftState>, List<NumericalPropagator>, List<EpochDerivativesEquations>, double, double, int) - Constructor for class org.orekit.utils.MultipleShooter
Simple Constructor.
MultipleShooting - Interface in org.orekit.utils
Interface for Multiple shooting methods.
MultiplexedMeasurement - Class in org.orekit.estimation.measurements
Class multiplexing several measurements as one.
MultiplexedMeasurement(List<ObservedMeasurement<?>>) - Constructor for class org.orekit.estimation.measurements.MultiplexedMeasurement
Simple constructor.
multiply(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Multiply the argument matrix with the current matrix.
multiply(String, Unit) - Method in class org.orekit.utils.units.Unit
Create product of units.
MultiSatStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step handler for multi-sat propagation.

N

N2 - Static variable in class org.orekit.models.earth.displacement.Tide
N₂ tide.
N_M - Static variable in class org.orekit.files.ccsds.definitions.Units
Newton metre unit.
NadirPointing - Class in org.orekit.attitudes
This class handles nadir pointing attitude provider.
NadirPointing(Frame, BodyShape) - Constructor for class org.orekit.attitudes.NadirPointing
Creates new instance.
nameChanged(String, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter name has been changed.
NANO_TESLA - Static variable in class org.orekit.files.ccsds.definitions.Units
Nano Tesla unit.
NarrowLaneCombination - Class in org.orekit.estimation.measurements.gnss
Narrow-Lane combination.
NAUTICAL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector
Sun elevation at nautical dawn/dusk (12° below horizon).
NavigationSystem - Enum in org.orekit.gnss.metric.ntrip
Enumerate for navigation system in DataStreamRecord.
NB_PER_Y - Static variable in class org.orekit.files.ccsds.definitions.Units
#/year unit.
Ndm - Class in org.orekit.files.ccsds.ndm
CCSDS Navigation Data Message.
Ndm(List<String>, List<NdmConstituent<?, ?>>) - Constructor for class org.orekit.files.ccsds.ndm.Ndm
Simple constructor.
NdmConstituent<H extends Header,S extends Segment<?,?>> - Class in org.orekit.files.ccsds.ndm
Constituents of a CCSDS Navigation Data Message.
NdmConstituent(H, List<S>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.NdmConstituent
Constructor.
NdmParser - Class in org.orekit.files.ccsds.ndm
A parser for the CCSDS NDM (Navigation Data Message).
NdmParser(ParserBuilder) - Constructor for class org.orekit.files.ccsds.ndm.NdmParser
Simple constructor.
NdmWriter - Class in org.orekit.files.ccsds.ndm
Writer for CCSDS Navigation Data Message.
NdmWriter(WriterBuilder) - Constructor for class org.orekit.files.ccsds.ndm.NdmWriter
Simple constructor.
negate() - Method in class org.orekit.utils.FieldPVCoordinates
Get the opposite of the instance.
negate() - Method in class org.orekit.utils.PVCoordinates
Get the opposite of the instance.
NegateDetector - Class in org.orekit.propagation.events
An event detector that negates the sign on another event detector's g function.
NegateDetector(EventDetector) - Constructor for class org.orekit.propagation.events.NegateDetector
Create a new event detector that negates an existing event detector.
NEPTUNE - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Neptune.
NeQuickModel - Class in org.orekit.models.earth.ionosphere
NeQuick ionospheric delay model.
NeQuickModel(double[]) - Constructor for class org.orekit.models.earth.ionosphere.NeQuickModel
Build a new instance.
NeQuickModel(double[], TimeScale) - Constructor for class org.orekit.models.earth.ionosphere.NeQuickModel
Build a new instance.
NetworkCrawler - Class in org.orekit.data
Provider for data files directly fetched from network.
NetworkCrawler(URL...) - Constructor for class org.orekit.data.NetworkCrawler
Build a data classpath crawler.
NetworkRecord - Class in org.orekit.gnss.metric.ntrip
Network record in source table.
NetworkRecord(String) - Constructor for class org.orekit.gnss.metric.ntrip.NetworkRecord
Build a data stream record by parsing a source table line.
newBulletinBParser(IERSConventions, ItrfVersionProvider, TimeScales) - Static method in interface org.orekit.frames.EOPHistoryLoader.Parser
Create a new parser for EOP data in the Bulletin B format.
newBundle(String, Locale, String, ClassLoader, boolean) - Method in class org.orekit.errors.OrekitMessages.UTF8Control
NewcombOperators - Class in org.orekit.propagation.semianalytical.dsst.utilities
Implementation of the Modified Newcomb Operators.
newEopC04Parser(IERSConventions, ItrfVersionProvider, TimeScales) - Static method in interface org.orekit.frames.EOPHistoryLoader.Parser
Create a new parser for EOP data in the EOP C04 format.
newFinalsColumnsParser(IERSConventions, ItrfVersionProvider, TimeScales, boolean) - Static method in interface org.orekit.frames.EOPHistoryLoader.Parser
Create a new parser for EOP data in the rapid and predicted columnar format.
newFinalsXmlParser(IERSConventions, ItrfVersionProvider, TimeScales) - Static method in interface org.orekit.frames.EOPHistoryLoader.Parser
Create a new parser for EOP data in the rapid and predicted XML format.
newLine() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Finish current line.
newLine() - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Finish current line.
newSegment() - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter
Create a writer for a new AEM attitude ephemeris segment.
newSegment() - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter
Create a writer for a new OEM ephemeris segment.
newSegment(Frame) - Method in class org.orekit.files.ilrs.StreamingCpfWriter
Create a writer for a new CPF ephemeris segment.
NEWTON - Static variable in class org.orekit.utils.units.Unit
Newton unit.
NewtonianAttraction - Class in org.orekit.forces.gravity
Force model for Newtonian central body attraction.
NewtonianAttraction(double) - Constructor for class org.orekit.forces.gravity.NewtonianAttraction
Simple constructor.
next() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the next time span.
next() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the next transition.
NiellMappingFunctionModel - Class in org.orekit.models.earth.troposphere
The Niell Mapping Function model for radio wavelengths.
NiellMappingFunctionModel() - Constructor for class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
Builds a new instance.
NiellMappingFunctionModel(TimeScale) - Constructor for class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
Builds a new instance.
NodeDetector - Class in org.orekit.propagation.events
Finder for node crossing events.
NodeDetector(Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Build a new instance.
NodeDetector(Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Build a new instance.
NodeDetector(double, Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Build a new instance.
nonCentralPart(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the non-central part of the gravity field.
NONE - Static variable in class org.orekit.utils.units.Unit
No unit.
normalize(FieldOrbit<T>, FieldOrbit<T>) - Method in enum org.orekit.orbits.OrbitType
Normalize one orbit with respect to a reference one.
normalize(Orbit, Orbit) - Method in enum org.orekit.orbits.OrbitType
Normalize one orbit with respect to a reference one.
normalize() - Method in class org.orekit.utils.FieldPVCoordinates
Normalize the position part of the instance.
normalize() - Method in class org.orekit.utils.PVCoordinates
Normalize the position part of the instance.
NORMALIZED_EQUATORIAL_RADIUS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Equatorial radius rescaled (1.0).
NormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide normalized spherical harmonics coefficients.
NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential
The normalized geopotential coefficients at a specific instance in time.
NORTH_POLE - Static variable in class org.orekit.bodies.GeodeticPoint
North pole.
notCombine(EventDetector) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that negates the g function of another detector.
notifyResetters(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Notify resetters.
notifyResetters(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Notify resetters.
NRLMSISE00 - Class in org.orekit.models.earth.atmosphere
This class implements the mathematical representation of the 2001 Naval Research Laboratory Mass Spectrometer and Incoherent Scatter Radar Exosphere (NRLMSISE-00) of the MSIS® class model.
NRLMSISE00(NRLMSISE00InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.models.earth.atmosphere.NRLMSISE00
Constructor.
NRLMSISE00(NRLMSISE00InputParameters, PVCoordinatesProvider, BodyShape, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.NRLMSISE00
Constructor.
NRLMSISE00.FieldOutput<T extends CalculusFieldElement<T>> - Class in org.orekit.models.earth.atmosphere
This class is a placeholder for the computed densities and temperatures.
NRLMSISE00InputParameters - Interface in org.orekit.models.earth.atmosphere
Container for solar activity data, compatible with NRLMSISE-00 atmosphere model.
NS - Static variable in class org.orekit.gnss.metric.parser.Units
Nanoseconds units.
NSKey(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
Simple constructor.
NtripClient - Class in org.orekit.gnss.metric.ntrip
Source table for ntrip streams retrieval.
NtripClient(String, int) - Constructor for class org.orekit.gnss.metric.ntrip.NtripClient
Build a client for NTRIP.
NULL_CORRECTION - Static variable in class org.orekit.frames.PoleCorrection
Null correction (xp = 0, yp = 0).
numberOfCandidates() - Method in interface org.orekit.estimation.measurements.gnss.AmbiguityAcceptance
Get the number of candidate solutions to search for.
numberOfCandidates() - Method in class org.orekit.estimation.measurements.gnss.SimpleRatioAmbiguityAcceptance
Get the number of candidate solutions to search for.
numberOfObsTypes(SatelliteSystem) - Method in class org.orekit.gnss.clock.RinexClock
Get the number of observation types for a given system.
NumericalPropagator - Class in org.orekit.propagation.numerical
This class propagates orbits using numerical integration.
NumericalPropagator(ODEIntegrator) - Constructor for class org.orekit.propagation.numerical.NumericalPropagator
Create a new instance of NumericalPropagator, based on orbit definition mu.
NumericalPropagator(ODEIntegrator, AttitudeProvider) - Constructor for class org.orekit.propagation.numerical.NumericalPropagator
Create a new instance of NumericalPropagator, based on orbit definition mu.
NumericalPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for numerical propagator.
NumericalPropagatorBuilder(Orbit, ODEIntegratorBuilder, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a new instance.
NumericalPropagatorBuilder(Orbit, ODEIntegratorBuilder, PositionAngle, double, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a new instance.

O

O1 - Static variable in class org.orekit.models.earth.displacement.Tide
O₁ tide.
ObjectType - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Object type used in CCSDS Orbit Comprehensive Messages.
ObservableSatellite - Class in org.orekit.estimation.measurements
Class modeling a satellite that can be observed.
ObservableSatellite(int) - Constructor for class org.orekit.estimation.measurements.ObservableSatellite
Simple constructor.
Observation - Class in org.orekit.files.ccsds.ndm.tdm
The Observation class contains the data from an observation line.
Observation(ObservationType, AbsoluteDate, double) - Constructor for class org.orekit.files.ccsds.ndm.tdm.Observation
Simple constructor.
ObservationData - Class in org.orekit.gnss
Observation Data.
ObservationData(ObservationType, double, int, int) - Constructor for class org.orekit.gnss.ObservationData
Simple constructor.
ObservationDataSet - Class in org.orekit.gnss
Observation Data set.
ObservationDataSet(RinexObservationHeader, SatelliteSystem, int, AbsoluteDate, double, List<ObservationData>) - Constructor for class org.orekit.gnss.ObservationDataSet
Simple constructor.
ObservationsBlock - Class in org.orekit.files.ccsds.ndm.tdm
The Observations Block class contain metadata and the list of observation data lines.
ObservationsBlock() - Constructor for class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock
ObservationsBlock constructor.
ObservationType - Enum in org.orekit.files.ccsds.ndm.tdm
Keys for TDM observations entries.
ObservationType - Enum in org.orekit.gnss
Enumerate for all the Observation Types for Rinex 2 and 3.
ObservedMeasurement<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements
Interface for measurements used for orbit determination.
OceanLoadDeformationCoefficients - Enum in org.orekit.forces.gravity.potential
Supported Ocean load Deformation coefficients (Love numbers k'i).
OceanLoading - Class in org.orekit.models.earth.displacement
Modeling of displacement of reference points due to ocean loading.
OceanLoading(OneAxisEllipsoid, OceanLoadingCoefficients) - Constructor for class org.orekit.models.earth.displacement.OceanLoading
Simple constructor.
OceanLoadingCoefficients - Class in org.orekit.models.earth.displacement
Site specific coefficients for ocean loading.
OceanLoadingCoefficients(String, GeodeticPoint, Tide[][], double[][], double[][], double[][], double[][], double[][], double[][]) - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Simple constructor.
OceanLoadingCoefficientsBLQFactory - Class in org.orekit.models.earth.displacement
Factory for ocean loading coefficients, using Onsala Space Observatory files in BLQ format.
OceanLoadingCoefficientsBLQFactory(String) - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Simple constructor.
OceanLoadingCoefficientsBLQFactory(String, DataProvidersManager) - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
This constructor allows specification of the source of the BLQ auxiliary data files.
OceanTides - Class in org.orekit.forces.gravity
Ocean tides force model.
OceanTides(Frame, double, double, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides
Simple constructor.
OceanTides(Frame, double, double, boolean, double, int, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides
Simple constructor.
OceanTides(Frame, double, double, boolean, double, int, int, int, IERSConventions, UT1Scale, GravityFields) - Constructor for class org.orekit.forces.gravity.OceanTides
Simple constructor.
OceanTidesReader - Class in org.orekit.forces.gravity.potential
Reader for ocean tides coefficients.
OceanTidesReader(String) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesReader
Simple constructor.
OceanTidesWave - Class in org.orekit.forces.gravity.potential
Container for ocen tides coefficients for one tide wave.
OceanTidesWave(int, int, int, double[][][]) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesWave
Simple constructor.
Ocm - Class in org.orekit.files.ccsds.ndm.odm.ocm
This class gathers the informations present in the Orbit Comprehensive Message (OCM).
Ocm(Header, List<Segment<OcmMetadata, OcmData>>, IERSConventions, DataContext, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Simple constructor.
OcmData - Class in org.orekit.files.ccsds.ndm.odm.ocm
Data container for Orbit Comprehensive Messages.
OcmData(List<TrajectoryStateHistory>, PhysicalProperties, List<CovarianceHistory>, List<ManeuverHistory>, Perturbations, OrbitDetermination, UserDefined) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Simple constructor.
OcmDataSubStructureKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Keywords for OCM data sub-structure.
OcmMetadata - Class in org.orekit.files.ccsds.ndm.odm.ocm
OcmMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Keys for OCM container entries.
OcmParser - Class in org.orekit.files.ccsds.ndm.odm.ocm
A parser for the CCSDS OCM (Orbit Comprehensive Message).
OcmParser(IERSConventions, boolean, DataContext, double, ParsedUnitsBehavior) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Complete constructor.
OcmSatelliteEphemeris - Class in org.orekit.files.ccsds.ndm.odm.ocm
OCM ephemeris blocks for a single satellite.
OcmSatelliteEphemeris(String, double, List<TrajectoryStateHistory>) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.
OcmWriter - Class in org.orekit.files.ccsds.ndm.odm.ocm
Writer for CCSDS Orbit Comprehensive Message.
OcmWriter(IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter
Complete constructor.
ODEIntegratorBuilder - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction to build first order integrators for propagators conversion.
OdMethodFacade - Class in org.orekit.files.ccsds.definitions
Facade in front of several orbit determination methods in CCSDS messages.
OdMethodFacade(String, OdMethodType, String) - Constructor for class org.orekit.files.ccsds.definitions.OdMethodFacade
Simple constructor.
OdMethodType - Enum in org.orekit.files.ccsds.definitions
Type of orbit determination method used in CCSDS Orbit Comprehensive Messages.
OdmMetadata - Class in org.orekit.files.ccsds.ndm.odm
This class gathers the meta-data present in the Orbital Data Message (ODM).
OdmMetadata(TimeSystem) - Constructor for class org.orekit.files.ccsds.ndm.odm.OdmMetadata
Simple constructor.
OdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm
Keys for ODM metadata entries.
OdmParser<T extends NdmConstituent<?,?>,P extends OdmParser<T,?>> - Class in org.orekit.files.ccsds.ndm.odm
Common parser for Orbit Parameter/Ephemeris/Mean/Comprehensive Messages.
OdmParser(String, String, IERSConventions, boolean, DataContext, AbsoluteDate, double, ParsedUnitsBehavior) - Constructor for class org.orekit.files.ccsds.ndm.odm.OdmParser
Complete constructor.
ODParameters - Class in org.orekit.files.ccsds.ndm.cdm
Container for OD parameters data block.
ODParameters() - Constructor for class org.orekit.files.ccsds.ndm.cdm.ODParameters
Simple constructor.
ODParametersKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM OD parameters entries.
ODParametersWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for OD parameters data block for CCSDS Conjunction Data Messages.
Oem - Class in org.orekit.files.ccsds.ndm.odm.oem
This class stores all the information of the OEM File parsed by OEMParser.
Oem(Header, List<OemSegment>, IERSConventions, DataContext, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.Oem
Simple constructor.
OemData - Class in org.orekit.files.ccsds.ndm.odm.oem
The Ephemerides data blocks class contain list of orbital data points.
OemData() - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemData
EphemeridesBlock constructor.
OemMetadata - Class in org.orekit.files.ccsds.ndm.odm.oem
Metadata for Orbit Ephemeris Messages.
OemMetadata(int) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Simple constructor.
OemMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.oem
Keys for OEM container entries.
OemParser - Class in org.orekit.files.ccsds.ndm.odm.oem
A parser for the CCSDS OEM (Orbit Ephemeris Message).
OemParser(IERSConventions, boolean, DataContext, AbsoluteDate, double, int, ParsedUnitsBehavior) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Complete constructor.
OemSatelliteEphemeris - Class in org.orekit.files.ccsds.ndm.odm.oem
OEM ephemeris blocks for a single satellite.
OemSatelliteEphemeris(String, double, List<OemSegment>) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.
OemSegment - Class in org.orekit.files.ccsds.ndm.odm.oem
The Ephemerides Blocks class contain metadata, the list of ephemerides data lines and optional covariance matrices (and their metadata).
OemSegment(OemMetadata, OemData, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
Simple constructor.
OemWriter - Class in org.orekit.files.ccsds.ndm.odm.oem
A writer for Orbit Ephemeris Message (OEM) files.
OemWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.OemWriter
Constructor used to create a new OEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
of(Frame) - Static method in class org.orekit.attitudes.InertialProvider
Creates an attitude provider aligned with the given frame.
of(TimeScales, CelestialBodies) - Static method in interface org.orekit.frames.Frames
Create a set of frames from the given data.
of(TimeScales, Supplier<Frame>) - Static method in interface org.orekit.frames.Frames
Create a set of frames from the given data.
of(AbsoluteDate, Rotation) - Static method in interface org.orekit.frames.StaticTransform
Create a new static transform from a rotation and zero translation.
of(AbsoluteDate, Vector3D) - Static method in interface org.orekit.frames.StaticTransform
Create a new static transform from a translation and rotation.
of(AbsoluteDate, Vector3D, Rotation) - Static method in interface org.orekit.frames.StaticTransform
Create a new static transform from a translation and rotation.
of(Collection<? extends OffsetModel>, BiFunction<? super IERSConventions, ? super TimeScales, ? extends Collection<? extends EOPEntry>>) - Static method in interface org.orekit.time.TimeScales
Create a set of time scales where all the data is loaded from the given functions.
offset(AbsoluteDate) - Method in class org.orekit.files.ccsds.definitions.TimeConverter
Generate relative offset.
OFFSET_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation
Suffix for ground station position and clock offset parameters names.
offsetFrom(AbsoluteDate, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Compute the apparent clock offset between two instant in the perspective of a specific time scale.
offsetFrom(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents
Compute the seconds offset between two instances.
offsetFrom(FieldAbsoluteDate<T>, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the apparent clock offset between two instant in the perspective of a specific time scale.
offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in class org.orekit.geometry.fov.CircularFieldOfView
Get the offset of target body with respect to the Field Of View Boundary.
offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Get the offset of target body with respect to the Field Of View Boundary.
offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in interface org.orekit.geometry.fov.FieldOfView
Get the offset of target body with respect to the Field Of View Boundary.
offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView
Get the offset of target body with respect to the Field Of View Boundary.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.BDTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.BDTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GalileoScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GalileoScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GMSTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GMSTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GPSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GPSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.IRNSSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.IRNSSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.QZSSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.QZSSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.SatelliteClockScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.SatelliteClockScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TAIScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TAIScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TCBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCGScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TCGScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TDBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TDBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UT1Scale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UT1Scale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
Get the offset to convert locations from TAIScale to instance.
OffsetModel - Class in org.orekit.time
TAI UTC offset model.
OffsetModel(DateComponents, int, double, double) - Constructor for class org.orekit.time.OffsetModel
Constructor for a linear offset model.
OffsetModel(DateComponents, int) - Constructor for class org.orekit.time.OffsetModel
Constructor for a constant offset model.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.BDTScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GalileoScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GLONASSScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GPSScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.IRNSSScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.QZSSScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.SatelliteClockScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TAIScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in interface org.orekit.time.TimeScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TTScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.UTCScale
Get the offset to convert locations from instance to TAIScale.
OHM - Static variable in class org.orekit.utils.units.Unit
Ohm unit.
omega - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
final perigee argument.
omega - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final perigee argument.
omgdot - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
common parameter for perigee argument (omega) computation.
omgdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for perigee argument (omega) computation.
Omm - Class in org.orekit.files.ccsds.ndm.odm.omm
This class gathers the informations present in the Orbital Mean-Elements Message (OMM).
Omm(Header, List<Segment<OmmMetadata, OmmData>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.Omm
Simple constructor.
OmmData - Class in org.orekit.files.ccsds.ndm.odm.omm
Container for Orbit Mean-elements Message data.
OmmData(KeplerianElements, SpacecraftParameters, OmmTle, CartesianCovariance, UserDefined, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Simple constructor.
OmmMetadata - Class in org.orekit.files.ccsds.ndm.odm.omm
 
OmmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
 
OmmMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.omm
Keys for OMM container entries.
OmmParser - Class in org.orekit.files.ccsds.ndm.odm.omm
A parser for the CCSDS OMM (Orbiter Mean-Elements Message).
OmmParser(IERSConventions, boolean, DataContext, AbsoluteDate, double, double, ParsedUnitsBehavior) - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Complete constructor.
OmmTle - Class in org.orekit.files.ccsds.ndm.odm.omm
Container for TLE data.
OmmTle() - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Create an empty data set.
OmmTleKey - Enum in org.orekit.files.ccsds.ndm.odm.omm
Keys for TLE entries.
OmmWriter - Class in org.orekit.files.ccsds.ndm.odm.omm
Writer for CCSDS Orbit Mean Mean-Elements Message.
OmmWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.omm.OmmWriter
Complete constructor.
OnBoardAntennaInterSatellitesPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on inter-satellites phase measurements.
OnBoardAntennaInterSatellitesPhaseModifier(Vector3D, Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesPhaseModifier
Simple constructor.
OnBoardAntennaInterSatellitesRangeModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on inter-satellites range measurements.
OnBoardAntennaInterSatellitesRangeModifier(Vector3D, Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier
Simple constructor.
OnBoardAntennaOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on one-way GNSS phase measurements.
OnBoardAntennaOneWayGNSSPhaseModifier(Vector3D, Vector3D, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSPhaseModifier
Simple constructor.
OnBoardAntennaOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on one-way GNSS range measurements.
OnBoardAntennaOneWayGNSSRangeModifier(Vector3D, Vector3D, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSRangeModifier
Simple constructor.
OnBoardAntennaPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on phase measurements.
OnBoardAntennaPhaseModifier(Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaPhaseModifier
Simple constructor.
OnBoardAntennaRangeModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on range measurements.
OnBoardAntennaRangeModifier(Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaRangeModifier
Simple constructor.
OnBoardAntennaTurnAroundRangeModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on turn around range measurements.
OnBoardAntennaTurnAroundRangeModifier(Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier
Simple constructor.
onDate(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the normalized spherical harmonic coefficients at a specific instance in time.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider
Get the normalized spherical harmonic coefficients at a specific instance in time.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider
Get the raw spherical harmonic coefficients on a specific date.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider
Get the un-normalized spherical harmonic coefficients at a specific instance in time.
ONE - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
1 represented as a polynomial.
ONE - Static variable in class org.orekit.utils.units.Unit
Dimensionless unit.
ONE_PER_ER - Static variable in class org.orekit.files.ccsds.definitions.Units
Earth radii reciprocal unit.
ONE_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units
Seconds reciprocal unit.
ONE_THIRD - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Constant 1.0 / 3.0.
OneAxisEllipsoid - Class in org.orekit.bodies
Modeling of a one-axis ellipsoid.
OneAxisEllipsoid(double, double, Frame) - Constructor for class org.orekit.bodies.OneAxisEllipsoid
Simple constructor.
OneWayGNSSPhase - Class in org.orekit.estimation.measurements.gnss
One-way GNSS phase measurement.
OneWayGNSSPhase(PVCoordinatesProvider, double, AbsoluteDate, double, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
Simple constructor.
OneWayGNSSPhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical one-way GNSS phase measurement with ambiguity.
OneWayGNSSPhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier
Constructor.
OneWayGNSSRange - Class in org.orekit.estimation.measurements.gnss
One-way GNSS range measurement.
OneWayGNSSRange(PVCoordinatesProvider, double, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.OneWayGNSSRange
Simple constructor.
OnOff - Enum in org.orekit.files.ccsds.definitions
On/Off status for various elements.
ooA - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
1 / A .
ooA - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
1 / A .
ooAB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
1 / (A * B) .
ooAB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
1 / (A * B) .
ooBpo - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
1 / (1 + B) .
ooBpo - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
1 / (1 + B) .
ooMu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
1 / μ .
ooMu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
1 / μ .
openOnce() - Method in interface org.orekit.data.DataSource.ReaderOpener
Open the stream once.
openOnce() - Method in interface org.orekit.data.DataSource.StreamOpener
Open the stream once.
openReaderOnce() - Method in interface org.orekit.data.DataSource.Opener
Open a characters stream reader once.
openStreamOnce() - Method in interface org.orekit.data.DataSource.Opener
Open a bytes stream once.
Opm - Class in org.orekit.files.ccsds.ndm.odm.opm
This class gathers the informations present in the Orbital Parameter Message (OPM).
Opm(Header, List<Segment<CommonMetadata, OpmData>>, IERSConventions, DataContext, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.Opm
Simple constructor.
OpmData - Class in org.orekit.files.ccsds.ndm.odm.opm
Container for Orbit Parameter Message data.
OpmData(StateVector, KeplerianElements, SpacecraftParameters, CartesianCovariance, List<Maneuver>, UserDefined, double) - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Simple constructor.
OpmParser - Class in org.orekit.files.ccsds.ndm.odm.opm
A parser for the CCSDS OPM (Orbit Parameter Message).
OpmParser(IERSConventions, boolean, DataContext, AbsoluteDate, double, double, ParsedUnitsBehavior) - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Complete constructor.
OpmWriter - Class in org.orekit.files.ccsds.ndm.odm.opm
Writer for CCSDS Orbit Parameter Message.
OpmWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.OpmWriter
Complete constructor.
OpsStatus - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Operational status used in CCSDS Orbit Comprehensive Messages.
Orbit - Class in org.orekit.orbits
This class handles orbital parameters.
Orbit(Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.Orbit
Default constructor.
Orbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.Orbit
Set the orbit from Cartesian parameters.
OrbitCategory - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Orbit category used in CCSDS Orbit Comprehensive Messages.
OrbitCorrection - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR orbit correction data.
OrbitCorrection(double, double, double, double, double, double) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection
Constructor.
OrbitDetermination - Class in org.orekit.files.ccsds.ndm.odm.ocm
Orbit determination data.
OrbitDeterminationKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Keys for orbit determination data entries.
OrbitDeterminationPropagatorBuilder - Interface in org.orekit.propagation.conversion
Base class for orbit determination model builders.
OrbitRelativeFrame - Enum in org.orekit.files.ccsds.definitions
Frames used in CCSDS Orbit Data Messages.
OrbitType - Enum in org.orekit.orbits
Enumerate for orbital parameters types.
orCombine(EventDetector...) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical OR of the given event detectors.
orCombine(Collection<? extends EventDetector>) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical OR of the given event detectors.
Ordering - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Keys for Covariance elements ordering.
OREKIT_DATA_PATH - Static variable in class org.orekit.data.DataProvidersManager
Name of the property defining the root directories or zip/jar files path for default configuration.
OrekitAttitudeEphemerisFile - Class in org.orekit.files.general
A class for encapsulating Orekit propagators within an AttitudeEphemerisFile complaint object that makes for easy serialization to external ephemeris formats like AEM.
OrekitAttitudeEphemerisFile() - Constructor for class org.orekit.files.general.OrekitAttitudeEphemerisFile
Standard default constructor.
OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment - Class in org.orekit.files.general
 
OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris - Class in org.orekit.files.general
Inner class of OrekitAttitudeEphemerisFile that defines the OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris corresponding object for this ephemeris type.
OrekitAttitudeEphemerisSegment(List<TimeStampedAngularCoordinates>, String, int, Frame, AngularDerivativesFilter) - Constructor for class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
Constructor for OrekitAttitudeEphemerisSegment.
OrekitConfiguration - Class in org.orekit.utils
Utility class for setting global configuration parameters.
OrekitEphemerisFile - Class in org.orekit.files.general
A class for encapsulating Orekit propagators within an EphemerisFile complaint object that makes for easy serialization to external ephemeris formats like OEM.
OrekitEphemerisFile() - Constructor for class org.orekit.files.general.OrekitEphemerisFile
Standard default constructor.
OrekitEphemerisFile.OrekitEphemerisSegment - Class in org.orekit.files.general
 
OrekitEphemerisFile.OrekitSatelliteEphemeris - Class in org.orekit.files.general
Inner class of OrekitEphemerisFile that defines the OrekitEphemerisFile.OrekitSatelliteEphemeris corresponding object for this ephemeris type.
OrekitEphemerisSegment(List<TimeStampedPVCoordinates>, Frame, double, int) - Constructor for class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
constructor for OrekitEphemerisSegment.
OrekitException - Exception in org.orekit.errors
This class is the base class for all specific exceptions thrown by the Orekit classes.
OrekitException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(OrekitException) - Constructor for exception org.orekit.errors.OrekitException
Copy constructor.
OrekitException(Localizable, Throwable) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(MathRuntimeException) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitFixedStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware fixed size step handler.
OrekitIllegalArgumentException - Exception in org.orekit.errors
Extension of IllegalArgumentException with localized message.
OrekitIllegalArgumentException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIllegalArgumentException
Create an exception with localized message.
OrekitIllegalStateException - Exception in org.orekit.errors
Extension of IllegalStateException with localized message.
OrekitIllegalStateException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIllegalStateException
Create an exception with localized message.
OrekitInternalError - Exception in org.orekit.errors
Extension of Runtime with localized message for internal errors only.
OrekitInternalError(Throwable) - Constructor for exception org.orekit.errors.OrekitInternalError
Create an exception with localized message.
OrekitIOException - Exception in org.orekit.errors
Extension of IOException with localized message.
OrekitIOException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIOException
Create an exception with localized message.
OrekitMessages - Enum in org.orekit.errors
Enumeration for localized messages formats.
OrekitMessages.UTF8Control - Class in org.orekit.errors
Control class loading properties in UTF-8 encoding.
OrekitParseException - Exception in org.orekit.errors
Extension of ParseException with localized message.
OrekitParseException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitParseException
Create an exception with localized message.
OrekitSatelliteAttitudeEphemeris(String) - Constructor for class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Standard constructor for building the satellite Ephemeris object.
OrekitSatelliteEphemeris(String) - Constructor for class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Standard constructor for building the satellite Ephemeris object.
OrekitStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step handler.
OrekitStepInterpolator - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step interpolator.
OrekitStepNormalizer - Class in org.orekit.propagation.sampling
This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.
OrekitStepNormalizer(double, OrekitFixedStepHandler) - Constructor for class org.orekit.propagation.sampling.OrekitStepNormalizer
Simple constructor.
org.orekit.annotation - package org.orekit.annotation
This package is the top level package for Orekit's specific annotations.
org.orekit.attitudes - package org.orekit.attitudes
This package provides classes to represent simple attitudes.
org.orekit.bodies - package org.orekit.bodies
This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.
org.orekit.compiler.plugin - package org.orekit.compiler.plugin
This package provides elements to handle data context plugin.
org.orekit.data - package org.orekit.data
This package provide base classes for exploring the configured data directory tree and read external data that can be used by the library.
org.orekit.errors - package org.orekit.errors
This package provides classes to generate and handle exceptions.
org.orekit.estimation - package org.orekit.estimation
This package is the top level package for orbit determination.
org.orekit.estimation.iod - package org.orekit.estimation.iod
This package provides initial orbit determination methods.
org.orekit.estimation.leastsquares - package org.orekit.estimation.leastsquares
The leastsquares package provides an implementation of a batch least squares estimator engine to perform an orbit determination.
org.orekit.estimation.measurements - package org.orekit.estimation.measurements
The measurements package defines everything that is related to orbit determination measurements.
org.orekit.estimation.measurements.filtering - package org.orekit.estimation.measurements.filtering
This package provides measurement pre-processing filters.
org.orekit.estimation.measurements.generation - package org.orekit.estimation.measurements.generation
This package provides Orbit Determination measurements generation.
org.orekit.estimation.measurements.gnss - package org.orekit.estimation.measurements.gnss
This package provides methods to handle GNSS measurements.
org.orekit.estimation.measurements.modifiers - package org.orekit.estimation.measurements.modifiers
This package provides measurement modifier.
org.orekit.estimation.sequential - package org.orekit.estimation.sequential
The sequential package provides an implementation of a Kalman Filter engine to perform an orbit determination.
org.orekit.files - package org.orekit.files
Top level package for various parsers.
org.orekit.files.ccsds - package org.orekit.files.ccsds
This package is gathers sub-packages providing parsers/writers for various CCSDS messages.
org.orekit.files.ccsds.definitions - package org.orekit.files.ccsds.definitions
This package contains definitions for CCSDS objects (frames, time systems...).
org.orekit.files.ccsds.ndm - package org.orekit.files.ccsds.ndm
This package contains the base hierarchy for CCSDS ADM, ODM and TDM.
org.orekit.files.ccsds.ndm.adm - package org.orekit.files.ccsds.ndm.adm
This package contains class managing CCSDS Attitude Data Message.
org.orekit.files.ccsds.ndm.adm.aem - package org.orekit.files.ccsds.ndm.adm.aem
This package contains class managing CCSDS Attitude Ephemeris Message.
org.orekit.files.ccsds.ndm.adm.apm - package org.orekit.files.ccsds.ndm.adm.apm
This package contains class managing CCSDS Attitude Parameter Message.
org.orekit.files.ccsds.ndm.cdm - package org.orekit.files.ccsds.ndm.cdm
This package contains class managing CCSDS Conjunction Data Message.
org.orekit.files.ccsds.ndm.odm - package org.orekit.files.ccsds.ndm.odm
This package contains class managing CCSDS Orbit Data Message.
org.orekit.files.ccsds.ndm.odm.ocm - package org.orekit.files.ccsds.ndm.odm.ocm
This package contains class managing CCSDS Orbit Comprehensive Message.
org.orekit.files.ccsds.ndm.odm.oem - package org.orekit.files.ccsds.ndm.odm.oem
This package contains class managing CCSDS Orbit Ephemeris Message.
org.orekit.files.ccsds.ndm.odm.omm - package org.orekit.files.ccsds.ndm.odm.omm
This package contains class managing CCSDS Orbit Mean-Elements Message.
org.orekit.files.ccsds.ndm.odm.opm - package org.orekit.files.ccsds.ndm.odm.opm
This package contains class managing CCSDS Orbit Parameter Message.
org.orekit.files.ccsds.ndm.tdm - package org.orekit.files.ccsds.ndm.tdm
This package contains class managing CCSDS Tracking Data Message.
org.orekit.files.ccsds.section - package org.orekit.files.ccsds.section
This package contains class managing the sections in CCSDS Messages.
org.orekit.files.ccsds.utils - package org.orekit.files.ccsds.utils
This package contains utilities shared by many CCSDS messages parsers/writers.
org.orekit.files.ccsds.utils.generation - package org.orekit.files.ccsds.utils.generation
This package contains utilities for CCSDS messages generation.
org.orekit.files.ccsds.utils.lexical - package org.orekit.files.ccsds.utils.lexical
This package contains utilities for CCSDS messages lexical analysis.
org.orekit.files.ccsds.utils.parsing - package org.orekit.files.ccsds.utils.parsing
This package contains classes related to the processing of parse tokens using the state design pattern.
org.orekit.files.general - package org.orekit.files.general
This package provides interfaces for orbit file representations and corresponding parsers.
org.orekit.files.ilrs - package org.orekit.files.ilrs
This package provides parsers for laser ranging data stored in CDR and CPF formats.
org.orekit.files.sinex - package org.orekit.files.sinex
This package provides classes related to station data.
org.orekit.files.sp3 - package org.orekit.files.sp3
This package provides a parser for orbit data stored in SP3 format.
org.orekit.forces - package org.orekit.forces
This package provides the interface for force models that will be used by the NumericalPropagator, as well as some classical spacecraft models for surface forces (spherical, box and solar array ...).
org.orekit.forces.drag - package org.orekit.forces.drag
This package provides all drag-related forces.
org.orekit.forces.empirical - package org.orekit.forces.empirical
This package provides empirical forces.
org.orekit.forces.gravity - package org.orekit.forces.gravity
This package provides all gravity-related forces.
org.orekit.forces.gravity.potential - package org.orekit.forces.gravity.potential
This package provides classes to read gravity field files and supports several different formats.
org.orekit.forces.inertia - package org.orekit.forces.inertia
This package provides inertial force model.
org.orekit.forces.maneuvers - package org.orekit.forces.maneuvers
This package provides models of simple maneuvers.
org.orekit.forces.maneuvers.jacobians - package org.orekit.forces.maneuvers.jacobians
Generators for columns of Jacobian matrices related to maneuver parameters.
org.orekit.forces.maneuvers.propulsion - package org.orekit.forces.maneuvers.propulsion
This package provides propulsion models intended to be used with class Maneuver.
org.orekit.forces.maneuvers.trigger - package org.orekit.forces.maneuvers.trigger
This package provides maneuver triggers' models intended to be used with class Maneuver.
org.orekit.forces.radiation - package org.orekit.forces.radiation
This package provides all radiation pressure related forces.
org.orekit.frames - package org.orekit.frames
This package provides classes to handle frames and transforms between them.
org.orekit.geometry.fov - package org.orekit.geometry.fov
This package provides classes for representing a spacecraft sensor Field Of View.
org.orekit.gnss - package org.orekit.gnss
This package provides classes related to GNSS applications.
org.orekit.gnss.antenna - package org.orekit.gnss.antenna
This package provides classes related to receiver and satellites antenna modeling.
org.orekit.gnss.attitude - package org.orekit.gnss.attitude
This package provides classes related to navigation satellites attitude modeling.
org.orekit.gnss.clock - package org.orekit.gnss.clock
This package provides classes related to navigation clock files.
org.orekit.gnss.metric - package org.orekit.gnss.metric
This package provides classes related to IGS binary formats.
org.orekit.gnss.metric.messages - package org.orekit.gnss.metric.messages
This package provides all supported IGS binary messages.
org.orekit.gnss.metric.messages.rtcm - package org.orekit.gnss.metric.messages.rtcm
This package provides all supported RTCM messages.
org.orekit.gnss.metric.messages.rtcm.ephemeris - package org.orekit.gnss.metric.messages.rtcm.ephemeris
This package provides all supported RTCM ephemeris messages.
org.orekit.gnss.metric.messages.rtcm.ephemeris.utils - package org.orekit.gnss.metric.messages.rtcm.ephemeris.utils
This package contains utility classes relate to RTCM ephemeris messages.
org.orekit.gnss.metric.messages.ssr - package org.orekit.gnss.metric.messages.ssr
This package provides all supported IGS SSR messages.
org.orekit.gnss.metric.messages.ssr.igm - package org.orekit.gnss.metric.messages.ssr.igm
This package provides all supported IGS Generic SSR Message types.
org.orekit.gnss.metric.messages.ssr.subtype - package org.orekit.gnss.metric.messages.ssr.subtype
This package provides all supported IGS SSR Sub-Type Message.
org.orekit.gnss.metric.ntrip - package org.orekit.gnss.metric.ntrip
This package provides streams reading from ntrip casters.
org.orekit.gnss.metric.parser - package org.orekit.gnss.metric.parser
This package provides the top level MessagesParser class that can extract messages from binary containers like ByteArrayEncodedMessages or {link org.orekit.metric.gnss.ssr.parser.InputStreamEncodedMessages InputStreamEncodedMessages}.
org.orekit.gnss.navigation - package org.orekit.gnss.navigation
This package provides classes related to RINEX navigation files.
org.orekit.models - package org.orekit.models
Top level package for physical models.
org.orekit.models.earth - package org.orekit.models.earth
This package provides models that simulate certain physical phenomena of Earth and the near-Earth environment.
org.orekit.models.earth.atmosphere - package org.orekit.models.earth.atmosphere
This package provides the atmosphere model interface and several implementations.
org.orekit.models.earth.atmosphere.data - package org.orekit.models.earth.atmosphere.data
This package provides classes to get atmospheric data, including solar flux and planetary geomagnetic indices.
org.orekit.models.earth.displacement - package org.orekit.models.earth.displacement
This package provides models computing reference points displacements on Earth surface.
org.orekit.models.earth.ionosphere - package org.orekit.models.earth.ionosphere
This package provides models that simulate the impact of the ionosphere.
org.orekit.models.earth.tessellation - package org.orekit.models.earth.tessellation
This package provides ways to do tessellation and sampling of zones of interest over an ellipsoid surface.
org.orekit.models.earth.troposphere - package org.orekit.models.earth.troposphere
This package provides models that simulate the impact of the troposphere.
org.orekit.models.earth.weather - package org.orekit.models.earth.weather
This package provides models that simulate global weather conditions on Earth.
org.orekit.orbits - package org.orekit.orbits
This package provides classes to represent orbits.
org.orekit.propagation - package org.orekit.propagation
Propagation
org.orekit.propagation.analytical - package org.orekit.propagation.analytical
Top level package for analytical propagators.
org.orekit.propagation.analytical.gnss - package org.orekit.propagation.analytical.gnss
This package provides classes to propagate GNSS orbits.
org.orekit.propagation.analytical.gnss.data - package org.orekit.propagation.analytical.gnss.data
This package provides classes related to navigation data containing in GNSS almanacs and navigation messages.
org.orekit.propagation.analytical.tle - package org.orekit.propagation.analytical.tle
This package provides classes to read and extrapolate tle's.
org.orekit.propagation.conversion - package org.orekit.propagation.conversion
This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.events - package org.orekit.propagation.events
This package provides interfaces and classes dealing with events occurring during propagation.
org.orekit.propagation.events.handlers - package org.orekit.propagation.events.handlers
This package provides an interface and classes dealing with events occurrence only.
org.orekit.propagation.integration - package org.orekit.propagation.integration
Utilities for integration-based propagators (both numerical and semi-analytical).
org.orekit.propagation.numerical - package org.orekit.propagation.numerical
Top level package for numerical propagators.
org.orekit.propagation.numerical.cr3bp - package org.orekit.propagation.numerical.cr3bp
Top level package for CR3BP Models used with a numerical propagator.
org.orekit.propagation.sampling - package org.orekit.propagation.sampling
This package provides interfaces and classes dealing with step handling during propagation.
org.orekit.propagation.semianalytical - package org.orekit.propagation.semianalytical
Top level package for semi-analytical propagators.
org.orekit.propagation.semianalytical.dsst - package org.orekit.propagation.semianalytical.dsst
This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.forces - package org.orekit.propagation.semianalytical.dsst.forces
This package provides force models for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.utilities - package org.orekit.propagation.semianalytical.dsst.utilities
This package provides utilities for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.utilities.hansen - package org.orekit.propagation.semianalytical.dsst.utilities.hansen
This package provides Hansen coefficient related utilities for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.time - package org.orekit.time
This independent package provides classes to handle epochs, time scales, and to compare instants together.
org.orekit.utils - package org.orekit.utils
This package provides useful objects.
org.orekit.utils.units - package org.orekit.utils.units
This package provides very basic handling of units.
OrphanFrame - Class in org.orekit.frames
Prototype frame that can be built from leaf to roots and later attached to a tree.
OrphanFrame(String) - Constructor for class org.orekit.frames.OrphanFrame
Simple constructor.
osculatingDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic
Get fitted osculating derivative.
osculatingSecondDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic
Get fitted osculating second derivative.
OsculatingToMeanElementsConverter - Class in org.orekit.propagation.conversion
This class converts osculating orbital elements into mean elements.
OsculatingToMeanElementsConverter(SpacecraftState, int, Propagator, double) - Constructor for class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter
Constructor.
osculatingValue(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic
Get fitted osculating value.
OutlierFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.
OutlierFilter(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.OutlierFilter
Simple constructor.
outputField(TimeConverter, Maneuver) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Output one maneuver field.

P

P1 - Static variable in class org.orekit.models.earth.displacement.Tide
P₁ tide.
PA - Static variable in enum org.orekit.orbits.OrbitType
Name for perigee argument.
ParameterDrivenDateIntervalDetector - Class in org.orekit.propagation.events
Detector for date intervals that may be offset thanks to parameter drivers.
ParameterDrivenDateIntervalDetector(String, AbsoluteDate, double) - Constructor for class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Build a new instance.
ParameterDrivenDateIntervalDetector(String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Build a new instance.
ParameterDriver - Class in org.orekit.utils
Class allowing to drive the value of a parameter.
ParameterDriver(String, double, double, double, double) - Constructor for class org.orekit.utils.ParameterDriver
Simple constructor.
ParameterDriversList - Class in org.orekit.utils
Class managing several parameter drivers, taking care of duplicated names.
ParameterDriversList() - Constructor for class org.orekit.utils.ParameterDriversList
Creates an empty list.
ParameterDriversList.DelegatingDriver - Class in org.orekit.utils
Specialized driver delegating to several other managing the same parameter name.
ParameterFunction - Interface in org.orekit.utils
Interface representing a scalar function depending on a ParameterDriver.
ParameterObserver - Interface in org.orekit.utils
Interface for observing parameters changes.
ParametersDriversProvider - Interface in org.orekit.utils
Provider for parameters drivers.
ParametricAcceleration - Class in org.orekit.forces.empirical
This class implements a parametric acceleration.
ParametricAcceleration(Vector3D, boolean, AccelerationModel) - Constructor for class org.orekit.forces.empirical.ParametricAcceleration
Simple constructor.
ParametricAcceleration(Vector3D, AttitudeProvider, AccelerationModel) - Constructor for class org.orekit.forces.empirical.ParametricAcceleration
Simple constructor.
parse(InputStream, String) - Method in class org.orekit.data.PoissonSeriesParser
Parse a stream.
parse(String) - Method in class org.orekit.data.PolynomialParser
Parse a polynomial expression.
parse(InputStream, String) - Method in class org.orekit.data.SimpleTimeStampedTableParser
Parse a stream.
parse(String) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
Parse a CCSDS frame.
parse(String, IERSConventions, boolean, DataContext, boolean, boolean, boolean) - Static method in class org.orekit.files.ccsds.definitions.FrameFacade
Simple constructor.
parse(String) - Static method in class org.orekit.files.ccsds.definitions.OdMethodFacade
Parse a string from OCM.
parse(String) - Static method in class org.orekit.files.ccsds.definitions.PocMethodFacade
Parse a string from CDM.
parse(String) - Static method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame
Build an instance from a normalized descriptor.
parse(String) - Method in class org.orekit.files.ccsds.definitions.TimeConverter
Parse a relative or absolute date.
parse(String) - Static method in enum org.orekit.files.ccsds.definitions.TimeSystem
Parse a value from a key=value entry.
parse(DataSource) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Parse an attitude ephemeris file from a data source.
parse(boolean, boolean, RotationOrder, boolean, ContextBinding, String[]) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Get the angular coordinates corresponding to the attitude data.
parse(DataSource) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Parse an ephemeris file from a data source.
parse(DataSource) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Parse an ephemeris file from a data source.
parse(DataSource) - Method in interface org.orekit.files.general.AttitudeEphemerisFileParser
Parse an attitude ephemeris file from a data source.
parse(DataSource) - Method in interface org.orekit.files.general.EphemerisFileParser
Parse an ephemeris file from a data source.
parse(DataSource) - Method in class org.orekit.files.ilrs.CPFParser
Parse an ephemeris file from a data source.
parse(DataSource) - Method in class org.orekit.files.ilrs.CRDParser
Parse a CRD file.
parse(DataSource) - Method in class org.orekit.files.sp3.SP3Parser
 
parse(InputStream, String) - Method in interface org.orekit.frames.EOPHistoryLoader.Parser
Parse EOP from the given input stream.
parse(InputStream) - Method in class org.orekit.gnss.clock.RinexClockParser
Parse an IGS clock file from an input stream using the UTF-8 charset.
parse(String) - Method in class org.orekit.gnss.clock.RinexClockParser
Parse an IGS clock file from a file on the local file system.
parse(BufferedReader, String) - Method in class org.orekit.gnss.clock.RinexClockParser
Parse an IGS clock file from a stream.
parse(EncodedMessage, boolean) - Method in class org.orekit.gnss.metric.parser.MessagesParser
Parse one message.
parse(EncodedMessage, int) - Method in interface org.orekit.gnss.metric.parser.MessageType
Parse an encoded message.
parse(DataSource) - Method in class org.orekit.gnss.navigation.RinexNavigationParser
Parse RINEX navigation messages.
parse(InputStream, String) - Method in class org.orekit.time.AGILeapSecondFilesLoader.Parser
Load UTC-TAI offsets entries read from some file.
parse(InputStream, String) - Method in class org.orekit.time.TAIUTCDatFilesLoader.Parser
Load UTC-TAI offsets entries read from some file.
parse(InputStream, String) - Method in class org.orekit.time.UTCTAIHistoryFilesLoader.Parser
Load UTC-TAI offsets entries read from some file.
parse(InputStream, String) - Method in interface org.orekit.time.UTCTAIOffsetsLoader.Parser
Parse leap seconds from the input stream.
parse(String) - Static method in class org.orekit.utils.units.Unit
Parse a unit.
parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSCalendarSegmentedTimeCode(byte, byte[], TimeScale) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSCalendarSegmentedTimeCode(byte, byte[], TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSDaySegmentedTimeCode(byte, byte[], DateComponents) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSDaySegmentedTimeCode(byte, byte[], DateComponents, TimeScale) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSDaySegmentedTimeCode(Field<T>, byte, byte[], DateComponents) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSDaySegmentedTimeCode(Field<T>, byte, byte[], DateComponents, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSUnsegmentedTimeCode(byte, byte, byte[], AbsoluteDate) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseCCSDSUnsegmentedTimeCode(byte, byte, byte[], AbsoluteDate, AbsoluteDate) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseCCSDSUnsegmentedTimeCode(Field<T>, byte, byte, byte[], FieldAbsoluteDate<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseCCSDSUnsegmentedTimeCode(Field<T>, byte, byte, byte[], FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseClockDataType(String) - Static method in enum org.orekit.gnss.clock.RinexClock.ClockDataType
Parse a string to get the time system.
parseCoefficient(String, List<List<Double>>, int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
parseCoefficient(String, double[][], int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
parseCoefficient(String, Flattener, double[], int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Parse a coefficient.
parseDate(String) - Static method in class org.orekit.time.DateComponents
Parse a string in ISO-8601 format to build a date.
parseDateTime(String) - Static method in class org.orekit.time.DateTimeComponents
Parse a string in ISO-8601 format to build a date/time.
ParsedMessage - Class in org.orekit.gnss.metric.messages
Abstract base class for decoded IGS messages.
ParsedMessage(int) - Constructor for class org.orekit.gnss.metric.messages.ParsedMessage
Simple constructor.
parseDouble(String) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Parse a double from a string.
ParsedUnitsBehavior - Enum in org.orekit.files.ccsds.ndm
Behavior adopted for units that have been parsed from a CCSDS message.
parseMessage(DataSource) - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
Parse a data source.
parseMessage(DataSource) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Parse a data source.
parseMessageNumber(EncodedMessage) - Method in class org.orekit.gnss.metric.parser.IgsSsrMessagesParser
Parse the message number.
parseMessageNumber(EncodedMessage) - Method in class org.orekit.gnss.metric.parser.MessagesParser
Parse the message number.
parseMessageNumber(EncodedMessage) - Method in class org.orekit.gnss.metric.parser.RtcmMessagesParser
Parse the message number.
parseMonth(String) - Static method in enum org.orekit.time.Month
Parse the string to get the month.
Parser() - Constructor for class org.orekit.gnss.RinexObservationLoader.Parser
 
Parser() - Constructor for class org.orekit.time.AGILeapSecondFilesLoader.Parser
Simple constructor.
Parser() - Constructor for class org.orekit.time.TAIUTCDatFilesLoader.Parser
Simple constructor.
Parser() - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader.Parser
Simple constructor.
Parser - Class in org.orekit.utils.units
Parser for units.
ParserBuilder - Class in org.orekit.files.ccsds.ndm
Builder for all CCSDS Message files parsers.
ParserBuilder() - Constructor for class org.orekit.files.ccsds.ndm.ParserBuilder
Simple constructor.
ParserBuilder(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.ParserBuilder
Simple constructor.
parseSatelliteSystem(String) - Static method in enum org.orekit.gnss.SatelliteSystem
Parse a string to get the satellite system.
parseSatelliteType(String) - Static method in enum org.orekit.gnss.antenna.SatelliteType
Parse a string to get the satellite type.
parseTime(String) - Static method in class org.orekit.time.TimeComponents
Parse a string in ISO-8601 format to build a time.
parseTimeSystem(String) - Static method in enum org.orekit.gnss.TimeSystem
Parse a string to get the time system.
ParseToken - Class in org.orekit.files.ccsds.utils.lexical
Token occurring during CCSDS file parsing.
ParseToken(TokenType, String, String, Unit, int, String) - Constructor for class org.orekit.files.ccsds.utils.lexical.ParseToken
Simple constructor.
ParseToken.BooleanConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume boolean values.
ParseToken.CenterConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume center values.
ParseToken.CenterListConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume center lists.
ParseToken.CharConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume character values.
ParseToken.DateConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume date values.
ParseToken.DoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume double values.
ParseToken.DoublyIndexedDoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume doubly-indexed double values.
ParseToken.EnumConsumer<T extends Enum<T>> - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume enum values.
ParseToken.EnumListConsumer<T extends Enum<T>> - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume lists of enum values.
ParseToken.FrameConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume frame values.
ParseToken.IndexedDoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume indexed double values.
ParseToken.IndexedStringConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume indexed string values.
ParseToken.IntConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume integer values.
ParseToken.IntegerArrayConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume integer array.
ParseToken.LabeledDoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume labeled double values.
ParseToken.StringConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume string values.
ParseToken.StringListConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume lists of strings values.
ParseToken.TimeSystemConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume time systems values.
ParseToken.UnitListConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume units lists values.
ParseToken.VectorConsumer - Interface in org.orekit.files.ccsds.utils.lexical
Interface representing instance methods that consume vector values.
parseType(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Parse an attitude type.
parseType(String) - Static method in enum org.orekit.files.sp3.SP3.SP3OrbitType
Parse a string to get the type.
PartialDerivativesEquations - Class in org.orekit.propagation.numerical
PartialDerivativesEquations(String, NumericalPropagator) - Constructor for class org.orekit.propagation.numerical.PartialDerivativesEquations
Deprecated.
Simple constructor.
PASCAL - Static variable in class org.orekit.utils.units.Unit
Pascal unit.
PAST_INFINITY - Static variable in class org.orekit.time.AbsoluteDate
Dummy date at infinity in the past direction.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, double, double[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, double, T[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(AbsoluteDate, GeodeticPoint, double, double) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
 
pathDelay(FieldAbsoluteDate<T>, GeodeticPoint, T, double) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
 
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(AbsoluteDate, GeodeticPoint, double, double, double, double[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldAbsoluteDate<T>, FieldGeodeticPoint<T>, T, T, double, T[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
 
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
 
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
PERCENT - Static variable in class org.orekit.utils.units.Unit
Percentage unit.
PERCENTS_TO_UNIT - Static variable in class org.orekit.utils.units.UnitsConverter
Percents to units converter.
perige - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
perigee, expressed in KM and ALTITUDE.
perige - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
perigee, expressed in KM and ALTITUDE.
permutation(int, double) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Perform one symmetric permutation involving rows/columns k0 and k0+1.
Perturbations - Class in org.orekit.files.ccsds.ndm.odm.ocm
Perturbation parameters.
Perturbations(CelestialBodies) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Simple constructor.
PerturbationsKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Keys for perturbations data entries.
Phase - Class in org.orekit.estimation.measurements.gnss
Class modeling a phase measurement from a ground station.
Phase(GroundStation, AbsoluteDate, double, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.Phase
Simple constructor.
PhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurement with ambiguity.
PhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
Constructor.
PhaseBias - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for phase bias data.
PhaseBias(int, boolean, int, int, double) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias
Constructor.
PhaseBuilder - Class in org.orekit.estimation.measurements.gnss
Builder for Phase measurements.
PhaseBuilder(CorrelatedRandomVectorGenerator, GroundStation, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.PhaseBuilder
Simple constructor.
PhaseCenterVariationFunction - Interface in org.orekit.gnss.antenna
Model for antennas phase center variations.
PhaseIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurement with ionospheric delay.
PhaseIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier
Constructor.
PhaseMinusCodeCombination - Class in org.orekit.estimation.measurements.gnss
Phase minus Code combination.
PhaseMinusCodeCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss
Phase minus code cycle slip detectors.
PhaseMinusCodeCycleSlipDetector(double, double, int, int) - Constructor for class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCycleSlipDetector
Polynomial single frequency cycle-slip detector Constructor.
PhaseTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurement with tropospheric delay.
PhaseTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier
Constructor.
PhysicalProperties - Class in org.orekit.files.ccsds.ndm.odm.ocm
Spacecraft physical properties.
PhysicalPropertiesKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Keys for physical properties data entries.
PLUTO - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Pluto.
PocMethodFacade - Class in org.orekit.files.ccsds.definitions
Facade in front of several probability of collision methods in CCSDS messages.
PocMethodFacade(String, PocMethodType) - Constructor for class org.orekit.files.ccsds.definitions.PocMethodFacade
Simple constructor.
PocMethodType - Enum in org.orekit.files.ccsds.definitions
Type of probability of collision method used in CCSDS Conjunction Data Messages.
pointAt(double) - Method in class org.orekit.bodies.Ellipse
Get a point of the 2D ellipse.
pointAtDistance(double, double, double) - Method in class org.orekit.frames.TopocentricFrame
Compute the point observed from the station at some specified distance.
pointOnLimb(Vector3D, Vector3D) - Method in class org.orekit.bodies.Ellipsoid
Find a point on ellipsoid limb, as seen by an external observer.
PoissonSeries - Class in org.orekit.data
Class representing a Poisson series for nutation or ephemeris computations.
PoissonSeries(PolynomialNutation, Map<Long, SeriesTerm>) - Constructor for class org.orekit.data.PoissonSeries
Build a Poisson series from an IERS table file.
PoissonSeries.CompiledSeries - Interface in org.orekit.data
This interface represents a fast evaluator for Poisson series.
PoissonSeriesParser - Class in org.orekit.data
Parser for Poisson series files.
PoissonSeriesParser(int) - Constructor for class org.orekit.data.PoissonSeriesParser
Build a parser for a Poisson series from an IERS table file.
PoleCorrection - Class in org.orekit.frames
Simple container class for pole correction parameters.
PoleCorrection(double, double) - Constructor for class org.orekit.frames.PoleCorrection
Simple constructor.
PolygonalFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with polygonal shape.
PolygonalFieldOfView(SphericalPolygonsSet, double) - Constructor for class org.orekit.geometry.fov.PolygonalFieldOfView
Build a new instance.
PolygonalFieldOfView(Vector3D, PolygonalFieldOfView.DefiningConeType, Vector3D, double, int, double) - Constructor for class org.orekit.geometry.fov.PolygonalFieldOfView
Build Field Of View with a regular polygon shape.
PolygonalFieldOfView.DefiningConeType - Enum in org.orekit.geometry.fov
Enumerate for cone/polygon relative position.
PolynomialAccelerationModel - Class in org.orekit.forces.empirical
Polynomial acceleration model.
PolynomialAccelerationModel(String, AbsoluteDate, int) - Constructor for class org.orekit.forces.empirical.PolynomialAccelerationModel
Simple constructor.
PolynomialFunctionMatrix - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
A quadratic matrix of PolynomialFunction.
PolynomialNutation - Class in org.orekit.data
Polynomial nutation function.
PolynomialNutation(double...) - Constructor for class org.orekit.data.PolynomialNutation
Build a polynomial from its coefficients.
PolynomialParser - Class in org.orekit.data
Parser for polynomials in IERS tables.
PolynomialParser(char, PolynomialParser.Unit) - Constructor for class org.orekit.data.PolynomialParser
Simple constructor.
PolynomialParser.Unit - Enum in org.orekit.data
Unit for the coefficients.
POS_X - Static variable in enum org.orekit.orbits.OrbitType
Name for position along X.
POS_Y - Static variable in enum org.orekit.orbits.OrbitType
Name for position along Y.
POS_Z - Static variable in enum org.orekit.orbits.OrbitType
Name for position along Z.
Position - Class in org.orekit.estimation.measurements
Class modeling a position only measurement.
Position(AbsoluteDate, Vector3D, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position
Constructor with one double for the standard deviation.
Position(AbsoluteDate, Vector3D, double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position
Constructor with one vector for the standard deviation.
Position(AbsoluteDate, Vector3D, double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position
Constructor with full covariance matrix and all inputs.
PositionAngle - Enum in org.orekit.orbits
Enumerate for true, eccentric and mean position angles.
PositionAngleDetector - Class in org.orekit.propagation.events
Detector for in-orbit position angle.
PositionAngleDetector(OrbitType, PositionAngle, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector
Build a new detector.
PositionAngleDetector(double, double, OrbitType, PositionAngle, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector
Build a detector.
PositionBuilder - Class in org.orekit.estimation.measurements.generation
Builder for Position measurements.
PositionBuilder(CorrelatedRandomVectorGenerator, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.PositionBuilder
Simple constructor.
positionShiftedBy(double) - Method in class org.orekit.utils.PVCoordinates
Get a time-shifted position.
PotentialCoefficientsReader - Class in org.orekit.forces.gravity.potential
This abstract class represents a Gravitational Potential Coefficients file reader.
PotentialCoefficientsReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Simple constructor.
PotentialCoefficientsReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Simple constructor.
power(String, Fraction) - Method in class org.orekit.utils.units.Unit
Create power of unit.
PowerTerm - Class in org.orekit.utils.units
A container for a term with associated power.
Predefined - Enum in org.orekit.frames
Predefined frames provided by Frames.
PREFIX - Static variable in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
Prefix for state name.
prepareData() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Prepare data for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Prepare header for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Prepare metadata for parsing.
previous() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the previous time span.
previous() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the previous transition.
process(ParseToken, ContextBinding, AdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.AdmMetadataKey
Process one token.
process(ParseToken, ContextBinding, AemMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Process an token.
process(ParseToken, ContextBinding, AttitudeEntry) - Method in enum org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Process an token.
process(ParseToken, ContextBinding, ApmQuaternion) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Process one token.
process(ParseToken, ContextBinding, Euler) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Process one token.
process(ParseToken, ContextBinding, Maneuver) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Process one token.
process(ParseToken, ContextBinding, SpacecraftParameters) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParametersKey
Process one token.
process(ParseToken, ContextBinding, SpinStabilized) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Process one token.
process(ParseToken, ContextBinding, AdditionalParameters) - Method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Process one token.
process(ParseToken, ContextBinding, CdmHeader) - Method in enum org.orekit.files.ccsds.ndm.cdm.CdmHeaderKey
Process an token.
process(ParseToken, ContextBinding, CdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Process an token.
process(ParseToken, ContextBinding, CdmRelativeMetadata) - Method in enum org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
Process one token.
process(ParseToken, ContextBinding, ODParameters) - Method in enum org.orekit.files.ccsds.ndm.cdm.ODParametersKey
Process one token.
process(ParseToken, ContextBinding, RTNCovariance) - Method in enum org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Process one token.
process(ParseToken, ContextBinding, StateVector) - Method in enum org.orekit.files.ccsds.ndm.cdm.StateVectorKey
Process one token.
process(ParseToken, CdmParser) - Method in enum org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
Process one token.
process(ParseToken, ContextBinding, CartesianCovariance) - Method in enum org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Process one token.
process(ParseToken, ContextBinding, CommonMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.CommonMetadataKey
Process one token.
process(ParseToken, ContextBinding, KeplerianElements) - Method in enum org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Process one token.
process(ParseToken, ContextBinding, CovarianceHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadataKey
Process an token.
process(String, ContextBinding, Maneuver, int, String) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Process one field.
process(ParseToken, ContextBinding, ManeuverHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadataKey
Process an token.
process(ParseToken, OcmParser) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Process one token.
process(ParseToken, ContextBinding, OcmMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Process an token.
process(ParseToken, ContextBinding, OrbitDetermination) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Process an token.
process(ParseToken, ContextBinding, Perturbations) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Process an token.
process(ParseToken, ContextBinding, PhysicalProperties) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.PhysicalPropertiesKey
Process an token.
process(ParseToken, ContextBinding, TrajectoryStateHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Process an token.
process(ParseToken, ContextBinding, OdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.OdmMetadataKey
Process one token.
process(ParseToken, ContextBinding, OemMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey
Process an token.
process(ParseToken, ContextBinding, OmmMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmMetadataKey
Process one token.
process(ParseToken, ContextBinding, OmmTle) - Method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
Process one token.
process(ParseToken, ContextBinding, Maneuver) - Method in enum org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
Process one token.
process(ParseToken, ContextBinding, SpacecraftParameters) - Method in enum org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey
Process one token.
process(ParseToken, ContextBinding, StateVector) - Method in enum org.orekit.files.ccsds.ndm.odm.StateVectorKey
Process one token.
process(ParseToken, ContextBinding, RangeUnitsConverter, TdmMetadata, ObservationsBlock) - Method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType
Process an observation line.
process(ParseToken, ContextBinding, ObservationsBlock) - Method in enum org.orekit.files.ccsds.ndm.tdm.TdmDataKey
Process one token.
process(ParseToken, ContextBinding, TdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Process an token.
process(ParseToken, ContextBinding, Header) - Method in enum org.orekit.files.ccsds.section.HeaderKey
Process an token.
process(ParseToken, AbstractConstituentParser<?, ?>) - Method in enum org.orekit.files.ccsds.section.KvnStructureKey
Process an token.
process(ParseToken, ContextBinding, Metadata) - Method in enum org.orekit.files.ccsds.section.MetadataKey
Process an token.
process(ParseToken, AbstractConstituentParser<?, ?>) - Method in enum org.orekit.files.ccsds.section.XmlStructureKey
Process an token.
process(ParseToken) - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
Process a parse token.
process(ParseToken) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Process a parse token.
processAsBoolean(ParseToken.BooleanConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a boolean.
processAsCenter(ParseToken.CenterConsumer, CelestialBodies) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a body center.
processAsCenterList(ParseToken.CenterListConsumer, CelestialBodies) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a body center list.
processAsDate(ParseToken.DateConsumer, ContextBinding) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a date.
processAsDouble(Unit, ParsedUnitsBehavior, ParseToken.DoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a double.
processAsDoublyIndexedDouble(int, int, Unit, ParsedUnitsBehavior, ParseToken.DoublyIndexedDoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a doubly-indexed double.
processAsEnum(Class<T>, ParseToken.EnumConsumer<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an enum.
processAsEnumsList(Class<T>, ParseToken.EnumListConsumer<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a list of enums.
processAsFrame(ParseToken.FrameConsumer, ContextBinding, boolean, boolean, boolean) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a frame.
processAsIndexedDouble(int, Unit, ParsedUnitsBehavior, ParseToken.IndexedDoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an indexed double.
processAsIndexedNormalizedString(int, ParseToken.IndexedStringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an indexed normalized string.
processAsIndexedUppercaseString(int, ParseToken.IndexedStringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an indexed normalized uppercase string.
processAsInteger(ParseToken.IntConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an integer.
processAsIntegerArray(ParseToken.IntegerArrayConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an array of integers.
processAsLabeledDouble(char, Unit, ParsedUnitsBehavior, ParseToken.LabeledDoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as an labeled double.
processAsNormalizedCharacter(ParseToken.CharConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a normalized character.
processAsNormalizedList(ParseToken.StringListConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a list of normalized strings.
processAsNormalizedString(ParseToken.StringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a normalized string.
processAsTimeSystem(ParseToken.TimeSystemConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a time system.
processAsUnitList(ParseToken.UnitListConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a list of units.
processAsUppercaseList(ParseToken.StringListConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a list of normalized uppercase strings.
processAsUppercaseString(ParseToken.StringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a normalized uppercase string.
processAsVector(ParseToken.VectorConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
Process the content as a vector.
ProcessingState - Interface in org.orekit.files.ccsds.utils.parsing
Interface for processing parsing tokens for CCSDS NDM files.
processMeasurements(Iterable<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Process several measurements.
processMeasurements(List<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
Process a single measurement.
processMeasurements(List<ObservedMeasurement<?>>, ExtendedKalmanFilter<MeasurementDecorator>) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Process a single measurement.
processRotationOrder(ParseToken, AdmParser.RotationOrderConsumer) - Static method in class org.orekit.files.ccsds.ndm.adm.AdmParser
Process a CCSDS Euler angles sequence as a RotationOrder.
processToken(ParseToken) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmHeaderProcessingState
Process one token.
processToken(ParseToken) - Method in class org.orekit.files.ccsds.section.HeaderProcessingState
Process one token.
processToken(ParseToken) - Method in class org.orekit.files.ccsds.section.KvnStructureProcessingState
Process one token.
processToken(ParseToken) - Method in class org.orekit.files.ccsds.section.XmlStructureProcessingState
Process one token.
processToken(ParseToken) - Method in class org.orekit.files.ccsds.utils.parsing.ErrorState
Process one token.
processToken(ParseToken) - Method in interface org.orekit.files.ccsds.utils.parsing.ProcessingState
Process one token.
projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.CircularFieldOfView
Find the direction on Field Of View Boundary closest to a line of sight.
projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Find the direction on Field Of View Boundary closest to a line of sight.
projectToBoundary(Vector3D) - Method in interface org.orekit.geometry.fov.FieldOfView
Find the direction on Field Of View Boundary closest to a line of sight.
projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView
Find the direction on Field Of View Boundary closest to a line of sight.
projectToEllipse(Vector2D) - Method in class org.orekit.bodies.Ellipse
Find the closest ellipse point.
projectToEllipse(TimeStampedPVCoordinates) - Method in class org.orekit.bodies.Ellipse
Project position-velocity-acceleration on an ellipse.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in interface org.orekit.bodies.BodyShape
Project a point to the ground.
projectToGround(TimeStampedPVCoordinates, Frame) - Method in interface org.orekit.bodies.BodyShape
Project a moving point to the ground.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid
Project a point to the ground.
projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid
Project a moving point to the ground.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.models.earth.Geoid
 
projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.models.earth.Geoid
 
propagate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator
Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Propagate from a start date towards a target date.
propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Propagate from a start date towards a target date.
propagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Propagate towards a target date.
propagate(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldPropagator
Propagate towards a target date.
propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldPropagator
Propagate from a start date towards a target date.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Propagate from a start date towards a target date.
propagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Propagate towards a target date.
propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Propagate from a start date towards a target date.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
Propagate towards a target date.
propagate(AbsoluteDate) - Method in interface org.orekit.propagation.Propagator
Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.propagation.Propagator
Propagate from a start date towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.PropagatorsParallelizer
Propagate from a start date towards a target date.
propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Gets the PVCoordinates of the GLONASS SV in ECEF frame.
propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Gets the PVCoordinates of the GNSS SV in ECEF frame.
propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Gets the PVCoordinates of the GNSS SV in ECEF frame.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Extrapolate an orbit up to a specific target date.
PropagationType - Enum in org.orekit.propagation
Enumerate to define the propagation type used by the propagator.
Propagator - Interface in org.orekit.propagation
This interface provides a way to propagate an orbit at any time.
PropagatorBuilder - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction to build propagators for conversion.
PropagatorConverter - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction for propagators conversions.
PropagatorsParallelizer - Class in org.orekit.propagation
This class provides a way to propagate simultaneously several orbits.
PropagatorsParallelizer(List<Propagator>, MultiSatStepHandler) - Constructor for class org.orekit.propagation.PropagatorsParallelizer
Simple constructor.
PropulsionModel - Interface in org.orekit.forces.maneuvers.propulsion
Generic interface for a propulsion model used in a Maneuver.
put(String, double[]) - Method in class org.orekit.utils.DoubleArrayDictionary
Add an entry.
put(String, T[]) - Method in class org.orekit.utils.FieldArrayDictionary
Add an entry.
put(String, double[]) - Method in class org.orekit.utils.FieldArrayDictionary
Add an entry.
putAll(Map<String, double[]>) - Method in class org.orekit.utils.DoubleArrayDictionary
Put all the entries from the map in the dictionary.
putAll(DoubleArrayDictionary) - Method in class org.orekit.utils.DoubleArrayDictionary
Put all the entries from another dictionary.
putAll(Map<String, T[]>) - Method in class org.orekit.utils.FieldArrayDictionary
Put all the entries from the map in the dictionary.
putAll(FieldArrayDictionary<T>) - Method in class org.orekit.utils.FieldArrayDictionary
Put all the entries from another dictionary.
PV - Class in org.orekit.estimation.measurements
Class modeling a position-velocity measurement.
PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with two double for the standard deviations.
PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with two vectors for the standard deviations.
PV(AbsoluteDate, Vector3D, Vector3D, double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with one vector for the standard deviations.
PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with 2 smaller covariance matrices.
PV(AbsoluteDate, Vector3D, Vector3D, double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with full covariance matrix and all inputs.
PVBuilder - Class in org.orekit.estimation.measurements.generation
Builder for PV measurements.
PVBuilder(CorrelatedRandomVectorGenerator, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.PVBuilder
Simple constructor.
PVCoordinates - Class in org.orekit.utils
Simple container for Position/Velocity/Acceleration triplets.
PVCoordinates() - Constructor for class org.orekit.utils.PVCoordinates
Simple constructor.
PVCoordinates(Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet with zero acceleration.
PVCoordinates(Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet.
PVCoordinates(double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Multiplicative constructor.
PVCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Subtractive constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(FieldVector3D<U>) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet from a FieldVector3D<Derivative>.
PVCoordinates(Vector3D) - Constructor for class org.orekit.utils.PVCoordinates
Builds PV coordinates with the givne position, zero velocity, and zero acceleration.
PVCoordinatesProvider - Interface in org.orekit.utils
Interface for PV coordinates providers.

Q

Q1 - Static variable in class org.orekit.models.earth.displacement.Tide
Q₁ tide.
Q22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
Q31 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
Q33 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
QOMS2T - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
QZSS_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of the earth's rotation rate in rad/s for QZSS user.
QZSS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for QZSS weeks: 1980-01-06T00:00:00 QZSS time.
QZSS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for QZSS weeks: 1980-01-06.
QZSS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
WGS 84 value of the Earth's universal gravitational parameter for QZSS user in m³/s².
QZSS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Number of weeks in the QZSS cycle.
QZSSAlmanac - Class in org.orekit.propagation.analytical.gnss.data
This class holds a QZSS almanac as read from YUMA files.
QZSSAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
Constructor.
QZSSNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a QZSS navigation message.
QZSSNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
Constructor.
QZSSScale - Class in org.orekit.time
QZSS time scale.

R

RAAN - Static variable in enum org.orekit.orbits.OrbitType
Name for right ascension of ascending node.
RADIAN - Static variable in class org.orekit.utils.units.Unit
Radian unit.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in interface org.orekit.forces.radiation.RadiationSensitive
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in interface org.orekit.forces.radiation.RadiationSensitive
Compute the acceleration due to radiation pressure.
RadiationSensitive - Interface in org.orekit.forces.radiation
Interface for spacecraft that are sensitive to radiation pressure forces.
radiusCorrection(double) - Method in enum org.orekit.propagation.events.VisibilityTrigger
Apply radius correction.
Range - Class in org.orekit.estimation.measurements
Class modeling a range measurement from a ground station.
Range(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Range
Simple constructor.
RangeBuilder - Class in org.orekit.estimation.measurements.generation
Builder for Range measurements.
RangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, boolean, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.RangeBuilder
Simple constructor.
rangeErrorIonosphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier
Compute the measurement error due to Ionosphere.
rangeErrorIonosphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier
Compute the measurement error due to Ionosphere.
rangeErrorTroposphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier
Compute the measurement error due to Troposphere.
rangeErrorTroposphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier
Compute the measurement error due to Troposphere.
RangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with ionospheric delay.
RangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier
Constructor.
RangeMeasurement(AbsoluteDate, double, int) - Constructor for class org.orekit.files.ilrs.CRD.RangeMeasurement
Constructor.
RangeMeasurement(AbsoluteDate, double, int, double) - Constructor for class org.orekit.files.ilrs.CRD.RangeMeasurement
Constructor.
RangeMode - Enum in org.orekit.files.ccsds.ndm.tdm
Type of range tones.
RangeModifierUtil - Class in org.orekit.estimation.measurements.modifiers
Utility class modifying theoretical range measurement.
RangeRate - Class in org.orekit.estimation.measurements
Class modeling one-way or two-way range rate measurement between two vehicles.
RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.RangeRate
Simple constructor.
RangeRateBuilder - Class in org.orekit.estimation.measurements.generation
Builder for RangeRate measurements.
RangeRateBuilder(CorrelatedRandomVectorGenerator, GroundStation, boolean, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.RangeRateBuilder
Simple constructor.
rangeRateErrorIonosphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier
Compute the measurement error due to Ionosphere.
rangeRateErrorIonosphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier
Compute the measurement error due to Ionosphere.
rangeRateErrorIonosphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier
Compute the measurement error due to Ionosphere.
rangeRateErrorIonosphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier
Compute the measurement error due to Ionosphere.
rangeRateErrorTroposphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier
Compute the measurement error due to Troposphere.
rangeRateErrorTroposphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier
Compute the measurement error due to Troposphere.
rangeRateErrorTroposphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Compute the measurement error due to Troposphere.
rangeRateErrorTroposphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Compute the measurement error due to Troposphere.
RangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range-rate measurement with ionospheric delay.
RangeRateIonosphericDelayModifier(IonosphericModel, double, boolean) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier
Constructor.
RangeRateModifierUtil - Class in org.orekit.estimation.measurements.modifiers
Utility class modifying theoretical range-rate measurement.
RangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range-rate measurements with tropospheric delay.
RangeRateTroposphericDelayModifier(DiscreteTroposphericModel, boolean) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Constructor.
RangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with tropospheric delay.
RangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier
Constructor.
RangeUnits - Enum in org.orekit.files.ccsds.ndm.tdm
Units of the range observable.
RangeUnitsConverter - Interface in org.orekit.files.ccsds.ndm.tdm
Interface for converting Range Units to meters.
RAPID_DATA_PREDICITON_COLUMNS_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the Rapid Data and Prediction EOP columns files (IAU2000 compatibles).
RAPID_DATA_PREDICITON_XML_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the Rapid Data and Prediction EOP XML files (IAU2000 compatibles).
RAPID_DATA_PREDICTION_COLUMNS_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the Rapid Data and Prediction EOP columns files (IAU1980 compatibles).
RAPID_DATA_PREDICTION_XML_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the Rapid Data and Prediction EOP XML files (IAU1980 compatibles).
rateFrameIsA() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Check if rates are specified in frame A.
rateFrameIsA() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Check if rates are specified in frame A.
rawDataIsBinary() - Method in interface org.orekit.data.DataSource.Opener
Check if the raw data is binary.
RawSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide raw spherical harmonics coefficients.
RawSphericalHarmonicsProvider.RawSphericalHarmonics - Interface in org.orekit.forces.gravity.potential
The raw spherical harmonics at a particular instant.
rawToSI(RangeUnitsConverter, TdmMetadata, AbsoluteDate, double) - Method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType
Convert a measurement to SI units.
readGravityField(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Read a gravity field coefficients provider from the first supported file.
readGravityField(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Read a gravity field coefficients provider from the first supported file.
readLine() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader
Deprecated.
Read a line from the input data stream.
readLineOrThrow(Localizable, Object...) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader
Deprecated.
Read a line from the input data stream, or if the end of the stream has been reached throw an exception.
Receiver(String, String, double, double, double) - Constructor for class org.orekit.gnss.clock.RinexClock.Receiver
Constructor.
ReceiverAntenna - Class in org.orekit.gnss.antenna
GNSS receiver antenna model.
ReceiverAntenna(String, String, Map<Frequency, FrequencyPattern>, String) - Constructor for class org.orekit.gnss.antenna.ReceiverAntenna
Simple constructor.
Record - Class in org.orekit.gnss.metric.ntrip
Record in source table.
Record(String) - Constructor for class org.orekit.gnss.metric.ntrip.Record
Build a record by parsing a source table line.
RecordAndContinue<T extends EventDetector> - Class in org.orekit.propagation.events.handlers
Handler that will record every time an event occurs and always return Action.CONTINUE.
RecordAndContinue() - Constructor for class org.orekit.propagation.events.handlers.RecordAndContinue
Create a new handler using an ArrayList to store events.
RecordAndContinue(List<RecordAndContinue.Event<T>>) - Constructor for class org.orekit.propagation.events.handlers.RecordAndContinue
Create a handler using the given collection to store events.
RecordAndContinue.Event<T> - Class in org.orekit.propagation.events.handlers
A single event detected during propagation.
RecordType - Enum in org.orekit.gnss.metric.ntrip
Enumerate for record types in sourcetable.
recoverAmbiguities() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Recover ambiguities prior to the Z-transformation.
recoverAmbiguities() - Method in class org.orekit.estimation.measurements.gnss.IntegerBootstrapping
Recover ambiguities prior to the Z-transformation.
reduction() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Perform LAMBDA reduction.
reduction() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod
Perform LAMBDA reduction.
reduction() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Perform MLAMBDA reduction.
ReferenceClock(String, String, double, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.gnss.clock.RinexClock.ReferenceClock
Constructor.
referenceDateChanged(AbsoluteDate, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter reference date has been changed.
ReferenceEllipsoid - Class in org.orekit.models.earth
A Reference Ellipsoid for use in geodesy.
ReferenceEllipsoid(double, double, Frame, double, double) - Constructor for class org.orekit.models.earth.ReferenceEllipsoid
Creates a new geodetic Reference Ellipsoid from four defining parameters.
referenceValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter reference value has been changed.
REFLECTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive
Parameter name for reflection coefficient.
refuseFurtherComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer
Set flag to refuse further comments.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Register an attitude provider.
registerSwitchEvents(Propagator) - Method in class org.orekit.attitudes.AttitudesSequence
Register all wrapped switch events to the propagator.
registerSwitchEvents(Field<T>, FieldPropagator<T>) - Method in class org.orekit.attitudes.AttitudesSequence
Register all wrapped switch events to the propagator.
RegularXmlTokenBuilder - Class in org.orekit.files.ccsds.utils.lexical
Regular builder using XML elements names and content for tokens.
RegularXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.utils.lexical.RegularXmlTokenBuilder
Simple constructor.
reinitializeBegin(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState
Reinitialize the beginning of the step.
reinitializeBegin(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState
Reinitialize the beginning of the step.
RelativisticClockInterSatellitesPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical inter-satellites phase measurement with relativistic clock correction.
RelativisticClockInterSatellitesPhaseModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesPhaseModifier
Simple constructor.
RelativisticClockInterSatellitesRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical inter-satellites range measurement with relativistic clock correction.
RelativisticClockInterSatellitesRangeModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesRangeModifier
Simple constructor.
RelativisticClockOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical one-way GNSS phase measurement with relativistic clock correction.
RelativisticClockOneWayGNSSPhaseModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSPhaseModifier
Simple constructor.
RelativisticClockOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical one-way GNSS range measurement with relativistic clock correction.
RelativisticClockOneWayGNSSRangeModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeModifier
Simple constructor.
RelativisticClockPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurement with relativistic clock correction.
RelativisticClockPhaseModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockPhaseModifier
Simple constructor.
RelativisticClockRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with relativistic clock correction.
RelativisticClockRangeModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeModifier
Simple constructor.
RelativisticClockRangeRateModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range-rate measurement with relativistic frequency deviation.
RelativisticClockRangeRateModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeRateModifier
Simple constructor.
relativisticCorrection(EstimatedMeasurement<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockModifier
Computes the relativistic clock correction.
RelativisticJ2ClockInterSatellitesPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical inter-satellites phase measurements with relativistic J2 clock correction.
RelativisticJ2ClockInterSatellitesPhaseModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesPhaseModifier
Modifier constructor.
RelativisticJ2ClockInterSatellitesRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical inter-satellites range measurements with relativistic J2 clock correction.
RelativisticJ2ClockInterSatellitesRangeModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesRangeModifier
Modifier constructor.
RelativisticJ2ClockOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical one-way phase measurements with relativistic J2 clock correction.
RelativisticJ2ClockOneWayGNSSPhaseModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSPhaseModifier
Modifier constructor.
RelativisticJ2ClockOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying one-way GNSS range theoretical measurements with relativistic J2 clock correction.
RelativisticJ2ClockOneWayGNSSRangeModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSRangeModifier
Modifier constructor.
RelativisticJ2ClockPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurements with relativistic J2 clock correction.
RelativisticJ2ClockPhaseModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockPhaseModifier
Modifier constructor.
RelativisticJ2ClockRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurements with relativistic J2 clock correction.
RelativisticJ2ClockRangeModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockRangeModifier
Modifier constructor.
relativisticJ2Correction(EstimatedMeasurement<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticJ2ClockModifier
Computes the relativistic J2 clock time delay correction.
Relativity - Class in org.orekit.forces.gravity
Post-Newtonian correction force due to general relativity.
Relativity(double) - Constructor for class org.orekit.forces.gravity.Relativity
Create a force model to add post-Newtonian acceleration corrections to an Earth orbit.
remove(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Remove a handler.
remove(FieldOrekitFixedStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Remove a handler.
remove(OrekitStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Remove a handler.
remove(OrekitFixedStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Remove a handler.
remove(String) - Method in class org.orekit.utils.DoubleArrayDictionary
Remove an entry.
remove(String) - Method in class org.orekit.utils.FieldArrayDictionary
remove an entry.
removeForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Remove all perturbing force models from the global perturbation model.
removeForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Remove all force models (except central attraction).
removeForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Remove all perturbing force models from the global perturbation model (except central attraction).
removeForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Remove all perturbing force models from the global perturbation model (except central attraction).
removeObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver
Remove an observer.
removeProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager
Remove one provider.
removeSolution() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Remove spurious solution.
replaceObserver(ParameterObserver, ParameterObserver) - Method in class org.orekit.utils.ParameterDriver
Replace an observer.
requiresDenseOutput() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Determines whether this handler needs dense output.
requiresDenseOutput() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Determines whether this handler needs dense output.
rescale(double, boolean, double[][], double[][], boolean, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
rescale(double, boolean, Flattener, Flattener, double[]) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Rescale coefficients arrays.
rescale(boolean, Flattener, Flattener, TimeDependentHarmonic[]) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Rescale coefficients arrays.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.NdmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Reset parser to initial state before parsing.
reset(FileFormat) - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
Reset parser to initial state before parsing.
reset(FileFormat, ProcessingState) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Reset parser to initial state before parsing.
resetActiveProvider(AttitudeProvider) - Method in class org.orekit.attitudes.AttitudesSequence
Reset the active provider.
resetFiltersToDefault() - Method in class org.orekit.data.DataProvidersManager
Reset all filters to default.
resetFitting(AbsoluteDate, double...) - Method in class org.orekit.utils.SecularAndHarmonic
Reset fitting.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState, PropagationType, double, int) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState, PropagationType, double, int) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.Ephemeris
Try (and fail) to reset the initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>, PropagationType, double, int) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>, PropagationType, double, int) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in interface org.orekit.propagation.Propagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Reset the initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Reset the initial state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean, double, int) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean, double, int) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.Ephemeris
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean, double, int) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean, double, int) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Reset an intermediate state.
resetOrbit(Orbit) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Reset the orbit in the propagator builder.
resetOrbit(Orbit, PropagationType) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Reset the orbit in the propagator builder.
resetOrbit(Orbit) - Method in interface org.orekit.propagation.conversion.OrbitDeterminationPropagatorBuilder
Reset the orbit in the propagator builder.
resetState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
Reset state as a maneuver triggers.
resetState(FieldSpacecraftState<T>) - Method in interface org.orekit.forces.maneuvers.trigger.FieldManeuverTriggersResetter
Reset state as a maneuver triggers.
resetState(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter
Reset state as a maneuver triggers.
resetState(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector
Reset the state prior to continue propagation.
resetState(SpacecraftState) - Method in class org.orekit.propagation.events.AdapterDetector
Reset the state prior to continue propagation.
resetState(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector
Reset the state prior to continue propagation.
resetState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Reset the state prior to continue propagation.
resetState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector
Reset the state prior to continue propagation.
resetState(T, SpacecraftState) - Method in interface org.orekit.propagation.events.handlers.EventHandler
Reset the state prior to continue propagation.
resetState(D, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Reset the state prior to continue propagation.
resetState(KK, FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler
Reset the state prior to continue propagation.
ResidualFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.filtering
Residual pre-processing filter.
ResidualFilter(double) - Constructor for class org.orekit.estimation.measurements.filtering.ResidualFilter
Constructor.
restrictStep(FieldSpacecraftState<T>, FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Create a new restricted version of the instance.
restrictStep(SpacecraftState, SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Create a new restricted version of the instance.
REV_PER_DAY - Static variable in class org.orekit.files.ccsds.definitions.Units
Revolutions per day unit.
REV_PER_DAY2_SCALED - Static variable in class org.orekit.files.ccsds.definitions.Units
Scaled revolutions per square day unit.
REV_PER_DAY3_SCALED - Static variable in class org.orekit.files.ccsds.definitions.Units
Scaled revolutions per cubic day divieded by 6 unit.
revert() - Method in class org.orekit.utils.AngularCoordinates
Revert a rotation/rotation rate/ rotation acceleration triplet.
revert() - Method in class org.orekit.utils.FieldAngularCoordinates
Revert a rotation / rotation rate / rotation acceleration triplet.
revert() - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Revert a rotation/rotation rate pair.
revert() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Revert a rotation/rotation rate pair.
REVOLUTION - Static variable in class org.orekit.utils.units.Unit
Revolution unit.
RichardsonExpansion - Class in org.orekit.orbits
Class implementing the Third-Order Richardson Expansion.
RichardsonExpansion(CR3BPSystem, LagrangianPoints) - Constructor for class org.orekit.orbits.RichardsonExpansion
Simple Constructor.
RinexClock - Class in org.orekit.gnss.clock
Represents a parsed clock file from the IGS.
RinexClock(Function<? super String, ? extends Frame>) - Constructor for class org.orekit.gnss.clock.RinexClock
Constructor.
RinexClock.ClockDataLine - Class in org.orekit.gnss.clock
Clock data for a single station.
RinexClock.ClockDataType - Enum in org.orekit.gnss.clock
Clock data type.
RinexClock.Receiver - Class in org.orekit.gnss.clock
Represents a receiver or a satellite with its position in the considered frame.
RinexClock.ReferenceClock - Class in org.orekit.gnss.clock
Represents a reference clock with its validity time span.
RinexClockParser - Class in org.orekit.gnss.clock
A parser for the clock file from the IGS.
RinexClockParser() - Constructor for class org.orekit.gnss.clock.RinexClockParser
Create an clock file parser using default values.
RinexClockParser(Function<? super String, ? extends Frame>) - Constructor for class org.orekit.gnss.clock.RinexClockParser
Create a clock file parser and specify the frame builder.
RinexClockParser(Function<? super String, ? extends Frame>, TimeScales) - Constructor for class org.orekit.gnss.clock.RinexClockParser
Constructor, build the IGS clock file parser.
RinexNavigation - Class in org.orekit.gnss.navigation
Represents a parsed RINEX navigation messages files.
RinexNavigation() - Constructor for class org.orekit.gnss.navigation.RinexNavigation
Constructor.
RinexNavigation.TimeSystemCorrection - Class in org.orekit.gnss.navigation
Container for time system corrections.
RinexNavigationParser - Class in org.orekit.gnss.navigation
Parser for RINEX navigation messages files.
RinexNavigationParser() - Constructor for class org.orekit.gnss.navigation.RinexNavigationParser
Constructor.
RinexNavigationParser(TimeScales) - Constructor for class org.orekit.gnss.navigation.RinexNavigationParser
Constructor.
RinexObservationHeader - Class in org.orekit.gnss
Container for Rinex observation file header.
RinexObservationHeader(double, SatelliteSystem, String, String, String, String, String, String, String, String, String, String, Vector3D, double, Vector2D, Vector3D, Vector3D, Vector3D, double, AbsoluteDate, AbsoluteDate, int, int) - Constructor for class org.orekit.gnss.RinexObservationHeader
Simple constructor, for Rinex 2 Header.
RinexObservationHeader(double, SatelliteSystem, String, String, String, String, String, String, String, String, String, String, Vector3D, double, Vector2D, Vector3D, String, Vector3D, Vector3D, double, Vector3D, Vector3D, String, double, AbsoluteDate, AbsoluteDate, int, List<AppliedDCBS>, List<AppliedPCVS>, List<RinexObservationLoader.Parser.PhaseShiftCorrection>, int, int, int, int) - Constructor for class org.orekit.gnss.RinexObservationHeader
Simple constructor, for Rinex 3 Header.
RinexObservationLoader - Class in org.orekit.gnss
Loader for Rinex measurements files.
RinexObservationLoader(String) - Constructor for class org.orekit.gnss.RinexObservationLoader
Simple constructor.
RinexObservationLoader(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.gnss.RinexObservationLoader
Create a RINEX loader/parser with the given source of RINEX auxiliary data files.
RinexObservationLoader(DataSource) - Constructor for class org.orekit.gnss.RinexObservationLoader
Simple constructor.
RinexObservationLoader(DataSource, TimeScales) - Constructor for class org.orekit.gnss.RinexObservationLoader
Loads RINEX from the given input stream using the specified auxiliary data.
RinexObservationLoader.Parser - Class in org.orekit.gnss
Parser for rinex files.
RinexObservationLoader.Parser.PhaseShiftCorrection - Class in org.orekit.gnss
Phase Shift corrections.
RinexObservationLoader.Parser.ScaleFactorCorrection - Class in org.orekit.gnss
Scale Factor to be applied.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.Aem
Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.Apm
Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.cdm.Cdm
Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Root element for XML messages.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.Oem
Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.Omm
Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.Opm
Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.tdm.Tdm
Root element for XML files.
ROOT22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
ROOT32 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
ROOT44 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
ROOT52 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
ROOT54 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
rotationFromInertial(PVCoordinates) - Method in enum org.orekit.frames.LOFType
Get the rotation from inertial frame to local orbital frame.
rotationFromInertial(Field<T>, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType
Get the rotation from inertial frame to local orbital frame.
rotationShiftedBy(double) - Method in class org.orekit.utils.AngularCoordinates
Get a time-shifted rotation.
RotationXmlTokenBuilder - Class in org.orekit.files.ccsds.ndm.adm
Builder for rotation angles and rates.
RotationXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.ndm.adm.RotationXmlTokenBuilder
Simple constructor.
Rtcm1019 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
RTCM 1019 message: GPS Satellite Ephemeris Data.
Rtcm1019(int, Rtcm1019Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019
Constructor.
Rtcm1019Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
Container for RTCM 1019 data.
Rtcm1019Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Constructor.
Rtcm1020 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
RTCM 1020 message: Glonass Satellite Ephemeris Data.
Rtcm1020(int, Rtcm1020Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020
Constructor.
Rtcm1020Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
Container for RTCM 1020 data.
Rtcm1020Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Constructor.
Rtcm1042 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
RTCM 1042 message: Beidou Satellite Ephemeris Data.
Rtcm1042(int, Rtcm1042Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042
Constructor.
Rtcm1042Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
Container for RTCM 1042 data.
Rtcm1042Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Constructor.
Rtcm1044 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
RTCM 1044 message: QZSS Satellite Ephemeris Data.
Rtcm1044(int, Rtcm1044Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044
Constructor.
Rtcm1044Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
Container for RTCM 1044 data.
Rtcm1044Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Constructor.
Rtcm1045 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
RTCM 1045 message: Galileo F/NAV Satellite Ephemeris Data.
Rtcm1045(int, Rtcm1045Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045
Constructor.
Rtcm1045Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
Container for RTCM 1045 data.
Rtcm1045Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Constructor.
RtcmData - Class in org.orekit.gnss.metric.messages.rtcm
Container for common data in RTCM message.
RtcmData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.RtcmData
 
RtcmDataField - Enum in org.orekit.gnss.metric.parser
Enum containing all intermediate level data fields that can be parsed to build a RTCM message.
RtcmEphemerisData - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
Container for common data in RTCM ephemeris message type.
RtcmEphemerisData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
Constructor.
RtcmEphemerisMessage<D extends RtcmEphemerisData> - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris
Base class for RTCM ephemeris messages.
RtcmEphemerisMessage(int, D) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisMessage
Constructor.
RtcmMessage<D extends RtcmData> - Class in org.orekit.gnss.metric.messages.rtcm
Base class for RTCM messages.
RtcmMessage(int, List<D>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.RtcmMessage
Constructor.
RtcmMessagesParser - Class in org.orekit.gnss.metric.parser
Parser for RTCM encoded messages.
RtcmMessagesParser(List<Integer>) - Constructor for class org.orekit.gnss.metric.parser.RtcmMessagesParser
Constructor.
RtcmMessageType - Enum in org.orekit.gnss.metric.parser
Enum containing the supported RTCM messages types.
RTNCovariance - Class in org.orekit.files.ccsds.ndm.cdm
Container for RTN covariance matrix data.
RTNCovariance() - Constructor for class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Simple constructor.
RTNCovarianceKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM covariance matrix entries.
RTNCovarianceWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for RTN covariance matrix data block for CCSDS Conjunction Data Messages.
run() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor
ruToMeters(TdmMetadata, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.tdm.IdentityConverter
Convert a range expressed in Range Units.
ruToMeters(TdmMetadata, AbsoluteDate, double) - Method in interface org.orekit.files.ccsds.ndm.tdm.RangeUnitsConverter
Convert a range expressed in Range Units.

S

S - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
S2 - Static variable in class org.orekit.models.earth.displacement.Tide
S₂ tide.
s4 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
s* new value for the contant s.
s4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
s* new value for the contant s.
S_2FASX4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
S_3FASX6 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
S_FASX2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
S_G22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
S_G32 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
S_G44 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
S_G52 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
S_G54 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
SaastamoinenModel - Class in org.orekit.models.earth.troposphere
The modified Saastamoinen model.
SaastamoinenModel(double, double, double) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel
Create a new Saastamoinen model for the troposphere using the given environmental conditions and table from the reference book.
SaastamoinenModel(double, double, double, String) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel
Create a new Saastamoinen model for the troposphere using the given environmental conditions.
SaastamoinenModel(double, double, double, String, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel
Create a new Saastamoinen model for the troposphere using the given environmental conditions.
sameDimension(Unit) - Method in class org.orekit.utils.units.Unit
Check if a unit has the same dimension as another unit.
sameDimensionSI() - Method in class org.orekit.utils.units.Unit
Create the SI unit with same dimension.
sample(SphericalPolygonsSet, double, double) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Sample a zone of interest into a grid sample of geodetic points.
SatelliteAntenna - Class in org.orekit.gnss.antenna
GNSS satellite antenna model.
SatelliteAntenna(String, String, Map<Frequency, FrequencyPattern>, SatelliteSystem, int, SatelliteType, int, String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.gnss.antenna.SatelliteAntenna
Simple constructor.
SatelliteClockScale - Class in org.orekit.time
Scale for on-board clock.
SatelliteClockScale(String, AbsoluteDate, TimeScale, double, double) - Constructor for class org.orekit.time.SatelliteClockScale
Create a linear model for satellite clock.
SatelliteSystem - Enum in org.orekit.gnss
Enumerate for satellite system.
SatelliteType - Enum in org.orekit.gnss.antenna
Enumerate for satellite types.
SATURN - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Saturn.
SBAS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
WGS 84 value of the Earth's universal gravitational parameter for SBAS user in m³/s².
SBASNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a SBAS navigation message.
SBASNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Constructor.
SBASOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data
This interface provides the minimal set of orbital elements needed by the SBASPropagator.
SBASPropagator - Class in org.orekit.propagation.analytical.gnss
This class aims at propagating a SBAS orbit from SBASOrbitalElements.
SBASPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss
This nested class aims at building a SBASPropagator.
SBASPropagatorBuilder(SBASOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Initializes the builder.
scale(double, Orbit) - Method in enum org.orekit.orbits.OrbitType
Compute scaling factor for parameters drivers.
scale(String, double) - Method in class org.orekit.utils.units.Unit
Scale a unit.
scaleChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter scale has been changed.
ScaledConstantThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion
Thrust propulsion model with parameters (for estimation) represented by scale factors on the X, Y and Z axis of the spacecraft frame.
ScaledConstantThrustPropulsionModel(double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Constructor with min/max deviation for the scale factors.
scaledIncrement(double, DoubleArrayDictionary.Entry) - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
Increment the value with another scaled entry.
scaledIncrement(T, FieldArrayDictionary<T>.Entry) - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Increment the value with another scaled entry.
scaledIncrement(double, FieldArrayDictionary<T>.Entry) - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Increment the value with another scaled entry.
Scheduler<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.generation
Interface for generating measurements sequences.
ScreenVolumeFrame - Enum in org.orekit.files.ccsds.ndm.cdm
Screening volume frame possibilities used in CCSDS Conjunction Data Messages.
ScreenVolumeShape - Enum in org.orekit.files.ccsds.ndm.cdm
Screening volume shape possibilities used in CCSDS Conjunction Data Messages.
SDP4 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Identifier for SDP4 type of ephemeris.
SDP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SDP4 type of ephemeris.
SDP8 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Identifier for SDP8 type of ephemeris.
SDP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SDP8 type of ephemeris.
SEC_TO_MILLI - Static variable in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
Seconds to milliseconds converter.
SECOND - Static variable in class org.orekit.utils.units.Unit
Second unit.
Section - Interface in org.orekit.files.ccsds.section
Top level interface for all CCSDS message sections.
SecularAndHarmonic - Class in org.orekit.utils
Class for fitting evolution of osculating orbital parameters.
SecularAndHarmonic(int, double...) - Constructor for class org.orekit.utils.SecularAndHarmonic
Simple constructor.
Segment<M extends Metadata,D extends Data> - Class in org.orekit.files.ccsds.section
NDM segments are (Metadata, Data) pairs.
Segment(M, D) - Constructor for class org.orekit.files.ccsds.section.Segment
Constructor.
SegmentWriter() - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter
 
SegmentWriter() - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter
 
select(Unit, Unit) - Method in enum org.orekit.files.ccsds.ndm.ParsedUnitsBehavior
Select the unit to use for interpreting parsed value.
select(DataSource) - Static method in class org.orekit.files.ccsds.utils.lexical.LexicalAnalyzerSelector
Select a LexicalAnalyzer for a DataSource based on content.
selectDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.BurstSelector
Select dates within an interval.
selectDates(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.time.DatesSelector
Select dates within an interval.
selectDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.FixedStepSelector
Select dates within an interval.
selectExtrapolator(FieldTLE<T>, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(FieldTLE<T>, Frames, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(FieldTLE<T>, AttitudeProvider, T, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE, Frames) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE, AttitudeProvider, double) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE, AttitudeProvider, double, Frame) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectionChanged(boolean, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter selection status has been changed.
selectPredefined(int, int) - Static method in enum org.orekit.frames.HelmertTransformation.Predefined
Select a predefined transform between two years.
selectTransformer(Transformer, double, boolean) - Method in enum org.orekit.propagation.events.FilterType
Get next function transformer in the specified direction.
SEMI_CIRCLE - Static variable in class org.orekit.gnss.metric.parser.Units
Semi-circles units.
SemiAnalyticalKalmanEstimator - Class in org.orekit.estimation.sequential
Implementation of an Extended Semi-analytical Kalman Filter (ESKF) to perform orbit determination.
SemiAnalyticalKalmanEstimator(MatrixDecomposer, DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
Kalman filter estimator constructor (package private).
SemiAnalyticalKalmanEstimatorBuilder - Class in org.orekit.estimation.sequential
Builder for a Semi-analytical Kalman Filter.
SemiAnalyticalKalmanEstimatorBuilder() - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder
Default constructor.
SemiAnalyticalKalmanModel - Class in org.orekit.estimation.sequential
Process model to use with a SemiAnalyticalKalmanEstimator.
SemiAnalyticalKalmanModel(DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Kalman process model constructor (package private).
SEMParser - Class in org.orekit.gnss
This class reads SEM almanac files and provides GPS almanacs.
SEMParser(String) - Constructor for class org.orekit.gnss.SEMParser
Simple constructor.
SEMParser(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.gnss.SEMParser
Create a SEM loader/parser with the given source of SEM auxiliary data files.
SequentialBatchLSEstimator - Class in org.orekit.estimation.leastsquares
Sequential least squares estimator for orbit determination.
SequentialBatchLSEstimator(SequentialGaussNewtonOptimizer, OrbitDeterminationPropagatorBuilder...) - Constructor for class org.orekit.estimation.leastsquares.SequentialBatchLSEstimator
Simple constructor.
setA(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the orbit semi-major axis.
setA(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
Set acceleration component.
setA2b(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Set rotation direction.
setAcceleration(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set acceleration component.
setAccelerationDirectionSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set one σ angular off-nominal acceleration direction.
setAccelerationInterpolation(OnOff) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set interpolation mode between current and next acceleration line.
setAccelerationMagnitudeSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set one σ percent error on acceleration magnitude.
setAccuracy(int, double) - Method in class org.orekit.files.sp3.SP3
Set the formal accuracy for a satellite.
setAccuracy(double) - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
Set the accuracy for this satellite.
setAccuracyProvider(AccuracyProvider) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
Set the accuracy provider of the ephemeris message.
setActualOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the actual OD time based on the observations available and the RECOMMENDED_OD_SPAN.
setActualOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set actual time span used for the OD of the object.
setAdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the Unique identifier of Attitude Data Message linked to this Orbit Data Message.
setAe(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the central body reference radius.
setAf0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the SV Clock Bias Correction Coefficient (s).
setAf1(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the SV Clock Drift Correction Coefficient (s/s).
setAf2(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Drift Rate Correction Coefficient (s/s²).
setAgency(String) - Method in class org.orekit.files.sp3.SP3
Set the agency string for this SP3 file.
setAgencyName(String) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the agency name.
setAgencyName(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Setter for the agency name.
setAGf0(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Setter for the SV clock bias.
setAGf1(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Setter for the SV relative frequency.
setAlbedoGridSize(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set albedo grid size.
setAlbedoModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set albedo model.
setAlternateNames(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the alternate names for this space object.
setAmplifierBandwidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the amplifier bandwidth.
setAmplifierGain(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the amplifier gain.
setAmplifierInUse(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the amplifier in use.
setAnalysisCenterID(String) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the analysis center ID.
setAnalysisCenterName(String) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the analysis center name.
setAngleType(AngleType) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the angleType.
setAngularThreshold(double) - Method in class org.orekit.bodies.OneAxisEllipsoid
Set the angular convergence threshold.
setAnomaly(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the orbit anomaly.
setAnomalyType(PositionAngle) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the type of anomaly.
setAODC(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
Setter for the age of data clock.
setAODE(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
Setter for the age of data ephemeric.
setApplicableWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the applicable wavelength.
setAppliedVoltage(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the applied voltage.
setAreAdditionalDataAvailable(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the flag indicating if additional parameters are in the message.
setAreaDRG(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the effective area of the object exposed to atmospheric drag.
setAreaPC(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the actual area of the object.
setAreaSRP(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the effective area of the object exposed to solar radiation pressure.
setAtmosphericModel(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set name of atmospheric model.
setAtmosphericModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set name of atmospheric model.
setAttitudeActuatorType(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the type of actuator for attitude control.
setAttitudeControlAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the accuracy of attitude control.
setAttitudeControlMode(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the attitude control mode.
setAttitudeKnowledgeAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the accuracy of attitude knowledge.
setAttitudePointingAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the overall accuracy of spacecraft to maintain attitude.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.AbstractPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Set the attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.FieldAbstractPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.FieldPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.StateMapper
Set the attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.Propagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set attitude provider.
setAttitudeType(AttitudeType) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set the format of the data lines in the message.
setBeamDivergence(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the beam divergence.
setBeidouNavigationMessage(BeidouNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Set the Beidou navigation message.
setBeidouToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Set the Beidou time of clock.
setBGDE1E5a(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Setter for the E1/E5a broadcast group delay (s).
setBGDE5bE1(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Setter for the E5b/E1 broadcast group delay (s).
setBN(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS Bn Word.
setBolDv(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the total ΔV capability at beginning of life.
setBStar(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the SGP/SGP4 drag-like coefficient.
setBusModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the bus model name.
setCacheSlotsNumber(int) - Static method in class org.orekit.utils.OrekitConfiguration
Set the number of slots to use in caches.
setCatalogName(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the satellite catalog name used for object.
setCatalogName(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the specification of satellite catalog source.
setCDAreaOverMass(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the object’s Cd x A/m used to propagate the state vector and covariance to TCA.
setCdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the Unique identifier of Conjunction Data Message linked to this Orbit Data Message.
setCdrgdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [7,7] in covariance matrix (with index starting at 1).
setCdrgn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [7,3] in covariance matrix (with index starting at 1).
setCdrgndot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [7,6] in covariance matrix (with index starting at 1).
setCdrgr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [7,1] in covariance matrix (with index starting at 1).
setCdrgrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [7,4] in covariance matrix (with index starting at 1).
setCdrgt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [7,2] in covariance matrix (with index starting at 1).
setCdrgtdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [7,5] in covariance matrix (with index starting at 1).
setCelestialSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the source and version of celestial body (e.g.
setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Set the body at origin of reference frame.
setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Set the origin of reference frame.
setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set the origin of reference frame.
setCenterOfMassOffset(double) - Method in class org.orekit.files.ilrs.CPFHeader
Set the approximate center of mass to reflector offset.
setCentralBodyRotation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set central body angular rotation rate.
setCic(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for te Cic parameter.
setCis(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Cis parameter.
setClassification(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the message classification.
setClassificationType(char) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the classification type.
setClockCorrection(ClockCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data
Set the clock correction data.
setClockCorrection(ClockCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
Set the clock correction data.
setClosedOrbitConstraint(boolean) - Method in class org.orekit.utils.AbstractMultipleShooting
Set the constraint of a closed orbit or not.
setCndotn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [6,3] in covariance matrix (with index starting at 1).
setCndotndot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [6,6] in covariance matrix (with index starting at 1).
setCndotr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [6,1] in covariance matrix (with index starting at 1).
setCndotrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [6,4] in covariance matrix (with index starting at 1).
setCndott(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [6,2] in covariance matrix (with index starting at 1).
setCndottdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [6,5] in covariance matrix (with index starting at 1).
setCnm(double[][]) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Set the cosine parameters of spherical harmonics expansion of degree N and order M.
setCnn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [3,3] in covariance matrix (with index starting at 1).
setCnr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [3,1] in covariance matrix (with index starting at 1).
setCnt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [3,2] in covariance matrix (with index starting at 1).
setCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the probability (between 0.0 and 1.0) that Object1 and Object2 will collide.
setCollisionProbaMethod(PocMethodFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the method that was used to calculate the collision probability.
setComparator(Comparator<IntegerLeastSquareSolution>) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Set a custom comparator for integer least square solutions comparison.
setConfidence(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set confidence metric.
setConfigurationRecords(CRDConfiguration) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Set the configuration records for the current data block.
setConsiderN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set number of consider parameters.
setConsiderParameters(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set description of consider parameters.
setConstellation(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the name of the constellation this space object belongs to.
setContext(ContextBinding) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Reset context binding.
setContext(ContextBinding) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Reset context binding.
setConvergenceChecker(ConvergenceChecker<LeastSquaresProblem.Evaluation>) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set a custom convergence checker.
setConvergenceRMS(double) - Method in class org.orekit.utils.SecularAndHarmonic
Set RMS for convergence.
setCoordinateSystem(String) - Method in class org.orekit.files.sp3.SP3
Set the coordinate system used for the orbit entries.
setCorrectionAberrationDiurnal(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the diurnal aberration correction.
setCorrectionAberrationYearly(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the yearly aberration correction.
setCorrectionAngle1(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the correctionAngle1.
setCorrectionAngle2(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the correctionAngle2.
setCorrectionDoppler(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the correctionDoppler.
setCorrectionMagnitude(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the magnitude correction.
setCorrectionRcs(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the radar cross section correction.
setCorrectionReceive(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the correctionReceive.
setCorrectionsApplied(CorrectionApplied) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the correctionApplied.
setCorrectionTransmit(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the correctionTransmit.
setCountry(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the name of the country where the space object owner is based.
setCovarianceMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set an entry in the RTN covariance matrix.
setCovarianceMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Set an entry in the Position/Velocity covariance matrix.
setCovarianceMethod(CovarianceMethod) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the method name used to calculate covariance during OD.
setCovBasis(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Set basis of this covariance time history data.
setCovBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Set identification number of the orbit determination or simulation upon which this covariance is based.
setCovConfidence(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Set the measure of confidence in covariance error matching reality.
setCovFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Set epoch of the covariance reference frame.
setCovID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Set covariance identification number.
setCovNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Set identification number of next covariance.
setCovOrdering(Ordering) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Set covariance ordering.
setCovPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Set identification number of previous covariance.
setCovReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Set reference frame of the covariance.
setCovScaleMax(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Set the maximum scale factor to apply to achieve realism.
setCovScaleMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Set the minimum scale factor to apply to achieve realism.
setCovType(ElementsType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Set covariance element set type.
setCovUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Set covariance element set units.
setCRAreaOverMass(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the object’s Cr x A/m used to propagate the state vector and covariance to TCA.
setCrc(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Crc parameter.
setCrdotn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [4, 3] in covariance matrix (with index starting at 1).
setCrdotr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [4,1] in covariance matrix (with index starting at 1).
setCrdotrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [4, 4] in covariance matrix (with index starting at 1).
setCrdott(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [4, 2] in covariance matrix (with index starting at 1).
setCreationDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.section.Header
Set the file creation date and time in UTC.
setCreationDate(AbsoluteDate) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the creation date.
setCreationDate(AbsoluteDate) - Method in class org.orekit.gnss.navigation.RinexNavigation
Setter for the creation date.
setCreationDateString(String) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the creation date as a string.
setCreationDateString(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Setter for the creation date as a string.
setCreationTimeString(String) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the creation time as a string.
setCreationTimeString(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Setter for the creation time as a string.
setCreationTimeZoneString(String) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the creation time zone.
setCreationTimeZoneString(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Setter for the creation time zone.
setCrr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [1,1] in covariance matrix (with index starting at 1).
setCrs(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Crs parameter.
setCrsIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header
Set the Global/Regional CRS Indicator.
setCrsIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header
Set the Global/Regional CRS Indicator.
setCsrpdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,7] in covariance matrix (with index starting at 1).
setCsrpn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,3] in covariance matrix (with index starting at 1).
setCsrpndot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,6] in covariance matrix (with index starting at 1).
setCsrpr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,1] in covariance matrix (with index starting at 1).
setCsrprdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,4] in covariance matrix (with index starting at 1).
setCsrpsrp(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,8] in covariance matrix (with index starting at 1).
setCsrpt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,2] in covariance matrix (with index starting at 1).
setCsrptdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [8,5] in covariance matrix (with index starting at 1).
setCtdotn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [5,3] in covariance matrix (with index starting at 1).
setCtdotr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [5,1] in covariance matrix (with index starting at 1).
setCtdotrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [5,4] in covariance matrix (with index starting at 1).
setCtdott(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [5,2] in covariance matrix (with index starting at 1).
setCtdottdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [5,5] in covariance matrix (with index starting at 1).
setCthrdrg(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,7] in covariance matrix (with index starting at 1).
setCthrn(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,3] in covariance matrix (with index starting at 1).
setCthrndot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,6] in covariance matrix (with index starting at 1).
setCthrr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,1] in covariance matrix (with index starting at 1).
setCthrrdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,4] in covariance matrix (with index starting at 1).
setCthrsrp(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,8] in covariance matrix (with index starting at 1).
setCthrt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,2] in covariance matrix (with index starting at 1).
setCthrtdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,5] in covariance matrix (with index starting at 1).
setCthrthr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [9,9] in covariance matrix (with index starting at 1).
setCtr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [2,1] in covariance matrix (with index starting at 1).
setCtt(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Set the object [2,2] in covariance matrix (with index starting at 1).
setCuc(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Cuc parameter.
setCus(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Cus parameter.
setDarkCount(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the dark count.
setDataQuality(DataQuality) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the dataQuality.
setDataReleaseFlag(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the flag indicating the data release.
setDataType(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the data type.
setDataTypes(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set observation data types used.
setDataTypes(List<ObservationType>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the data types in the data section.
setDataUsed(String) - Method in class org.orekit.files.sp3.SP3
Set the data used indicator for this SP3 file.
setDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set date.
setDate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the reference date of the ephemeris.
setDate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the reference epoch.
setDateAndTime(String) - Method in class org.orekit.files.ilrs.CRDHeader
Set the string value of date and time.
setDayFraction(double) - Method in class org.orekit.files.sp3.SP3
Set the day fraction for this SP3 file.
setDcBodyFrame(SpacecraftBodyFrame) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set spacecraft body frame in which ManeuverHistoryMetadata.getDcBodyTrigger() is specified.
setDcBodyTrigger(Vector3D) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set direction in body frame for triggering duty cycle.
setDcExecStart(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set the start time of initial duty cycle-based maneuver execution.
setDcExecStop(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set the end time of final duty cycle-based maneuver execution.
setDcMaxCycles(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set the maximum number of "ON" duty cycles.
setDcMinCycles(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set the minimum number of "ON" duty cycles.
setDcPhaseStartAngle(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set phase angle of pulse start.
setDcPhaseStopAngle(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set phase angle of pulse stop.
setDcRefDir(Vector3D) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set reference direction for triggering duty cycle.
setDcRefTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set duty cycle thrust reference time.
setDcTimePulseDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set duty cycle pulse "ON" duration.
setDcTimePulsePeriod(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set duty cycle elapsed time between start of a pulse and start of next pulse.
setDcType(DutyCycleType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set type of duty cycle.
setDcWindowClose(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set the end time of duty cycle-based maneuver window.
setDcWindowOpen(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set the start time of duty cycle-based maneuver window.
setDefault(LazyLoadedDataContext) - Static method in interface org.orekit.data.DataContext
Set the default data context that is used to implement Orekit's static factories.
setDeltaInc(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Sets the the correction of orbit reference inclination at reference time.
setDeltaMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set mass change.
setDeltaMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Set mass change during maneuver (value is < 0).
setDeltaN(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the delta of satellite mean motion.
setDeltaSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Sets the difference between the square root of the semi-major axis and the square root of the nominal semi-major axis.
setDeltaTN(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the deltaTauN value.
setDeployDirSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set one σ angular off-nominal deployment vector direction.
setDeployDv(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set velocity increment component of deployed "child" object.
setDeployDvCda(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.
setDeployDvRatio(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set ratio of child-to-host ΔV vectors.
setDeployDvSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set one σ percent error on deployment ΔV magnitude.
setDeployId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set identifier of resulting "child" object deployed from this host.
setDeployMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set decrement in host mass as a result of deployment.
setDetectorId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the detector configuration ID.
setDetectorRecord(CRDConfiguration.DetectorConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Set the detector configuration record.
setDetectorType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the detector type.
setDockedWith(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the other space objects this object is docked to.
setDomes(String) - Method in class org.orekit.files.sinex.Station
Set the DOMES number.
setDopplerCountBias(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Set the Doppler count bias.
setDopplerCountRollover(boolean) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Set the indicator for Doppler count rollover.
setDopplerCountScale(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Set the Doppler count Scale.
setDragArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Set the drag area.
setDragCoeff(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Set the drag coefficient.
setDragCoefficient(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the the nominal drag coefficient.
setDragConstantArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
setDragUncertainty(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the drag coefficient 1σ uncertainty.
setDryMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the mass without propellant.
setDuration(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Set duration (value is 0 for impulsive maneuver).
setDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set duration.
setDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Set duration (value is 0 for impulsive maneuver).
setDv(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set velocity increment component.
setDV(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Set velocity increment component.
setDvDirSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set one σ angular off-nominal ΔV direction.
setDvMagSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set one σ percent error on ΔV magnitude.
setE(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the orbit eccentricity.
setE(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter the eccentricity.
setEarthTides(boolean) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set boolean that indicates if Earth and ocean tides are taken into account or not.
setEccentricities(Vector3D) - Method in class org.orekit.files.sinex.Station
Set the last known station antenna eccentricities.
setEccRefSystem(Station.ReferenceSystem) - Method in class org.orekit.files.sinex.Station
Set the reference system used to define the eccentricity vector (local or cartesian).
setElem(int, int, PolynomialFunction) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Set an element of the matrix.
setElementSetNo(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the element set number for this satellite.
setEn(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the GLONASS En Word.
setEnabled(boolean) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Enable or disable a measurement.
setEnabled(boolean) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Enable or disable a measurement.
setEndEpoch(AbsoluteDate) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the ending epoch (UTC).
setEndTagSeen(boolean) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Set the flag for XML end tag.
setEOPContinuityThreshold(double) - Static method in class org.orekit.frames.FramesFactory
Set the threshold to check EOP continuity.
setEOPContinuityThreshold(double) - Method in class org.orekit.frames.LazyLoadedEop
Set the threshold to check EOP continuity.
setEOPContinuityThreshold(double) - Method in class org.orekit.frames.LazyLoadedFrames
Set the threshold to check EOP continuity.
setEopSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the source and version of Earth Orientation Parameters.
setEphemerisNames(Map<Integer, String>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the external ephemeris names for participants.
setEphemerisType(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the ephemeris type.
setEphemName(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the name of external ephemeris used for OD.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Set the epoch of the data.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Set matrix epoch.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set epoch of state vector, Keplerian elements and covariance matrix data.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set time tag for orbit determination solved-for state.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
Set epoch of state vector, Keplerian elements and covariance matrix data.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Set the coordinates reference epoch.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.sp3.SP3
Set the epoch of the SP3 file.
setEpochDelayCorrection(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Set the epoch delay correction.
setEpochEigenInt(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set positional error ellipsoid 1σ intermediate eigenvalue at the epoch of OD.
setEpochEigenMaj(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set positional error ellipsoid 1σ major eigenvalue at the epoch of OD.
setEpochEigenMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set positional error ellipsoid 1σ minor eigenvalue at the epoch of OD.
setEpochFreedom(int, boolean) - Method in class org.orekit.utils.AbstractMultipleShooting
Set the epoch a patch point to free or not.
setEpochIdentifier(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the epoch identifier.
setEpochIgnition(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Set epoch ignition.
setEpochInterval(double) - Method in class org.orekit.files.sp3.SP3
Set the epoch interval for this SP3 file.
setEpochStart(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Set epoch start.
setEpochT0(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the epoch to which all relative times are referenced in data blocks.
setEpochToc(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the time of clock epoch.
setEpochToc(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the time of clock epoch.
setEquatorialRadius(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set oblate spheroid equatorial radius of central body.
setEstimatedValue(double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Set the estimated value.
setEulerRotSeq(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set the rotation order for Euler angles.
setEulerRotSeq(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Set the rotation order for Euler angles.
setEvaluationsCounter(Incrementor) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Set the counter for evaluations.
setExternalClockReference(String) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the external clock reference.
setExternalSignalProcessing(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the external signal processing.
setFallback(ProcessingState) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Set fallback processing state.
setFileType(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Setter for the file type.
setFilter(CartesianDerivativesFilter) - Method in class org.orekit.files.ilrs.CPF
Set the derivatives filter.
setFilter(CartesianDerivativesFilter) - Method in class org.orekit.files.sp3.SP3
Set the derivatives filter.
setFiring(boolean, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Set the firing start or end date depending on the firing flag.
setFix(int, int, double, double, double, double, double) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Set GPS fix data to send as NMEA sentence to Ntrip caster if required.
setFixedF10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux Unit daily proxy F10.7.
setFixedF10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux Unit 81-day running center-average proxy F10.7.
setFixedGeomagneticAp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the planetary 3-hour-range geomagnetic index aₚ.
setFixedGeomagneticDst(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the planetary 1-hour-range geomagnetic index Dst.
setFixedGeomagneticKp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the planetary 3-hour-range geomagnetic index Kₚ.
setFixedM10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux daily proxy M10.7.
setFixedM10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy M10.7.
setFixedS10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux daily proxy S10.7.
setFixedS10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy S10.7.
setFixedY10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux daily proxy Y10.7.
setFixedY10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy Y10.7.
setFormat(String) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the file format.
setFormatVersion(double) - Method in class org.orekit.files.ccsds.section.Header
Set the CCSDS NDM (ADM, ODM or TDM) format version.
setFormatVersion(double) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the format version.
setFormatVersion(double) - Method in class org.orekit.gnss.navigation.RinexNavigation
Setter for the format version.
setFrameA(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Set frame A.
setFrameB(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
Set frame B.
setFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Set epoch of reference frame, if not intrinsic to the definition of the reference frame.
setFrameEpochString(String) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Set epoch of reference frame, if not intrinsic to the definition of the reference frame.
setFrameName(String) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the frame name.
setFreqOffset(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the freqOffset.
setFrequencyNumber(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Setter for the frequency number.
setFrequencySource(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Set the frequency source.
setFT(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS FT Word.
setGalileoDataValidityStatus(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Set the Galileo data validity status.
setGalileoNavigationMessage(GalileoNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Set the Galileo navigation message.
setGalileoToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
Set the Galileo time of clock.
setGammaN(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Setter for the SV relative frequency bias.
setGdop(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set generalize Dilution Of Precision.
setGlonassNavigationMessage(GLONASSNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the Glonass navigation message.
setGm(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set gravitational coefficient of attracting body.
setGnssIod(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
Set the GNSS IOD.
setGnssIod(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
Set the GNSS IOD.
setGpsCodeOnL2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Set the GPS code on L2.
setGpsFitInterval(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Set the GPS fit interval.
setGpsL2PDataFlag(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Set the GPS L2 P-code data flag.
setGpsNavigationMessage(GPSNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Set the GPS navigation message.
setGpsToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
Set the GPS time of clock.
setGpsWeek(int) - Method in class org.orekit.files.sp3.SP3
Set the GPS week of the SP3 file.
setGravitationalAssist(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set the origin of gravitational assist.
setGravityModel(String, int, int) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set gravity model.
setGravityModel(String, int, int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set gravity model.
setHandlers(List<EventHandler<D>>) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Change handlers list with user input.
setHarvesters(MatricesHarvester[]) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Setter for the jacobian harvesters.
setHeader(CRDHeader) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Set the header for the current data block.
setHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the health status.
setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
Sets the health status.
setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Sets the health status.
setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
Sets the health status.
setHealthAvailabilityIndicator(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the flag indicating if GLONASS almanac health is available.
setHealthE1(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Sets the E1-B/C signal health status.
setHealthE5a(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Sets the E5a signal health status.
setHealthE5b(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Sets the E5b signal health status.
setHeightIonosphericLayer(double) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Set the height of the ionospheric layer.
setHighRateClockCorrection(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data
Set the high rate clock correction to be added to the polynomial clock correction.
setHumiSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the humidity sensor manufacturer.
setHumiSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the humidity sensor model.
setHumiSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the humidity sensor serial number.
setI(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the orbit inclination.
setI0(double, double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
Sets the Inclination Angle at Reference Time (rad).
setI0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the Inclination Angle at Reference Time (rad).
setI11(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Set the moment of Inertia about the 1-axis (N.m²).
setI12(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Set the moment of Inertia about the 1 and 2 axes (N.m²).
setI13(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Set the moment of Inertia about the 1 and 3 axes (N.m²).
setI22(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Set the moment of Inertia about the 2-axis (N.m²).
setI23(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Set the moment of Inertia about the 2 and 3 axes (N.m²).
setI33(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Set the moment of Inertia about the 3-axis (N.m²).
setId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set identification number.
setIDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Rate of Inclination Angle (rad/s).
setIgnoreCentralAttraction(boolean) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set the flag to ignore or not the creation of a NewtonianAttraction.
setIgnoreCentralAttraction(boolean) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the flag to ignore or not the creation of a NewtonianAttraction.
setIlrsSatelliteId(String) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the IRLS satellite ID (based on COSPAR ID).
setInertiaMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set an entry in the inertia matrix.
setInertiaReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Set the coordinate system for the inertia tensor.
setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.analytical.tle.TLEJacobiansMapper
Set the Jacobian with respect to state into a one-dimensional additional state array.
setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations
Deprecated.
Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations
Deprecated.
Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Set the Jacobian with respect to state into a one-dimensional additional state array.
setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.numerical.JacobiansMapper
Set the Jacobian with respect to state into a one-dimensional additional state array.
setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Deprecated.
Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Deprecated.
Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
Set the Jacobian with respect to state into a one-dimensional additional state array.
setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Deprecated.
Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Deprecated.
Set the initial value of the Jacobian with respect to state and parameter.
setInitialPhi(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Method adding the standard initial values of the additional state to the initial spacecraft state.
setInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set the initial state.
setInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the initial state.
setInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the initial state with osculating orbital elements.
setInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the initial state.
setInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the initial state with osculating orbital elements.
setInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the initial state.
setInitialWetMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the total mass at beginning of life.
setInRotationAngles(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Set flag for rotation angle parsing.
setIntegrationInterval(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the integrationInterval.
setIntegrationRef(IntegrationReference) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the integrationRef.
setInternationalDes(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the international designator used for object.
setInternationalDesignator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the international designator for the object.
setInterpMethodEOP(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the interpolation method for Earth Orientation Parameters.
setInterpMethodSW(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set the interpolation method for Space Weather data.
setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set the interpolation degree.
setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set the interpolation degree.
setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Set the interpolation degree.
setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Set the interpolation degree.
setInterpolationGridToFixedNumberOfPoints(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the interpolation grid generator.
setInterpolationGridToFixedNumberOfPoints(int) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the interpolation grid generator.
setInterpolationGridToMaxTimeGap(double) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the interpolation grid generator.
setInterpolationGridToMaxTimeGap(T) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the interpolation grid generator.
setInterpolationMethod(String) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set the interpolation method to be used.
setInterpolationMethod(InterpolationMethod) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set the interpolation method to be used.
setInterpolationMethod(InterpolationMethod) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Set the interpolation method to be used.
setInterpolationMethod(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Set the interpolation method to be used.
setInterpolationSample(int) - Method in class org.orekit.files.ilrs.CPF
Set the interpolation sample.
setIntrackThrust(boolean) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set boolean that indicates if intrack thrust modeling was into account or not.
setIOD(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
Sets the Issue of Data (IOD).
setIODC(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
Setter for the Issue of Data Clock.
setIODC(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
Setter for the Issue of Data, Clock.
setIODE(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
Setter for the Issue of Data Ephemeris.
setIODE(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
Setter for the Issue of Data, Ephemeris.
setIODEC(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Setter for the Issue of Data, Ephemeris and Clock.
setIODN(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Setter for the issue of data navigation.
setIODNav(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Setter for the Issue of Data of the navigation batch.
setIodSsr(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Set the IOD SSR.
setIonosphericCorrectionType(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Setter for the ionospheric correction type.
setIsCenterOfMassCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CPFHeader
Set the flag telling if the center of mass correction is applied.
setIsCenterOfMassCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
Set the center of mass correction applied indicator.
setIsCompatibleWithTIVs(boolean) - Method in class org.orekit.files.ilrs.CPFHeader
Set the flag for compatibility with TIVs.
setIsConsistencyMaintained(boolean) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header
Set the flag indicating if phase biases maintain consistency between non-dispersive and all original dispersive phase signals.
setIsFirst(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set the flag for the placement of the quaternion QC in the attitude data.
setIsMelbourneWubbenaConsistencyMaintained(boolean) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header
Set the flag indicating if consistency between code and phase biases is maintained for the MW combinations.
setIsReceiveAmplitudeCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
Set the receive amplitude correction applied indicator.
setIsSpacecraftTimeSimplified(boolean) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the spacecraft time simplified flag.
setIsStationSystemDelayApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
Set the station system delay applied indicator.
setIsTransponderDelayApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
Set the spacecraft system delay applied (transponders) indicator.
setIsTroposphericRefractionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
Set the tropospheric refraction correction applied indicator.
setIterationsCounter(Incrementor) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Set the counter for iterations.
setITRFVersion(int) - Method in class org.orekit.files.sinex.SinexLoader
Set the ITRF version used in EOP entries processing.
setJulianDay(int) - Method in class org.orekit.files.sp3.SP3
Set the julian day for this SP3 file.
setKlobucharAlpha(double[]) - Method in class org.orekit.gnss.navigation.RinexNavigation
Set the "alpha" ionspheric parameters.
setKlobucharBeta(double[]) - Method in class org.orekit.gnss.navigation.RinexNavigation
Set the "beta" ionospheric parameters.
setLaserId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the laser configuration ID.
setLaserRecord(CRDConfiguration.LaserConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Set the laser configuration record.
setLaserType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the laser type.
setLNFifthString(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS ln Word extracted from fifth string of the subframe.
setLNThirdString(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS ln Word extracted from third string of the subframe.
setLocalTimingId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Set the local timing system configuration ID.
setLod(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the length of day.
setLowElevationThreshold(double) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
Set the low elevation threshold value for path delay computation.
setM(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS M Word.
setM0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the Mean Anomaly at Reference Time (rad).
setMainFieldCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField
Set the given main field coefficients.
setManBasis(ManBasis) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set basis of this maneuver history data.
setManBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set identification number of the orbit determination or simulation upon which this maneuver is based.
setManComposition(List<ManeuverFieldType>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set maneuver element of information.
setManDeviceID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set identifier of the device used for this maneuver.
setManeuverable(Maneuvrable) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the object maneuver ability.
setManeuversFrequency(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the average frequency of orbit or attitude maneuvers (in SI units, hence per second).
setManFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set epoch of the maneuver reference frame.
setManID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set maneuver identification number.
setManNextEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set start time of next maneuver.
setManNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set identification number of next maneuver.
setManPredSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set prediction source on which this maneuver is based.
setManPrevEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set completion time of previous maneuver.
setManPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set identification number of previous maneuver.
setManPurpose(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set the purposes of the maneuver.
setManReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set reference frame of the maneuver.
setManufacturer(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set manufacturer name.
setManUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Set maneuver element of information units.
setMappers(AbstractJacobiansMapper[]) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Deprecated.
setMass(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the mass of the object.
setMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Set the spacecraft mass.
setMass(double) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Set the initial mass.
setMass(double) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Set the initial mass.
setMatrix(PolynomialFunction[][]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Set values for all elements.
setMatrixLine(int, PolynomialFunction[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Set the value of a line of the matrix.
setMaxAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the maximum cross-sectional area for collision probability estimation purposes.
setMaxEvaluations(int) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set the maximum number of model evaluations.
setMaximumObsGap(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set maximum time between observations in the OD of the object.
setMaxIter(int) - Method in class org.orekit.utils.SecularAndHarmonic
Set maximum number of iterations.
setMaxIterations(int) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set the maximum number of iterations.
setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Set the degree limit for the next file parsing.
setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the degree limit for the next file parsing.
setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Set the order limit for the next file parsing.
setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the order limit for the next file parsing.
setMaxPredictedEigenMaj(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set maximum predicted major eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
setMaxRcs(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the maximum radar cross-section.
setMaxThrust(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the maximum composite thrust the spacecraft can accomplish.
setMaxValue(double) - Method in class org.orekit.utils.ParameterDriver
Set maximum parameter value.
setMeanElementTheory(String) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
Set the description of the Mean Element Theory.
setMeanMotion(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the orbit mean motion.
setMeanMotionDot(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the first time derivative of the mean motion.
setMeanMotionDotDot(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the second time derivative of the mean motion.
setMessageFor(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmHeader
Set the spacecraft name for which the CDM is provided stored in MESSAGE_FOR key.
setMessageId(String) - Method in class org.orekit.files.ccsds.section.Header
Set the ID that uniquely identifies a message from a given originator.
setMeteorologicalId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the meteorological configuration ID.
setMeteorologicalRecord(CRDConfiguration.MeteorologicalConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Set the meteorological record.
setMethod(OdMethodFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set orbit determination method.
setMinAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the minimum cross-sectional area for collision probability estimation purposes.
setMinPredictedEigenMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set minimum predicted minor eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
setMinRcs(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the minimum radar cross-section.
setMinValue(double) - Method in class org.orekit.utils.ParameterDriver
Set minimum parameter value.
setMissDistance(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the norm of relative position vector at TCA.
setMode(TrackingMode) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the mode.
setMu(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the gravitational coefficient.
setMu(double) - Method in class org.orekit.files.ilrs.CPF
Set the gravitational coefficient.
setMu(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the central body attraction coefficient.
setMu(double) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set the central attraction coefficient μ.
setMu(T) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set the central attraction coefficient μ.
setMu(T) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set the central attraction coefficient μ.
setMu(double) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the central attraction coefficient μ.
setMu(double) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the central attraction coefficient μ.
setMu(T) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the central attraction coefficient μ.
setMuCreated(double) - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
Set the gravitational coefficient created from the knowledge of the central body.
setMuParsed(double) - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
Set the gravitational coefficient parsed in the ODM File.
setN4(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the four-year interval number starting from 1996.
setNA(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS NA Word.
setName(int, SatelliteSystem) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Create the name of a satellite from its PRN number and satellite System it belongs to.
setName(String) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the satellite target name.
setName(String) - Method in class org.orekit.utils.ParameterDriver
Change the name of this parameter driver.
setNBodyPerturbations(List<BodyFacade>) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set n-body perturbation bodies.
setNBodyPerturbations(List<BodyFacade>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set n-body perturbation bodies.
setNeQuickAlpha(double[]) - Method in class org.orekit.gnss.navigation.RinexNavigation
Set the "alpha" ionospheric parameters.
setNextLeapEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the epoch of next leap second.
setNextLeapTaimutc(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the difference (TAI – UTC) in seconds incorporated at epoch OcmMetadata.getNextLeapEpoch().
setNextMessageEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the creation date of next message from a given originator.
setNextMessageID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the unique ID identifying next message from a given originator.
setNominalFireRate(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the nominal fire rate.
setNoradID(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the NORAD Catalog Number ("Satellite Number").
setNoradId(String) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the satellite NORAD ID.
setNormalizedValue(double) - Method in class org.orekit.utils.ParameterDriver
Set normalized value.
setNt(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the current date.
setNumberOfBiasesProcessed(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
Set the number of biases processed for the current satellite.
setNumberOfBiasesProcessed(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Set the number of biases processed for the current satellite.
setNumberOfEpochs(int) - Method in class org.orekit.files.sp3.SP3
Set the number of epochs as contained in the SP3 file.
setNumberOfIonosphericLayers(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
Set the number of ionospheric layers.
setNumberOfLeapSeconds(int) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the number of leap seconds.
setNumberOfLeapSeconds(int) - Method in class org.orekit.gnss.navigation.RinexNavigation
Setter for the current number of leap seconds.
setNumberOfLeapSecondsGNSS(int) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the number of leap seconds for GNSS time scales.
setNumberOfSatellites(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader
Set the number of satellites for the current IGM message.
setNutation(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the nutation angle of spin axis (rad).
setNutationPeriod(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the body nutation period of the spin axis (s).
setNutationPhase(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the inertial nutation phase (rad).
setNutLn(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the nutation correction in longitude.
setNutOb(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the nutation correction in obliquity.
setNutX(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the nutation correction X.
setNutY(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the nutation correction Y.
setObject(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the object name for which metadata are given.
setObjectDesignator(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the satellite designator for the object for which metadata are given.
setObjectDesignator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the unique satellite identification designator for the object.
setObjectID(String) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Set the spacecraft ID for which the attitude data are provided.
setObjectID(String) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Set the spacecraft ID for which the orbit state is provided.
setObjectName(String) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Set the spacecraft name for which the attitude data are provided.
setObjectName(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the spacecraft name used for object.
setObjectName(String) - Method in class org.orekit.files.ccsds.ndm.odm.OdmMetadata
Set the spacecraft name for which the orbit state is provided.
setObjectType(ObjectType) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the type of object.
setObjectType(ObjectType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the type of object.
setOblateFlattening(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set central body oblate spheroid oblateness.
setObsAvailable(int) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the number of observations available for the OD of the object.
setObsAvailable(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set number of observations available within the actual OD span.
setObservations(List<Observation>) - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock
Set the list of Observations Data Lines.
setObserver(BatchLSObserver) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set an observer for iterations.
setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Set the observer.
setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
Set the observer.
setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Set the observer.
setObsUsed(int) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the number of observations accepted for the OD of the object.
setObsUsed(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set number of observations accepted within the actual OD span.
setOceanTidesModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set ocean tides model.
setOcmDataElements(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the list of elements of information data blocks included in this message.
setOebAreaAlongIntermediate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the cross-sectional area of Optimally Enclosing Box along Y-OEB.
setOebAreaAlongMax(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the cross-sectional area of Optimally Enclosing Box along X-OEB.
setOebAreaAlongMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the cross-sectional area of Optimally Enclosing Box along Z-OEB.
setOebIntermediate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
setOebMax(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the dimensions of Optimally Enclosing Box along X-OEB (i.e max).
setOebMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the dimensions of Optimally Enclosing Box along Z-OEB (i.e min).
setOebParentFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the Optimally Enclosing Box parent reference frame.
setOebParentFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the Optimally Enclosing Box parent reference frame epoch.
setOebQ(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
set the component of quaternion defining Optimally Enclosing Box.
setOmega0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the Longitude of Ascending Node of Orbit Plane at Weekly Epoch (rad).
setOmegaDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the rate of Rate of Right Ascension (rad/s).
setOperator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the operator of the space object.
setOperatorContactPosition(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the contact position for the object owner / operator.
setOperatorEmail(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the object operator email.
setOperatorOrganization(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the contact organisation of the object.
setOperatorPhone(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the operator phone of the object.
setOpsStatus(OpsStatus) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the operational status.
setOrbAveraging(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set type of averaging (Osculating, mean Brouwer, other.
setOrbitCategory(OrbitCategory) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the orbit category.
setOrbitCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the central body name for object 1 and 2.
setOrbitCorrection(OrbitCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
Set the orbit correction data.
setOrbitCorrection(OrbitCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
Set the orbit correction data.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set propagation orbit type.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set propagation orbit type.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set propagation orbit type.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set propagation orbit type.
setOrbitTypeKey(String) - Method in class org.orekit.files.sp3.SP3
Set the orbit type key for this SP3 file.
setOrbRevNum(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set the integer orbit revolution number.
setOrbRevNumBasis(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set the basis for orbit revolution number.
setOriginator(String) - Method in class org.orekit.files.ccsds.section.Header
Set the file originator.
setOriginatorAddress(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the address of Programmatic Point Of Contact at originator.
setOriginatorEmail(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the email address of Programmatic Point Of Contact at originator.
setOriginatorPhone(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the phone number of Programmatic Point Of Contact at originator.
setOriginatorPOC(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the programmatic Point Of Contact at originator.
setOriginatorPosition(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the position of Programmatic Point Of Contact at originator.
setOutputPulseType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the output pulse type.
setOutputPulseWidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the output pulse width.
setOwner(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the owner of the space object.
setP(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
Set position component.
setP(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS P Word.
setP1(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS P1 Word.
setP2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS P2 Word.
setP3(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the the GLONASS P3 Word.
setP4(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS P4 Word.
setPa(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the orbit argument of pericenter.
setPa(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter fir the Argument of Perigee (rad).
setParameterDerivatives(ParameterDriver, double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Set the partial derivatives of the simulated measurement with respect to parameter.
setParameters(double[]) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Set the selected parameters.
setParametersConvergenceThreshold(double) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set convergence threshold.
setParticipants(Map<Integer, String>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the participants.
setPatchPointComponentFreedom(int, int, boolean) - Method in class org.orekit.utils.AbstractMultipleShooting
Set a component of a patch point to free or not.
setPath(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the path.
setPath1(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the path1.
setPath2(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the path2.
setPosition(Vector3D) - Method in class org.orekit.files.sinex.Station
Set the station position.
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set position angle type.
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set position angle type.
setPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper
Set position angle type.
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set position angle type.
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set position angle type.
setPredictionProvider(String) - Method in class org.orekit.files.ilrs.CRDHeader
Set the prediction provider.
setPredictionType(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the prediction type.
setPressSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the pressure sensor manufacturer.
setPressSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the pressure sensor model.
setPressSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the pressure sensor serial number.
setPressure(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Set the local pressure at the evaluation location
setPrevId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set identification of previous orbit determination.
setPreviousMessageEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the creation date of previous message from a given originator.
setPreviousMessageID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the unique ID identifying previous message from a given originator.
setPrf(double) - Method in class org.orekit.files.ilrs.CPFHeader
Set the Pulse Repetition Frequency (PRF).
setPrimaryWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the primary wavelength.
setPrmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the Unique identifier of Pointing Request Message linked to this Orbit Data Message.
setPRN(int) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the PRN number of the satellite.
setPRN(int) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the PRN number of the satellite.
setProcessingSoftwares(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Set the processing softwares.
setProcessingSoftwareVersions(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Set the processing software versions.
setProductionEpoch(DateComponents) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the date component of the ephemeris production.
setProductionHour(int) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the hour of ephemeris production.
setProgramName(String) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the program name.
setProgramName(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
Setter for the program name.
setPropagator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set the orbit propagator used to generate this trajectory.
setProxy(Proxy.Type, String, int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Set proxy parameters.
setPulseEnergy(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the pulse energy.
setPulseInOutgoingSemiTrain(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the number of pulses in outgoing semi-train.
setPulseWidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
Set the pulse width.
setQ(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Set quaternion component.
setQDot(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Set quaternion derivative component.
setQualityIndicator(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the data quality indicator.
setQuantumEfficiency(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the quantum efficiency at applicable wavelength.
setQzssCodeOnL2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Set the QZSS code on L2.
setQzssFitInterval(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Set the QZSS fit interval.
setQzssNavigationMessage(QZSSNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Set the QZSS navigation message.
setQzssToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
Set the QZSS time of clock.
setRaan(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Set the orbit right ascension of ascending node.
setRangeMode(RangeMode) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the rangeMode.
setRangeType(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the range type indicator.
setRangeUnits(RangeUnits) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the rangeUnits.
setRateFrameIsA(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set the frame in which rates are specified.
setRateFrameIsA(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Set the frame in which rates are specified.
setRawCoefficients(boolean, double[][], double[][], String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
setRawCoefficients(boolean, Flattener, double[], double[], String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the tesseral-sectorial coefficients matrix.
setRawCorrectionRange(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the raw correction for range.
setRawRangeModulus(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the raw range modulus.
setRcs(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the typical (50th percentile) radar cross-section.
setRdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the Unique identifier of Reentry Data Message linked to this Orbit Data Message.
setReadComplete(boolean) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the indicator for completed read.
setReceiveBand(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the receiveBand.
setReceiveDelays(Map<Integer, Double>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the receiveDelays.
setRecommendedOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the recommended OD time span calculated for the object.
setRecommendedOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set time span of observation recommended for the OD of the object.
setReconnectParameters(double, double, int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Set Reconnect parameters.
setReductionTheory(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set reduction theory used for precession and nutation modeling.
setReferenceDate(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver
Set reference date.
setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Set the reference frame in which data are given.
setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Set the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).
setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Set Coordinate system for velocity increment vector.
setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Set the reference frame in which data are given: used for RADEC tracking data.
setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester
Set up reference state.
setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Set up reference state.
setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Set up reference state.
setReferenceState(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester
Set up reference state.
setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Set up reference state.
setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
Set up reference state.
setReferenceTrajectories(Propagator[]) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Setter for the reference trajectories.
setReferenceValue(double) - Method in class org.orekit.utils.ParameterDriver
Set reference parameter value.
setRefFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the name of the reference frame in which the state vector data are given.
setRefFrame(Frame) - Method in class org.orekit.files.ilrs.CPFHeader
Set the reference frame.
setRefFrameId(int) - Method in class org.orekit.files.ilrs.CPFHeader
Set the reference frame identifier.
setRefFrameString(String) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Set Coordinate system for the torque vector, for absolute frames.
setReflectance(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the typical (50th percentile) coefficient of reflectance.
setRelativeMetadata(CdmRelativeMetadata) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set the relative metadata following header, they are the common metadata for the CDM.
setRelativePositionN(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the N component of Object2’s position relative to Object1’s in RTN frame.
setRelativePositionR(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the R component of Object2’s position relative to Object1’s in RTN frame.
setRelativePositionT(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the T component of Object2’s position relative to Object1’s in RTN frame.
setRelativeSpeed(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the norm of relative velocity vector at TCA.
setRelativeVelocityN(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the N component of Object2’s velocity relative to Object1’s in RTN frame.
setRelativeVelocityR(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the R component of Object2’s velocity relative to Object1’s in RTN frame.
setRelativeVelocityT(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the T component of Object2’s velocity relative to Object1’s in RTN frame.
setRemainingDv(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the total ΔV remaining for spacecraft.
setResetAtEnd(boolean) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Allow/disallow resetting the initial state at end of propagation.
setResetAtEnd(boolean) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Allow/disallow resetting the initial state at end of propagation.
setResidualsAccepted(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the percentage of residuals accepted in the OD of the object (from 0 to 100).
setRevAtEpoch(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Set the revolution rumber.
setRolloverReference(DateComponents) - Static method in class org.orekit.time.GNSSDate
Set a reference date for ensuring continuity across GNSS week rollover.
setRotationalAngleType(int) - Method in class org.orekit.files.ilrs.CPFHeader
Set the rotation angle type.
setRotationAngle(char, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Set the Euler angle about (rad).
setRotationRate(char, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Set the rate of Euler angle (rad/s).
setSatConfiguration(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Sets the satellite configuration.
setSatelliteID(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
Set the satellite ID.
setSatelliteID(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData
Set the satellite ID.
setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Override the default value of the parameter.
setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Override the default value of the parameter.
setSatelliteSystem(SatelliteSystem) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the satellite system.
setSatelliteSystem(SatelliteSystem) - Method in class org.orekit.gnss.navigation.RinexNavigation
Setter for the satellite system.
setScale(double) - Method in class org.orekit.utils.ParameterDriver
Set scale.
setSclkOffsetAtEpoch(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the spacecraft clock count at OcmMetadata.getEpochT0().
setSclkSecPerSISec(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the number of spacecraft clock seconds occurring during one SI second.
setScreenEntryTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the time in UTC when Object2 enters the screening volume.
setScreenExitTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the time in UTC when Object2 exits the screening volume.
setScreenVolumeFrame(ScreenVolumeFrame) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the name of the Object1 centered reference frame in which the screening volume data are given.
setScreenVolumeShape(ScreenVolumeShape) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the shape of the screening volume.
setScreenVolumeX(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the R or T (depending on if RTN or TVN is selected) component size of the screening volume in the corresponding frame.
setScreenVolumeY(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the T or V (depending on if RTN or TVN is selected) component size of the screening volume in the corresponding frame.
setScreenVolumeZ(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the N component size of the screening volume in the corresponding frame.
setSecondsOfWeek(double) - Method in class org.orekit.files.sp3.SP3
Set the seconds of the GPS week for this SP3 file.
setSecularVariationCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField
Set the given secular variation coefficients.
setSedr(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the amount of energy being removed from the object’s orbit by atmospheric drag.
setSelected(boolean) - Method in class org.orekit.utils.ParameterDriver
Configure a parameter selection status.
setSelectedCoefficients(Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the selected short periodic coefficients that must be stored as additional states.
setSelectedCoefficients(Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the selected short periodic coefficients that must be stored as additional states.
setSensors(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set description of sensors used.
setSensorsN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set number of sensors used.
setSequenceNumber(int) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the ephemeris sequence number.
setShadowBodies(List<BodyFacade>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set celestial bodies casting shadows.
setShadowModel(ShadowModel) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set shadow model used for solar radiation pressure.
setShortPeriodJacobians(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
Deprecated.
setShortPeriodTerms(List<ShortPeriodTerms>) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Override the default value short periodic terms.
setSic(String) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the SIC ID.
setSigma(double[]) - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
Set the current value of sigma.
setSisa(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Setter for the signal in space accuracy.
setSiteCode(String) - Method in class org.orekit.files.sinex.Station
Set the site code (station identifier).
setSma(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the semi-major axis.
setSnm(double[][]) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Set the sine parameters of spherical harmonics expansion of degree N and order M.
setSoftwareId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Set the software configuration ID.
setSoftwareRecord(CRDConfiguration.SoftwareConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Set the software configuration record.
setSolarRadArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Set the solar radiation pressure area.
setSolarRadCoeff(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Get the solar radiation pressure coefficient.
setSolarRadiationPressure(boolean) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Set boolean that indicates if Solar Radiation Pressure is taken into account or not.
setSolidTidesModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set solid tides model.
setSolveN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set number of solved-for states.
setSolveStates(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set description of state elements solved-for.
setSource(String) - Method in class org.orekit.files.ilrs.CPFHeader
Set the ephemeris source.
setSource(String) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Sets the source of this GPS almanac.
setSource(String) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
Sets the source of this GPS almanac.
setSpacecraftClockAndDriftApplied(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the spacecraft clock offset and drift applied indicator.
setSpacecraftEpochTimeScale(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the spacecraft epoch time scale.
setSpaceWeatherEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set epoch of the Space Weather data.
setSpaceWeatherSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set Space Weather data source.
setSpatialFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the spatial filter.
setSpectralFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the spectral filter.
setSphericalHarmonicsDegree(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Set the degree of spherical harmonic expansion.
setSphericalHarmonicsOrder(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Set the order of spherical harmonic expansion.
setSpinAlpha(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the right ascension of spin axis vector (rad).
setSpinAngle(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the phase of the satellite about the spin axis (rad).
setSpinAngleVel(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the angular velocity of satellite around spin axis (rad/s).
setSpinDelta(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Set the declination of the spin axis vector (rad).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Setter for the Square Root of Semi-Major Axis (m^1/2).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
Sets the Square Root of Semi-Major Axis (m^1/2).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Setter for the Square Root of Semi-Major Axis (m^1/2).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSAlmanac
Setter for the Square Root of Semi-Major Axis (m^1/2).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
Setter for the Square Root of Semi-Major Axis (m^1/2).
setSrpCoefficient(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the nominal SRP coefficient.
setSrpConstantArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the attitude-independent SRP area, not already into attitude-dependent area along OEB.
setSrpModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
Set Solar Radiation Pressure model.
setSrpUncertainty(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the SRP coefficient 1σ uncertainty.
setSsrEpoch1s(double) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Set the SSR Epoch Time 1s.
setSsrMultipleMessageIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Set the SSR Multiple Message Indicator.
setSsrProviderId(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Set the SSR Provider ID.
setSsrSolutionId(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Set the SSR Solution ID.
setSsrUpdateInterval(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
Set the SSR Update Interval.
setSsrUra(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data
Set the SSR User Range Accuracy (URA).
setStartDate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator
Set a start date.
setStartDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Set a start date.
setStartEpoch(AbsoluteDate) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the staring epoch (UTC).
setStartScreenPeriod(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the start time in UTC of the screening period for the conjunction assessment.
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set start of total time span covered by attitude data.
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the time of the earliest data contained in the OCM.
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Set start of total time span covered by ephemerides data and covariance data.
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the startTime.
setStateDerivatives(int, double[]...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Set the partial derivatives of the simulated measurement with respect to state Cartesian coordinates.
setStationClockAndDriftApplied(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the station clock offset and drift applied indicator.
setStationIdentifier(String) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the station identifier.
setStationName(String) - Method in class org.orekit.files.ilrs.CRDHeader
Set the station name from official list.
setStationName(String) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the station name.
setStationNetword(String) - Method in class org.orekit.files.ilrs.CRDHeader
Set the station network.
setStationOscDrift(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the estimated station oscillator drift in parts in 10¹⁵.
setStationUTCOffset(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the estimated station UTC offset.
setStatus(EstimatedMeasurement.Status) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Set the status.
setStep(int) - Method in class org.orekit.files.ilrs.CPFHeader
Set the time between table entries.
setStepHandler(T, FieldOrekitFixedStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator
Set a single handler for fixed stepsizes.
setStepHandler(FieldOrekitStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator
Set a single handler for variable stepsizes.
setStepHandler(double, OrekitFixedStepHandler) - Method in interface org.orekit.propagation.Propagator
Set a single handler for fixed stepsizes.
setStepHandler(OrekitStepHandler) - Method in interface org.orekit.propagation.Propagator
Set a single handler for variable stepsizes.
setStopScreenPeriod(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the stop time in UTC of the screening period for the conjunction assessment.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set end of total time span covered by attitude data.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the time of the latest data contained in the OCM.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Set end of total time span covered by ephemerides data and covariance data.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the stopTime.
setSubDailySequenceNumber(int) - Method in class org.orekit.files.ilrs.CPFHeader
Set the sub-daily ephemeris sequence number.
setSupportedNames(String) - Method in class org.orekit.data.AbstractSelfFeedingLoader
Set the supported names regular expression.
setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
Setter for the user SV accuracy.
setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
Setter for the user SV accuracy.
setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
Setter for the user SV accuracy.
setSvHealth(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
Set the satellite health status.
setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
Setter for the SV health status.
setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
Setter for the satellite health status.
setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Setter for the satellite health status.
setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
Setter for the satellite health status.
setSVN(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Sets the "SVN" reference number.
setSystemId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
Set the system configuration ID.
setSystemIdentifier(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the system identifier.
setSystemNumber(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the system number.
setSystemOccupancy(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the system occupancy.
setSystemRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Set the system configuration record.
setTaimutcT0(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the difference (TAI – UTC) in seconds at epoch OcmMetadata.getEpochT0().
setTargetClass(int) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the target class.
setTargetLocation(int) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the target location.
setTauC(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the GLONASS time scale correction to UTC time.
setTauGps(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the correction to GPS time relative to GLONASS time.
setTauN(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Setter for the SV clock bias.
setTca(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the date and time in UTC of the closest approach.
setTdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the Unique identifier of Tracking Data Message linked to this Orbit Data Message.
setTechAddress(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the address of Technical Point Of Contact at originator.
setTechEmail(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the email address of Technical Point Of Contact at originator.
setTechOrg(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the creating agency or operator.
setTechPhone(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the phone number of Technical Point Of Contact at originator.
setTechPOC(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the Technical Point Of Contact at originator.
setTechPosition(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the position of Technical Point Of Contact at originator.
setTemperature(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Set the local temperature at the evaluation location
setTempSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the temperature sensor manufacturer.
setTempSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the temperature sensor model.
setTempSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
Set the temperature sensor serial number.
setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
Setter for the Group Delay Differential (s).
setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Setter for the Group Delay Differential (s).
setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
Setter for the Group Delay Differential (s).
setTGD1(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
Setter for the B1/B3 Group Delay Differential (s).
setTGD2(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
Setter for the B2/B3 Group Delay Differential (s).
setThrust(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set thrust component.
setThrustAcceleration(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Set the object’s acceleration due to in-track thrust used to propagate the state vector and covariance to TCA.
setThrustDirectionSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set one σ angular off-nominal thrust direction.
setThrustEfficiency(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set thrust efficiency η.
setThrustInterpolation(OnOff) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set interpolation mode between current and next thrust line.
setThrustIsp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set thrust specific impulse.
setThrustMagnitudeSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
Set one σ percent error on thrust magnitude.
setTideSystem(TideSystem) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the TideSystem used in the gravity field.
setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the reference time of the orbit as a duration from week start.
setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
Setter for the message frame time.
setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Setter for the reference time of the SBAS orbit in GPS seconds of the week.
setTimeLastObsEnd(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the start of a time interval (UTC) that contains the time of the last accepted observation.
setTimeLastObsStart(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the start of a time interval (UTC) that contains the time of the last accepted observation.
setTimeout(int) - Method in class org.orekit.data.NetworkCrawler
Set the timeout for connection.
setTimeout(int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Set timeout for connections and reads.
setTimer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Set the timer name.
setTimerSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Set the timer serial number.
setTimeScale(TimeScale) - Method in class org.orekit.files.ilrs.CPF
Set the time scale.
setTimeScale(TimeScale) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the data time scale.
setTimeSinceFirstObservation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set time elapsed between first accepted observation on epoch.
setTimeSinceLastObservation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set time elapsed between last accepted observation on epoch.
setTimeSource(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
Set the time source.
setTimeSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the span of time in seconds that the OCM covers.
setTimeSystem(TimeSystem) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set the Time System that: for CDM, is used for relative metadata, metadata, OD parameters, state vector.
setTimeSystem(TimeSystem) - Method in class org.orekit.files.ccsds.section.Metadata
Set the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.
setTimeSystem(TimeSystem) - Method in class org.orekit.files.sp3.SP3
Set the time system used in this SP3 file.
setTimeSystem(TimeSystem) - Method in class org.orekit.gnss.clock.RinexClock
Setter for the file time system.
setTimetagRef(TimetagReference) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the timetagRef.
setTimingRecord(CRDConfiguration.TimingSystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Set the timing system configuration record.
setTk(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Set the time referenced to the beginning of the frame within the current day.
setTorque(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Set the torque vector (N.m).
setTrackId(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the tracking data identifier.
setTrackingSoftwares(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Set the tracking softwares.
setTrackingSoftwareVersions(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
Set the tracking software versions.
setTracksAvailable(int) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the number of sensor tracks available for the OD of the object.
setTracksAvailable(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set number of sensors tracks available for the OD within the actual OD span.
setTracksUsed(int) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the number of sensor tracks used for the OD of the object.
setTracksUsed(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set number of sensors tracks accepted for the OD within the actual OD span.
setTrajBasis(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set basis of this trajectory state time history data.
setTrajBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set identification number of the orbit determination or simulation upon which this trajectory is based.
setTrajFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set epoch of the trajectory reference frame.
setTrajID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set trajectory identification number.
setTrajNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set identification number of next trajectory.
setTrajPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set identification number of previous trajectory.
setTrajReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set reference frame of the trajectory.
setTrajType(ElementsType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set trajectory element set type.
setTrajUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set trajectory element set units.
setTransmissionOfSpectralFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
Set the percentage of transmission of spectral filter.
setTransmitBand(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the transmitBand.
setTransmitDelays(Map<Integer, Double>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the transmitDelays.
setTranspClkRef(double) - Method in class org.orekit.files.ilrs.CPFHeader
Set the transponder Clock Reference Time.
setTranspClkRefTime(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the transponder clock reference time.
setTransponderId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the transponder configuration ID.
setTransponderRecord(CRDConfiguration.TransponderConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Set the transponder configuration record.
setTranspOscDrift(double) - Method in class org.orekit.files.ilrs.CPFHeader
Set the transponder Oscillator Drift in parts.
setTranspOscDrift(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the estimated transponder oscillator drift in parts in 10¹⁵.
setTranspTransmitDelay(double) - Method in class org.orekit.files.ilrs.CPFHeader
Set the transponder transmit delay.
setTranspUtcOffset(double) - Method in class org.orekit.files.ilrs.CPFHeader
Set the transponder UTC offset.
setTranspUTCOffset(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
Set the estimated transponder UTC offset.
setTurnaroundDenominator(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the turnaroundDenominator.
setTurnaroundNumerator(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Setter for the turnaroundNumerator.
setTypAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.
setType(SP3.SP3FileType) - Method in class org.orekit.files.sp3.SP3
Set the file type for this SP3 file.
setUpEventDetector(ODEIntegrator, EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Wrap an Orekit event detector and register it to the integrator.
setUpEventDetector(FieldODEIntegrator<T>, FieldEventDetector<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Wrap an Orekit event detector and register it to the integrator.
setupMatricesComputation(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.AbstractPropagator
Set up computation of State Transition Matrix and Jacobians matrix with respect to parameters.
setupMatricesComputation(String, RealMatrix, DoubleArrayDictionary) - Method in interface org.orekit.propagation.Propagator
Set up computation of State Transition Matrix and Jacobians matrix with respect to parameters.
setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set up State Transition Matrix and Jacobian matrix handling.
setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set up State Transition Matrix and Jacobian matrix handling.
setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set up State Transition Matrix and Jacobian matrix handling.
setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set up all user defined event detectors.
setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set up all user defined event detectors.
setURA(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
Sets the average URA number.
setURA(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
Setter for the user range accuracy.
setURA(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
Setter for the user range accuracy.
setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set start of useable time span covered by attitude data.
setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Set start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Set end of useable time span covered by ephemerides data.
setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Set end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Set end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
setUt1MinusUtc(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the UT1-UTC offset.
setUt1mutcT0(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Set the difference (UT1 – UTC) in seconds at epoch OcmMetadata.getEpochT0().
setV(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
Set velocity component.
setValidFrom(AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Set the start of validity.
setValidUntil(AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Set the end of validity.
setValue(double) - Method in class org.orekit.utils.ParameterDriver
Set parameter value.
setVelocity(Vector3D) - Method in class org.orekit.files.sinex.Station
Set the station velocity.
setVersion(int) - Method in class org.orekit.files.ilrs.ILRSHeader
Set the format version.
setVmAbsolute(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the typical (50th percentile) visual magnitude.
setVmApparent(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the typical (50th percentile) apparent visual magnitude.
setVmApparentMax(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the maximum apparent visual magnitude.
setVmApparentMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the minimum apparent visual magnitude.
setVtecQualityIndicator(double) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
Set the VTEC quality indicator.
setWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
Set the transmit wavelength.
setWeek(int) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Setter for the reference week of the orbit.
setWeightedRMS(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Set the weighted Root Mean Square (RMS) of the residuals from a batch least squares OD.
setWeightedRms(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Set weighted RMS residual ratio.
setWetMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
Set the total mass at T₀.
setX(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Set object Position Vector X component.
setX(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite X position.
setXdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Set object Velocity Vector X component.
setXDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite X velocity.
setXDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite X acceleration.
setxPo(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the X polar motion.
setY(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Set object Position Vector Y component.
setY(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite Y position.
setYawAngle(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Set the yaw angle used for computation of phase wind-up correction.
setYawRate(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Set the yaw rate.
setYdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Set object Velocity Vector Y component.
setYDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite Y velocity.
setYDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite Y acceleration.
setYearOfCentury(int) - Method in class org.orekit.files.ilrs.CRDHeader
Set the year of century from CPF or TLE.
setyPo(double) - Method in class org.orekit.files.sinex.SinexEopEntry
Set the Y polar motion.
setZ(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Set object Position Vector Z component.
setZ(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite Z position.
setZdot(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Set object Velocity Vector Z component.
setZDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite Z velocity.
setZDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Setter for the satellite Z acceleration.
SGP - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Identifier for SGP type of ephemeris.
SGP - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SGP type of ephemeris.
SGP4 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Identifier for SGP4 type of ephemeris.
SGP4 - Class in org.orekit.propagation.analytical.tle
This class contains methods to compute propagated coordinates with the SGP4 model.
SGP4(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.SGP4
Constructor for a unique initial TLE.
SGP4(TLE, AttitudeProvider, double, Frame) - Constructor for class org.orekit.propagation.analytical.tle.SGP4
Constructor for a unique initial TLE.
SGP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SGP4 type of ephemeris.
SGP8 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Identifier for SGP8 type of ephemeris.
SGP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SGP8 type of ephemeris.
SGP_SGP4_THEORY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
Constant for SGP/SGP4 mean elements theory.
ShadowModel - Enum in org.orekit.files.ccsds.ndm.odm.ocm
Shadow model for solar radiation pressure.
shapiroCorrection(TimeStampedPVCoordinates, TimeStampedPVCoordinates) - Method in class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier
Compute Shapiro path dilation between two points in a gravity field.
ShapiroInterSatellitePhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical inter-satellites phase measurement with Shapiro time delay.
ShapiroInterSatellitePhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier
Simple constructor.
ShapiroInterSatelliteRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with Shapiro time delay.
ShapiroInterSatelliteRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier
Simple constructor.
ShapiroOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical one-way GNSS phase measurement with Shapiro time delay.
ShapiroOneWayGNSSPhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier
Simple constructor.
ShapiroOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with Shapiro time delay.
ShapiroOneWayGNSSRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier
Simple constructor.
ShapiroPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurement with Shapiro time delay.
ShapiroPhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier
Simple constructor.
ShapiroRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with Shapiro time delay.
ShapiroRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier
Simple constructor.
shiftedBy(double) - Method in class org.orekit.attitudes.Attitude
Get a time-shifted attitude.
shiftedBy(double) - Method in class org.orekit.attitudes.FieldAttitude
Get a time-shifted attitude.
shiftedBy(T) - Method in class org.orekit.attitudes.FieldAttitude
Get a time-shifted attitude.
shiftedBy(double) - Method in class org.orekit.frames.FieldTransform
Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.frames.FieldTransform
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.frames.Transform
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.orbits.CartesianOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.CircularOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.EquinoctialOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.FieldCartesianOrbit
Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.orbits.FieldCartesianOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.FieldCircularOrbit
Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.orbits.FieldCircularOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get a time-shifted orbit.
shiftedBy(T) - Method in class org.orekit.orbits.FieldOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.KeplerianOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.Orbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.propagation.FieldSpacecraftState
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.propagation.FieldSpacecraftState
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.propagation.SpacecraftState
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.time.AbsoluteDate
Get a time-shifted date.
shiftedBy(T) - Method in class org.orekit.time.FieldAbsoluteDate
Get a time-shifted date.
shiftedBy(double) - Method in class org.orekit.time.FieldAbsoluteDate
Get a time-shifted date.
shiftedBy(double) - Method in interface org.orekit.time.FieldTimeShiftable
Get a time-shifted instance.
shiftedBy(KK) - Method in interface org.orekit.time.FieldTimeShiftable
Get a time-shifted instance.
shiftedBy(double) - Method in interface org.orekit.time.TimeShiftable
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.utils.AbsolutePVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.AngularCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldAngularCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.FieldAngularCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldPVCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.FieldPVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.PVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedPVCoordinates
Get a time-shifted state.
ShiftingTransformProvider - Class in org.orekit.frames
Transform provider using thread-safe shifts on transforms sample.
ShiftingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double) - Constructor for class org.orekit.frames.ShiftingTransformProvider
Simple constructor.
SHM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for SHM files.
SHMFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the SHM gravity field format.
SHMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader
Simple constructor.
SHMFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader
Simple constructor.
SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Name of the prefix for short period coefficients keys.
SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Name of the prefix for short period coefficients keys.
SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Name of the prefix for short period coefficients keys.
ShortPeriodicsInterpolatedCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolated short periodics coefficients.
ShortPeriodicsInterpolatedCoefficient(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Simple constructor.
ShortPeriodTerms - Interface in org.orekit.propagation.semianalytical.dsst.forces
Additive short period terms contributing to the mean to osculating orbit mapping.
sign(double) - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Return the symbol of parameter a.
SignalCode - Enum in org.orekit.gnss
Enumerate for satellite signal code.
SignalInSpaceAccuracy - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris.utils
Signal-In-Space Accuracy (SISA).
SignalInSpaceAccuracy(int) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.SignalInSpaceAccuracy
Simple constructor.
signalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Compute propagation delay on a link leg (typically downlink or uplink).
signalTimeOfFlight(TimeStampedFieldPVCoordinates<T>, FieldVector3D<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Compute propagation delay on a link leg (typically downlink or uplink).
signedAmplitude(SpacecraftState, double[]) - Method in interface org.orekit.forces.empirical.AccelerationModel
Compute the signed amplitude of the acceleration.
signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.empirical.AccelerationModel
Compute the signed amplitude of the acceleration.
signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel
Compute the signed amplitude of the acceleration.
signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel
Compute the signed amplitude of the acceleration.
signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel
Compute the signed amplitude of the acceleration.
signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel
Compute the signed amplitude of the acceleration.
SignSemantic - Enum in org.orekit.estimation.measurements.generation
Enumerate for the semantic of the g function sign during measurements generation.
SimpleExponentialAtmosphere - Class in org.orekit.models.earth.atmosphere
Simple exponential atmospheric model.
SimpleExponentialAtmosphere(BodyShape, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
Create an exponential atmosphere.
SimpleRatioAmbiguityAcceptance - Class in org.orekit.estimation.measurements.gnss
Ambiguity acceptance test based on a ratio of the two best candidates.
SimpleRatioAmbiguityAcceptance(double) - Constructor for class org.orekit.estimation.measurements.gnss.SimpleRatioAmbiguityAcceptance
Simple constructor.
SimpleTimeStampedTableParser<T extends TimeStamped> - Class in org.orekit.data
Parser for simple tables containing time stamped data.
SimpleTimeStampedTableParser(int, SimpleTimeStampedTableParser.RowConverter<T>) - Constructor for class org.orekit.data.SimpleTimeStampedTableParser
Simple constructor.
SimpleTimeStampedTableParser.RowConverter<S extends TimeStamped> - Interface in org.orekit.data
Interface for converting a table row into time-stamped data.
SinexEopEntry - Class in org.orekit.files.sinex
Container for EOP entry read in a Sinex file.
SinexEopEntry(AbsoluteDate) - Constructor for class org.orekit.files.sinex.SinexEopEntry
Constructor.
SinexLoader - Class in org.orekit.files.sinex
Loader for Solution INdependent EXchange (SINEX) files.
SinexLoader(String) - Constructor for class org.orekit.files.sinex.SinexLoader
Simple constructor.
SinexLoader(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.files.sinex.SinexLoader
Construct a loader by specifying the source of SINEX auxiliary data files.
SinexLoader(DataSource) - Constructor for class org.orekit.files.sinex.SinexLoader
Simple constructor.
SinexLoader(DataSource, TimeScale) - Constructor for class org.orekit.files.sinex.SinexLoader
Loads SINEX from the given input stream using the specified auxiliary data.
SingleBodyAbsoluteAttraction - Class in org.orekit.forces.gravity
Body attraction force model computed as absolute acceleration towards a body.
SingleBodyAbsoluteAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Simple constructor.
SingleBodyRelativeAttraction - Class in org.orekit.forces.gravity
Body attraction force model computed as relative acceleration towards frame center.
SingleBodyRelativeAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Simple constructor.
SingleFrequencyHatchFilter - Class in org.orekit.estimation.measurements.filtering
Single frequency Hatch filter.
SingleFrequencyHatchFilter(ObservationData, ObservationData, MeasurementType, double, double, int, double) - Constructor for class org.orekit.estimation.measurements.filtering.SingleFrequencyHatchFilter
Constructor for the Single Frequency Hatch Filter.
SingleFrequencySmoother - Class in org.orekit.estimation.measurements.filtering
Handler to perform pseudo-range smoothing using single frequency measurements.
SingleFrequencySmoother(MeasurementType, double, int, double) - Constructor for class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother
Simple constructor.
SingleLayerModelMappingFunction - Class in org.orekit.models.earth.ionosphere
Single Layer Model (SLM) ionospheric mapping function.
SingleLayerModelMappingFunction() - Constructor for class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction
Constructor with default value.
SingleLayerModelMappingFunction(double) - Constructor for class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction
Constructor.
sini0 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
sinus original inclination.
sini0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
sinus original inclination.
siToCcsdsName(String) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Convert a SI unit name to a CCSDS name.
siToCcsdsName(String) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Convert a SI unit name to a CCSDS name.
siToRaw(RangeUnitsConverter, TdmMetadata, AbsoluteDate, double) - Method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType
Convert a measurement from SI units.
size() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
Get the size of the value array.
size() - Method in class org.orekit.utils.DoubleArrayDictionary
Get the number of dictionary entries.
size() - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Get the size of the value array.
size() - Method in class org.orekit.utils.FieldArrayDictionary
Get the number of dictionary entries.
SM_COEFFICIENTS - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Identifier for sMm coefficients.
SmallManeuverAnalyticalModel - Class in org.orekit.forces.maneuvers
Analytical model for small maneuvers.
SmallManeuverAnalyticalModel(SpacecraftState, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Build a maneuver defined in spacecraft frame.
SmallManeuverAnalyticalModel(SpacecraftState, Frame, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Build a maneuver defined in user-specified frame.
SmoothedObservationDataSet - Class in org.orekit.estimation.measurements.filtering
Container used to store smoothed observation data along with the original data set it originates from.
SmoothedObservationDataSet(ObservationData, ObservationDataSet) - Constructor for class org.orekit.estimation.measurements.filtering.SmoothedObservationDataSet
Simple constructor.
SmoothFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with shape defined by a smooth single loop.
SmoothFieldOfView(Vector3D, Vector3D, double) - Constructor for class org.orekit.geometry.fov.SmoothFieldOfView
Build a new instance.
SoftwareConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
 
SOLAR_FLUX_UNIT - Static variable in class org.orekit.utils.units.Unit
Solar Flux Unit.
SOLAR_SYSTEM_BARYCENTER - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for solar system barycenter.
SolarRadiationPressure - Class in org.orekit.forces.radiation
Solar radiation pressure force model.
SolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure
Simple constructor with default reference values.
SolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure
Complete constructor.
SOLFSMYDataLoader - Class in org.orekit.models.earth.atmosphere.data
This class reads solar activity data from SOLFSMY files for the class JB2008SpaceEnvironmentData.
SOLFSMYDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader
Constructor.
SOLFSMYDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data
Container class for Solar activity indexes.
SolidTides - Class in org.orekit.forces.gravity
Solid tides force model.
SolidTides(Frame, double, double, TideSystem, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides
Simple constructor.
SolidTides(Frame, double, double, TideSystem, boolean, double, int, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides
Simple constructor.
solveILS(int, double[], int[], RealMatrix) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Find the best solutions to an Integer Least Square problem.
solveILS(int, double[], int[], RealMatrix) - Method in interface org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolver
Find the best solutions to an Integer Least Square problem.
sort() - Method in class org.orekit.utils.ParameterDriversList
Sort the parameters lexicographically.
SourceTable - Class in org.orekit.gnss.metric.ntrip
Source table for ntrip streams retrieval.
SOUTH_POLE - Static variable in class org.orekit.bodies.GeodeticPoint
South pole.
SP3 - Class in org.orekit.files.sp3
Represents a parsed SP3 orbit file.
SP3(double, int, Function<? super String, ? extends Frame>) - Constructor for class org.orekit.files.sp3.SP3
Create a new SP3 file object.
SP3.SP3Coordinate - Class in org.orekit.files.sp3
A single record of position clock and possibly derivatives in an SP3 file.
SP3.SP3Ephemeris - Class in org.orekit.files.sp3
An ephemeris for a single satellite in a SP3 file.
SP3.SP3FileType - Enum in org.orekit.files.sp3
File type indicator.
SP3.SP3OrbitType - Enum in org.orekit.files.sp3
Orbit type indicator.
SP3_FRAME_CENTER_STRING - Static variable in class org.orekit.files.sp3.SP3
String representation of the center of ephemeris coordinate system.
SP3Coordinate(AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.files.sp3.SP3.SP3Coordinate
Create a coordinate with only position.
SP3Coordinate(AbsoluteDate, Vector3D, Vector3D, double, double) - Constructor for class org.orekit.files.sp3.SP3.SP3Coordinate
Create a coordinate with position and velocity.
SP3Ephemeris(String) - Constructor for class org.orekit.files.sp3.SP3.SP3Ephemeris
Create an ephemeris for a single satellite.
SP3Parser - Class in org.orekit.files.sp3
A parser for the SP3 orbit file format.
SP3Parser() - Constructor for class org.orekit.files.sp3.SP3Parser
Create an SP3 parser using default values.
SP3Parser(double, int, Function<? super String, ? extends Frame>) - Constructor for class org.orekit.files.sp3.SP3Parser
Create an SP3 parser and specify the extra information needed to create a Propagator from the ephemeris data.
SP3Parser(double, int, Function<? super String, ? extends Frame>, TimeScales) - Constructor for class org.orekit.files.sp3.SP3Parser
Create an SP3 parser and specify the extra information needed to create a Propagator from the ephemeris data.
SpacecraftBodyFrame - Class in org.orekit.files.ccsds.definitions
Frames used in CCSDS Attitude Data Messages for the spacecraft body.
SpacecraftBodyFrame(SpacecraftBodyFrame.BaseEquipment, String) - Constructor for class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame
Simple constructor.
SpacecraftBodyFrame.BaseEquipment - Enum in org.orekit.files.ccsds.definitions
Equipment on which the frame is located.
SpacecraftParameters - Class in org.orekit.files.ccsds.ndm.adm.apm
Container for spacecraft parameters data.
SpacecraftParameters() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Simple constructor.
SpacecraftParameters - Class in org.orekit.files.ccsds.ndm.odm
Container for spacecraft parameters.
SpacecraftParameters() - Constructor for class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Create an empty state data set.
SpacecraftParametersKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
Keys for APM spacecraft parameters entries.
SpacecraftParametersKey - Enum in org.orekit.files.ccsds.ndm.odm
Keys for ODM spacecraft parameters entries.
SpacecraftParametersWriter - Class in org.orekit.files.ccsds.ndm.odm
Writer for spacecraft parameters data.
SpacecraftParametersWriter(String, String, SpacecraftParameters) - Constructor for class org.orekit.files.ccsds.ndm.odm.SpacecraftParametersWriter
Create a writer.
SpacecraftState - Class in org.orekit.propagation
This class is the representation of a complete state holding orbit, attitude and mass information at a given date.
SpacecraftState(Orbit) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit only.
SpacecraftState(Orbit, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit and attitude.
SpacecraftState(Orbit, double) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from orbit and mass.
SpacecraftState(Orbit, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude and mass.
SpacecraftState(Orbit, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
SpacecraftState(Orbit, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit and additional states.
SpacecraftState(Orbit, Attitude, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
SpacecraftState(Orbit, Attitude, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude and additional states.
SpacecraftState(Orbit, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
SpacecraftState(Orbit, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from orbit, mass and additional states.
SpacecraftState(Orbit, Attitude, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude, mass and additional states.
SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude, mass, additional states and derivatives.
SpacecraftState(AbsolutePVCoordinates) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from position-velocity-acceleration only.
SpacecraftState(AbsolutePVCoordinates, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from position-velocity-acceleration and attitude.
SpacecraftState(AbsolutePVCoordinates, double) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from position-velocity-acceleration and mass.
SpacecraftState(AbsolutePVCoordinates, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from position-velocity-acceleration, attitude and mass.
SpacecraftState(AbsolutePVCoordinates, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
SpacecraftState(AbsolutePVCoordinates, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from position-velocity-acceleration and additional states.
SpacecraftState(AbsolutePVCoordinates, Attitude, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
SpacecraftState(AbsolutePVCoordinates, Attitude, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from position-velocity-acceleration, attitude and additional states.
SpacecraftState(AbsolutePVCoordinates, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
SpacecraftState(AbsolutePVCoordinates, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from position-velocity-acceleration, mass and additional states.
SpacecraftState(AbsolutePVCoordinates, Attitude, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from position-velocity-acceleration, attitude, mass and additional states.
SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from position-velocity-acceleration, attitude, mass and additional states and derivatives.
SPEED_OF_LIGHT - Static variable in interface org.orekit.utils.Constants
Speed of light: 299792458.0 m/s.
SphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide spherical harmonics coefficients.
SpinStabilized - Class in org.orekit.attitudes
This class handles a spin stabilized attitude provider.
SpinStabilized(AttitudeProvider, AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.attitudes.SpinStabilized
Creates a new instance.
SpinStabilized - Class in org.orekit.files.ccsds.ndm.adm.apm
Container for Attitude Parameter Message data lines.
SpinStabilized() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Simple constructor.
SpinStabilizedKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
Keys for APM spin-stabilized entries.
sqrt(String) - Method in class org.orekit.utils.units.Unit
Create root of unit.
SSA - Static variable in class org.orekit.models.earth.displacement.Tide
Ssa tide.
SsrData - Class in org.orekit.gnss.metric.messages.ssr
Container for common data in SSR message data.
SsrData() - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrData
 
SsrHeader - Class in org.orekit.gnss.metric.messages.ssr
Container for common data in SSR messages header.
SsrHeader() - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrHeader
 
SsrIgm01 - Class in org.orekit.gnss.metric.messages.ssr.igm
GNSS SSR Orbit Correction Message.
SsrIgm01(int, SatelliteSystem, SsrIgm01Header, List<SsrIgm01Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01
Constructor.
SsrIgm01Data - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM01 data.
SsrIgm01Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
Constructor.
SsrIgm01Header - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM01 header.
SsrIgm01Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header
Constructor.
SsrIgm02 - Class in org.orekit.gnss.metric.messages.ssr.igm
GNSS SSR Clock Correction Message.
SsrIgm02(int, SatelliteSystem, SsrIgm02Header, List<SsrIgm02Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02
Constructor.
SsrIgm02Data - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM02 data.
SsrIgm02Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data
Constructor.
SsrIgm02Header - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM02 header.
SsrIgm02Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Header
Constructor.
SsrIgm03 - Class in org.orekit.gnss.metric.messages.ssr.igm
GNSS SSR Combined Orbit and Clock Correction Message.
SsrIgm03(int, SatelliteSystem, SsrIgm03Header, List<SsrIgm03Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03
Constructor.
SsrIgm03Data - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM03 data.
SsrIgm03Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
Constructor.
SsrIgm03Header - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM03 header.
SsrIgm03Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header
Constructor.
SsrIgm04 - Class in org.orekit.gnss.metric.messages.ssr.igm
GNSS SSR High Rate Clock Correction Message.
SsrIgm04(int, SatelliteSystem, SsrIgm04Header, List<SsrIgm04Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04
Constructor.
SsrIgm04Data - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM04 data.
SsrIgm04Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data
Constructor.
SsrIgm04Header - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM04 header.
SsrIgm04Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Header
Constructor.
SsrIgm05 - Class in org.orekit.gnss.metric.messages.ssr.igm
GNSS SSR Code Bias Message.
SsrIgm05(int, SatelliteSystem, SsrIgm05Header, List<SsrIgm05Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05
Constructor.
SsrIgm05Data - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM05 data.
SsrIgm05Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
Constructor.
SsrIgm05Header - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM05 header.
SsrIgm05Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Header
Constructor.
SsrIgm06 - Class in org.orekit.gnss.metric.messages.ssr.igm
GNSS SSR Phase Bias Message.
SsrIgm06(int, SatelliteSystem, SsrIgm06Header, List<SsrIgm06Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06
Constructor.
SsrIgm06Data - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM06 data.
SsrIgm06Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Constructor.
SsrIgm06Header - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM06 header.
SsrIgm06Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header
Constructor.
SsrIgm07 - Class in org.orekit.gnss.metric.messages.ssr.igm
GNSS SSR SSR URA Message.
SsrIgm07(int, SatelliteSystem, SsrIgm07Header, List<SsrIgm07Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07
Constructor.
SsrIgm07Data - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM07 data.
SsrIgm07Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data
Constructor.
SsrIgm07Header - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for SSR IGM07 header.
SsrIgm07Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Header
Constructor.
SsrIgmData - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for common data in IGS Generic SSR Message type.
SsrIgmData() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData
Constructor.
SsrIgmHeader - Class in org.orekit.gnss.metric.messages.ssr.igm
Container for common data in IGS Generic SSR Message type header.
SsrIgmHeader() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader
Constructor.
SsrIgmMessage<H extends SsrIgmHeader,D extends SsrIgmData> - Class in org.orekit.gnss.metric.messages.ssr.igm
The IGS Generic SSR Message types provide elements to calculate GNSS satellite corrections.
SsrIgmMessage(int, SatelliteSystem, H, List<D>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmMessage
Constructor.
SsrIm201 - Class in org.orekit.gnss.metric.messages.ssr.subtype
SSR Ionosphere VTEC Spherical Harmonics Message.
SsrIm201(int, SsrIm201Header, List<SsrIm201Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201
Constructor.
SsrIm201Data - Class in org.orekit.gnss.metric.messages.ssr.subtype
Container for SSR IM201 data.
SsrIm201Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
Constructor.
SsrIm201Header - Class in org.orekit.gnss.metric.messages.ssr.subtype
Container for SSR IM201 header.
SsrIm201Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
Constructor.
SsrMessage<H extends SsrHeader,D extends SsrData> - Class in org.orekit.gnss.metric.messages.ssr
Base class for SSR messages.
SsrMessage(int, H, List<D>) - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrMessage
Constructor.
SsrVtecIonosphericModel - Class in org.orekit.models.earth.ionosphere
Ionospheric model based on SSR IM201 message.
SsrVtecIonosphericModel(SsrIm201) - Constructor for class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel
Constructor.
STANDARD_ATM_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
NIST standard atmospheric pressure (Pa).
STANDARD_ATM_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
NIST standard atmospheric temperature (K).
STANDARDIZED_LOCALE - Static variable in class org.orekit.utils.AccurateFormatter
Standardized locale to use, to ensure files can be exchanged without internationalization issues.
start() - Method in class org.orekit.gnss.metric.parser.AbstractEncodedMessages
Start message extraction.
start() - Method in class org.orekit.gnss.metric.parser.ByteArrayEncodedMessages
Start message extraction.
start() - Method in interface org.orekit.gnss.metric.parser.EncodedMessage
Start message extraction.
START_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Default suffix for start driver.
START_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Default suffix for start driver.
started(TaskEvent) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
 
startMessage(String, String, double) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Start CCSDS message.
startMessage(String, String, double) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
Start CCSDS message.
startMessage(String, String, double) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Start CCSDS message.
startParse(String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Start parsing.
StartStopEventsTrigger<A extends AbstractDetector<A>,O extends AbstractDetector<O>> - Class in org.orekit.forces.maneuvers.trigger
Maneuver triggers based on a pair of event detectors that defines firing start and stop.
StartStopEventsTrigger(A, O) - Constructor for class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Simple constructor.
startStreaming(String, Type, boolean, boolean) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Connect to a mount point and start streaming data from it.
STATE_DIMENSION - Static variable in class org.orekit.propagation.AbstractMatricesHarvester
State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.analytical.tle.TLEJacobiansMapper
State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.integration.AbstractJacobiansMapper
State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.numerical.AbsoluteJacobiansMapper
State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.numerical.JacobiansMapper
State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
State dimension, fixed to 6.
stateChanged(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
Notify about a state change.
stateChanged(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Notify about a state change.
StateFunction - Interface in org.orekit.utils
Interface representing a vector function depending on SpacecraftState.
StateJacobian - Interface in org.orekit.utils
Interface representing the Jacobian of a vector function depending on SpacecraftState.
StateMapper - Class in org.orekit.propagation.integration
This class maps between raw double elements and SpacecraftState instances.
StateMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.StateMapper
Simple constructor.
stateToTLE(FieldSpacecraftState<T>, FieldTLE<T>) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE
Convert Spacecraft State into TLE.
stateToTLE(FieldSpacecraftState<T>, FieldTLE<T>, TimeScale, Frame) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE
Convert Spacecraft State into TLE.
stateToTLE(FieldSpacecraftState<T>, FieldTLE<T>, TimeScale, Frame, double, int) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE
Convert Spacecraft State into TLE.
stateToTLE(SpacecraftState, TLE) - Static method in class org.orekit.propagation.analytical.tle.TLE
Convert Spacecraft State into TLE.
stateToTLE(SpacecraftState, TLE, TimeScale, Frame) - Static method in class org.orekit.propagation.analytical.tle.TLE
Convert Spacecraft State into TLE.
stateToTLE(SpacecraftState, TLE, TimeScale, Frame, double, int) - Static method in class org.orekit.propagation.analytical.tle.TLE
Convert Spacecraft State into TLE.
StateVector - Class in org.orekit.files.ccsds.ndm.cdm
Container for state vector data.
StateVector() - Constructor for class org.orekit.files.ccsds.ndm.cdm.StateVector
Simple constructor.
StateVector - Class in org.orekit.files.ccsds.ndm.odm
Container for state vector data.
StateVector() - Constructor for class org.orekit.files.ccsds.ndm.odm.StateVector
Create an empty data set.
StateVectorKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM state vector entries.
StateVectorKey - Enum in org.orekit.files.ccsds.ndm.odm
Keys for ODM state vector container entries.
StateVectorWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for state vector data for CCSDS Conjunction Data Messages.
StateVectorWriter - Class in org.orekit.files.ccsds.ndm.odm
Writer for state vector data.
StateVectorWriter(String, String, StateVector, TimeConverter) - Constructor for class org.orekit.files.ccsds.ndm.odm.StateVectorWriter
Create a writer.
staticShiftedBy(double) - Method in class org.orekit.frames.Transform
Shift the transform in time considering all rates, then return only the translation and rotation portion of the transform.
StaticTransform - Interface in org.orekit.frames
A transform that only includes translation and rotation.
Station - Class in org.orekit.files.sinex
Station model.
Station() - Constructor for class org.orekit.files.sinex.Station
Constructor.
Station.ReferenceSystem - Enum in org.orekit.files.sinex
Eccentricity reference system.
StationDisplacement - Interface in org.orekit.models.earth.displacement
Interface for computing reference points displacement.
stec(AbsoluteDate, GeodeticPoint, GeodeticPoint) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
This method allows the computation of the Stant Total Electron Content (STEC).
stec(FieldAbsoluteDate<T>, FieldGeodeticPoint<T>, FieldGeodeticPoint<T>) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
This method allows the computation of the Stant Total Electron Content (STEC).
StepHandlerMultiplexer - Class in org.orekit.propagation.sampling
This class gathers several OrekitStepHandler instances into one.
StepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.StepHandlerMultiplexer
Simple constructor.
stillAcceptsData() - Method in interface org.orekit.data.DataLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.gnss.RinexObservationLoader.Parser
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.gnss.SEMParser
 
stillAcceptsData() - Method in class org.orekit.gnss.YUMAParser
 
stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.GeoMagneticModelLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
 
stillAcceptsData() - Method in class org.orekit.utils.InterpolationTableLoader
Check if the loader still accepts new data.
STMEquations - Class in org.orekit.propagation.numerical.cr3bp
Class calculating the state transition matrix coefficient for CR3BP Computation.
STMEquations(CR3BPSystem) - Constructor for class org.orekit.propagation.numerical.cr3bp.STMEquations
Simple constructor.
STOP_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
Default suffix for stop driver.
STOP_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
Default suffix for stop driver.
stopMonitoring() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor
Stop monitoring.
StopOnDecreasing<T extends EventDetector> - Class in org.orekit.propagation.events.handlers
Handle a detection event and choose what to do next.
StopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnDecreasing
 
StopOnEvent<T extends EventDetector> - Class in org.orekit.propagation.events.handlers
Event handler which will always return stop as a state.
StopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.StopOnEvent
 
StopOnIncreasing<T extends EventDetector> - Class in org.orekit.propagation.events.handlers
Handle a detection event and choose what to do next.
StopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnIncreasing
 
stopStreaming(int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Stop streaming data from all connected mount points.
StreamedMessage - Class in org.orekit.gnss.metric.ntrip
Container for streamed messages meta-data.
StreamingAemWriter - Class in org.orekit.files.ccsds.ndm.adm.aem
A writer for AEM files.
StreamingAemWriter(Generator, AemWriter, Header, AemMetadata) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter
Simple constructor.
StreamingAemWriter.SegmentWriter - Class in org.orekit.files.ccsds.ndm.adm.aem
A writer for a segment of an AEM.
StreamingCpfWriter - Class in org.orekit.files.ilrs
A writer for CPF files.
StreamingCpfWriter(Appendable, TimeScale, CPFHeader) - Constructor for class org.orekit.files.ilrs.StreamingCpfWriter
Create a CPF writer than streams data to the given output stream.
StreamingCpfWriter(Appendable, TimeScale, CPFHeader, boolean) - Constructor for class org.orekit.files.ilrs.StreamingCpfWriter
Create a CPF writer than streams data to the given output stream.
StreamingCpfWriter.HeaderLineWriter - Enum in org.orekit.files.ilrs
Writer for specific header lines.
StreamingCpfWriter.Segment - Class in org.orekit.files.ilrs
A writer for a segment of a CPF.
StreamingOemWriter - Class in org.orekit.files.ccsds.ndm.odm.oem
A writer for OEM files.
StreamingOemWriter(Generator, OemWriter, Header, OemMetadata) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter
Construct a writer that for each segment uses the reference frame of the first state's attitude.
StreamingOemWriter(Generator, OemWriter, Header, OemMetadata, boolean) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter
Construct a writer that writes position, velocity, and acceleration at each time step.
StreamingOemWriter(Generator, OemWriter, Header, OemMetadata, boolean, boolean) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter
Simple constructor.
StreamingOemWriter.SegmentWriter - Class in org.orekit.files.ccsds.ndm.odm.oem
A writer for a segment of an OEM.
StreamMonitor - Class in org.orekit.gnss.metric.ntrip
Monitor for retrieving streamed data from one mount point.
StreamMonitor(NtripClient, String, Type, boolean, boolean, double, double, int) - Constructor for class org.orekit.gnss.metric.ntrip.StreamMonitor
Build a monitor for streaming data from a mount point.
stringValue(EncodedMessage, int) - Method in interface org.orekit.gnss.metric.parser.DataField
Get the value of the field as a String.
subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Subtract an offset from the instance.
subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Subtract an offset from the instance.
subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Subtract an offset from the instance.
subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Subtract an offset from the instance.
SUN - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Sun.
SUN_RADIUS - Static variable in interface org.orekit.utils.Constants
Sun radius: 695500000 m.
SUPPORTED_NAMES - Static variable in class org.orekit.frames.ITRFVersionLoader
Regular expression for supported files names.
supportsTimeTransform() - Method in class org.orekit.models.earth.GeoMagneticField
Indicates whether this model supports time transformation or not.
switchOccurred(AttitudeProvider, AttitudeProvider, SpacecraftState) - Method in interface org.orekit.attitudes.AttitudesSequence.SwitchHandler
Method called when attitude is switched from one law to another law.
sxpInitialize(T[]) - Method in class org.orekit.propagation.analytical.tle.FieldSGP4
Initialization proper to each propagator (SGP or SDP).
sxpInitialize(T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Initialization proper to each propagator (SGP or SDP).
sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.SGP4
Initialization proper to each propagator (SGP or SDP).
sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Initialization proper to each propagator (SGP or SDP).
sxpPropagate(T, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldSGP4
Propagation proper to each propagator (SGP or SDP).
sxpPropagate(T, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Propagation proper to each propagator (SGP or SDP).
sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.SGP4
Propagation proper to each propagator (SGP or SDP).
sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Propagation proper to each propagator (SGP or SDP).
SystemConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
 

T

t2cof - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
3/2 * C1.
t2cof - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
3/2 * C1.
TabulatedLofOffset - Class in org.orekit.attitudes
This class handles an attitude provider interpolating from a predefined table containing offsets from a Local Orbital Frame.
TabulatedLofOffset(Frame, LOFType, List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter) - Constructor for class org.orekit.attitudes.TabulatedLofOffset
Creates new instance.
TabulatedLofOffset(Frame, LOFType, List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.attitudes.TabulatedLofOffset
Creates new instance.
TabulatedProvider - Class in org.orekit.attitudes
This class handles an attitude provider interpolating from a predefined table.
TabulatedProvider(Frame, List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter) - Constructor for class org.orekit.attitudes.TabulatedProvider
Creates new instance.
TabulatedProvider(List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate, AttitudeBuilder) - Constructor for class org.orekit.attitudes.TabulatedProvider
Creates new instance.
TAIScale - Class in org.orekit.time
International Atomic Time.
TAIUTCDatFilesLoader - Class in org.orekit.time
Loader for UTC-TAI extracted from tai-utc.dat file from USNO.
TAIUTCDatFilesLoader(String) - Constructor for class org.orekit.time.TAIUTCDatFilesLoader
Build a loader for tai-utc.dat file from USNO.
TAIUTCDatFilesLoader(String, DataProvidersManager) - Constructor for class org.orekit.time.TAIUTCDatFilesLoader
Build a loader for tai-utc.dat file from USNO.
TAIUTCDatFilesLoader.Parser - Class in org.orekit.time
Internal class performing the parsing.
TargetPointing - Class in org.orekit.attitudes
This class handles target pointing attitude provider.
TargetPointing(Frame, Frame, Vector3D) - Constructor for class org.orekit.attitudes.TargetPointing
Creates a new instance from body frame and target expressed in Cartesian coordinates.
TargetPointing(Frame, GeodeticPoint, BodyShape) - Constructor for class org.orekit.attitudes.TargetPointing
Creates a new instance from body shape and target expressed in geodetic coordinates.
TCBScale - Class in org.orekit.time
Barycentric Coordinate Time.
TCGScale - Class in org.orekit.time
Geocentric Coordinate Time.
TDBScale - Class in org.orekit.time
Barycentric Dynamic Time.
Tdm - Class in org.orekit.files.ccsds.ndm.tdm
This class stores all the information of the CCSDS Tracking Data Message parsed by TDMParser or TDMXMLParser.
Tdm(Header, List<Segment<TdmMetadata, ObservationsBlock>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.tdm.Tdm
Simple constructor.
TdmDataKey - Enum in org.orekit.files.ccsds.ndm.tdm
Keys for TDM observations entries, except the measurements themselves.
TdmMetadata - Class in org.orekit.files.ccsds.ndm.tdm
The TDMMetadata class gathers the meta-data present in the Tracking Data Message (TDM).
TdmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Create a new TDM meta-data.
TdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.tdm
Keys for TDM container entries.
TdmParser - Class in org.orekit.files.ccsds.ndm.tdm
Class for CCSDS Tracking Data Message parsers.
TdmParser(IERSConventions, boolean, DataContext, ParsedUnitsBehavior, RangeUnitsConverter) - Constructor for class org.orekit.files.ccsds.ndm.tdm.TdmParser
Complete constructor.
TdmWriter - Class in org.orekit.files.ccsds.ndm.tdm
Writer for CCSDS Tracking Data Message.
TdmWriter(IERSConventions, DataContext, RangeUnitsConverter) - Constructor for class org.orekit.files.ccsds.ndm.tdm.TdmWriter
Complete constructor.
TDOA - Class in org.orekit.estimation.measurements
Class modeling a Time Difference of Arrival measurement with a satellite as emitter and two ground stations as receivers.
TDOA(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.TDOA
Simple constructor.
TDOABuilder - Class in org.orekit.estimation.measurements.generation
Builder for TDOA measurements.
TDOABuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.TDOABuilder
Simple constructor.
TDOAIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical TDOA measurements with ionospheric delay.
TDOAIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.TDOAIonosphericDelayModifier
Constructor.
TDOATroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical TDOA measurements with tropospheric delay.
TDOATroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.TDOATroposphericDelayModifier
Constructor.
TESLA - Static variable in class org.orekit.utils.units.Unit
tesla unit.
tessellate(SphericalPolygonsSet, double, double, double, double, boolean, boolean) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Tessellate a zone of interest into tiles.
THDT - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularAzEl
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularRaDec
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.BistaticRange
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.BistaticRangeRate
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSRange
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.Phase
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.InterSatellitesRange
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Position
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.PV
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Range
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.RangeRate
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.TDOA
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.TurnAroundRange
Estimate the theoretical value.
theoryIsSgpSdp() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
Check if mean element theory in SGP or SDP.
theta2 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
cos io squared.
theta2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
cos io squared.
ThirdBodyAttraction - Class in org.orekit.forces.gravity
Third body attraction force model.
ThirdBodyAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.ThirdBodyAttraction
Simple constructor.
ThirdBodyAttractionEpoch - Class in org.orekit.forces.gravity
Third body attraction force model.
ThirdBodyAttractionEpoch(CelestialBody) - Constructor for class org.orekit.forces.gravity.ThirdBodyAttractionEpoch
Simple constructor.
ThreeEighthesIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for ThreeEighthesIntegrator.
ThreeEighthesIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder
Build a new instance.
THRUST - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Parameter name for thrust.
THRUST_SCALE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Thrust scaling factor.
ThrustDirectionAndAttitudeProvider - Class in org.orekit.forces.maneuvers.propulsion
This class is used in to both manage the attitude of the satellite and the direction of thrust.
ThrustDirectionProvider - Interface in org.orekit.forces.maneuvers.propulsion
Interface to compute the thrust direction of a maneuver.
ThrustPropulsionModel - Interface in org.orekit.forces.maneuvers.propulsion
Interface for a thrust-based propulsion model.
THRUSTX_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Parameter name for the scale factor on the X component of the thrust in S/C frame.
THRUSTY_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Parameter name for the scale factor on the Y component of the thrust in S/C frame.
THRUSTZ_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Parameter name for the scale factor on the Z component of the thrust in S/C frame.
TidalDisplacement - Class in org.orekit.models.earth.displacement
Modeling of displacement of reference points due to tidal effects.
TidalDisplacement(double, double, double, PVCoordinatesProvider, PVCoordinatesProvider, IERSConventions, boolean) - Constructor for class org.orekit.models.earth.displacement.TidalDisplacement
Simple constructor.
Tide - Class in org.orekit.models.earth.displacement
Class representing a tide.
Tide(int, int, int, int, int, int) - Constructor for class org.orekit.models.earth.displacement.Tide
Simple constructor.
Tide(int) - Constructor for class org.orekit.models.earth.displacement.Tide
Simple constructor.
TideSystem - Enum in org.orekit.forces.gravity.potential
Enumerate for tie systems.
TideSystemProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide tide systems.
Tile - Class in org.orekit.models.earth.tessellation
Simple data structure for a quadrilateral tile shape on a body surface.
Tile(GeodeticPoint, GeodeticPoint, GeodeticPoint, GeodeticPoint) - Constructor for class org.orekit.models.earth.tessellation.Tile
Create a tile.
TileAiming - Interface in org.orekit.models.earth.tessellation
Interface defining the aiming direction of tiles.
TimeComponents - Class in org.orekit.time
Class representing a time within the day broken up as hour, minute and second components.
TimeComponents(int, int, double) - Constructor for class org.orekit.time.TimeComponents
Build a time from its clock elements.
TimeComponents(int, int, double, int) - Constructor for class org.orekit.time.TimeComponents
Build a time from its clock elements.
TimeComponents(double) - Constructor for class org.orekit.time.TimeComponents
Build a time from the second number within the day.
TimeComponents(int, double) - Constructor for class org.orekit.time.TimeComponents
Build a time from the second number within the day.
TimeConverter - Class in org.orekit.files.ccsds.definitions
Dates reader/writer.
TimeConverter(TimeScale, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.definitions.TimeConverter
Build a time system.
TimeDerivativesEquations - Interface in org.orekit.propagation.numerical
Interface summing up the contribution of several forces into orbit and mass derivatives.
TimeInterpolable<T extends TimeInterpolable<T>> - Interface in org.orekit.time
This interface represents objects that can be interpolated in time.
TimeScalarFunction - Interface in org.orekit.time
This interface represents a scalar function of time.
TimeScale - Interface in org.orekit.time
Interface for time scales.
TimeScales - Interface in org.orekit.time
A collection of TimeScales.
TimeScalesFactory - Class in org.orekit.time
Factory for predefined time scales.
timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Compute the offset between two time scales at the current instant.
timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the offset between two time scales at the current instant.
TimeShiftable<T extends TimeShiftable<T>> - Interface in org.orekit.time
This interface represents objects that can be shifted in time.
TimeSpanDragForce - Class in org.orekit.forces.drag
Time span atmospheric drag force model.
TimeSpanDragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.TimeSpanDragForce
Constructor with default UTC time scale for the default names of the drag parameter drivers.
TimeSpanDragForce(Atmosphere, DragSensitive, TimeScale) - Constructor for class org.orekit.forces.drag.TimeSpanDragForce
Constructor.
TimeSpanEstimatedTroposphericModel - Class in org.orekit.models.earth.troposphere
Time span estimated tropospheric model.
TimeSpanEstimatedTroposphericModel(EstimatedTroposphericModel) - Constructor for class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Constructor with default UTC time scale.
TimeSpanEstimatedTroposphericModel(EstimatedTroposphericModel, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Constructor with default UTC time scale.
TimeSpanMap<T> - Class in org.orekit.utils
Container for objects that apply to spans of time.
TimeSpanMap(T) - Constructor for class org.orekit.utils.TimeSpanMap
Create a map containing a single object, initially valid throughout the timeline.
TimeSpanMap.Span<S> - Class in org.orekit.utils
Holder for one time span.
TimeSpanMap.Transition<S> - Class in org.orekit.utils
Class holding transition times.
TimeSpanParametricAcceleration - Class in org.orekit.forces.empirical
Time span parametric acceleration model.
TimeSpanParametricAcceleration(Vector3D, boolean, AccelerationModel) - Constructor for class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Simple constructor.
TimeSpanParametricAcceleration(Vector3D, AttitudeProvider, AccelerationModel) - Constructor for class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Simple constructor.
TimeStamped - Interface in org.orekit.time
This interface represents objects that have a AbsoluteDate date attached to them.
TimeStampedAngularCoordinates - Class in org.orekit.utils
TimeStampedAngularCoordinates(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Builds a rotation/rotation rate pair.
TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another pair.
TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Build one of the rotations that transform one pv coordinates into another one.
TimeStampedAngularCoordinates(AbsoluteDate, FieldRotation<U>) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Builds a TimeStampedAngularCoordinates from a FieldRotation<Derivative>.
TimeStampedCache<T extends TimeStamped> - Interface in org.orekit.utils
Interface for a data structure that can provide concurrent access to TimeStamped data surrounding a given date.
TimeStampedCacheException - Exception in org.orekit.errors
This class is the base class for all specific exceptions thrown by during the GenericTimeStampedCache.
TimeStampedCacheException(Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedCacheException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedCacheException(OrekitException) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedCacheException(MathRuntimeException) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedFieldAngularCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
TimeStampedFieldAngularCoordinates(AbsoluteDate, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another pair.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another pair.
TimeStampedFieldAngularCoordinates(AbsoluteDate, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds a rotation/rotation rate pair.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds a rotation/rotation rate pair.
TimeStampedFieldAngularCoordinates(Field<T>, TimeStampedAngularCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds an instance for a regular TimeStampedAngularCoordinates.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldRotation<U>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds a TimeStampedFieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.
TimeStampedFieldPVCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils
TimeStampedFieldPVCoordinates(AbsoluteDate, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Builds a PVCoordinates pair.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Builds a PVCoordinates pair.
TimeStampedFieldPVCoordinates(AbsoluteDate, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Basic constructor.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Basic constructor.
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Subtractive constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Subtractive constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldVector3D<U>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Builds a TimeStampedFieldPVCoordinates triplet from a FieldVector3D<FieldDerivativeStructure>.
TimeStampedGenerator<T extends TimeStamped> - Interface in org.orekit.utils
Generator to use for creating entries in time stamped caches.
TimeStampedPVCoordinates - Class in org.orekit.utils
TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Builds a TimeStampedPVCoordinates pair.
TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Build from position and velocity.
TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Build from position velocity acceleration coordinates.
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Multiplicative constructor
TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Subtractive constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, FieldVector3D<U>) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Builds a TimeStampedPVCoordinates triplet from a FieldVector3D<Derivative>.
TimeSystem - Enum in org.orekit.files.ccsds.definitions
The set of time systems defined in CCSDS standards (ADM, ODM, NDM).
TimeSystem - Enum in org.orekit.gnss
Enumerate for the time systems used in navigation files.
TimeSystemCorrection(String, double, double, int, int) - Constructor for class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection
Constructor.
TimetagReference - Enum in org.orekit.files.ccsds.ndm.tdm
Reference for time tag.
TimeVectorFunction - Interface in org.orekit.time
This interface represents a multi-valued function of time.
TimingSystemConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
 
tle - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
Initial state.
TLE - Class in org.orekit.propagation.analytical.tle
This class is a container for a single set of TLE data.
TLE(String, String) - Constructor for class org.orekit.propagation.analytical.tle.TLE
Simple constructor from unparsed two lines.
TLE(String, String, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.TLE
Simple constructor from unparsed two lines using the given time scale as UTC.
TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double) - Constructor for class org.orekit.propagation.analytical.tle.TLE
Simple constructor from already parsed elements.
TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.TLE
Simple constructor from already parsed elements using the given time scale as UTC.
tle - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
Initial state.
TLEBatchLSModel - Class in org.orekit.estimation.leastsquares
Deprecated.
as of 11.1, replaced by BatchLSModel
TLEBatchLSModel(OrbitDeterminationPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Constructor for class org.orekit.estimation.leastsquares.TLEBatchLSModel
Deprecated.
Simple constructor.
TLEConstants - Class in org.orekit.propagation.analytical.tle
Constants necessary to TLE propagation.
TLEJacobiansMapper - Class in org.orekit.propagation.analytical.tle
Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
TLEJacobiansMapper(String, ParameterDriversList, TLEPropagator) - Constructor for class org.orekit.propagation.analytical.tle.TLEJacobiansMapper
Simple constructor.
TLEKalmanModel - Class in org.orekit.estimation.sequential
Deprecated.
as of 11.1, replaced by KalmanModel
TLEKalmanModel(List<OrbitDeterminationPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.TLEKalmanModel
Deprecated.
Kalman process model constructor (package private).
TLEPartialDerivativesEquations - Class in org.orekit.propagation.analytical.tle
Deprecated.
TLEPartialDerivativesEquations(String, TLEPropagator) - Constructor for class org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations
Deprecated.
Simple constructor.
TLEPropagator - Class in org.orekit.propagation.analytical.tle
This class provides elements to propagate TLE's.
TLEPropagator(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.TLEPropagator
Protected constructor for derived classes.
TLEPropagator(TLE, AttitudeProvider, double, Frame) - Constructor for class org.orekit.propagation.analytical.tle.TLEPropagator
Protected constructor for derived classes.
TLEPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for TLEPropagator.
TLEPropagatorBuilder(TLE, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder
Build a new instance.
TLEPropagatorBuilder(TLE, PositionAngle, double, DataContext) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder
Build a new instance.
TLEPropagatorBuilder(TLE, PositionAngle, double, double, int) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder
Build a new instance.
TLEPropagatorBuilder(TLE, PositionAngle, double, DataContext, double, int) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder
Build a new instance.
toAbsoluteDate() - Method in class org.orekit.time.FieldAbsoluteDate
Transform the FieldAbsoluteDate in an AbsoluteDate.
toAbsolutePVCoordinates() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Converts to an AbsolutePVCoordinates instance.
toAngularCoordinates() - Method in class org.orekit.utils.FieldAngularCoordinates
Convert to a regular angular coordinates.
toArray(List<List<Double>>) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Deprecated.
as of 11.1, not used anymore
toAttitude() - Method in class org.orekit.attitudes.FieldAttitude
Converts to an Attitude instance.
toCartesian(AbsoluteDate, double[], double) - Method in enum org.orekit.files.ccsds.definitions.ElementsType
Convert to Cartesian coordinates.
toCartesian(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
Convert to Cartesian coordinates.
toDate(DateComponents) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Create a date from components.
toDate(DateComponents, TimeComponents) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Create a date from components.
toDate(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Convert the instance to a Java Date.
toDate(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Convert the instance to a Java Date.
toDerivativeStructurePV(int) - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldPVCoordinates<FieldDerivativeStructure>.
toDerivativeStructurePV(int) - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldPVCoordinates<DerivativeStructure>.
toDerivativeStructureRotation(int) - Method in class org.orekit.utils.AngularCoordinates
Transform the instance to a FieldRotation<DerivativeStructure>.
toDerivativeStructureRotation(int) - Method in class org.orekit.utils.FieldAngularCoordinates
Transform the instance to a FieldRotation<FieldDerivativeStructure>.
toDerivativeStructureVector(int) - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldVector3D<FieldDerivativeStructure>.
toDerivativeStructureVector(int) - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldVector3D<DerivativeStructure>.
toEopEntry(IERSConventions.NutationCorrectionConverter, ITRFVersion, TimeScale) - Method in class org.orekit.files.sinex.SinexEopEntry
Converts to an EOPEntry.
toEquinox(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter
Convert nutation corrections.
toFieldPVCoordinatesProvider(Field<T>) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider
Convert to a FieldPVCoordinatesProvider with a specific type.
toGeodetic(S2Point) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Convert a point on the unit 2-sphere to geodetic coordinates.
TokenType - Enum in org.orekit.files.ccsds.utils.lexical
Enumerate for tokens occurring during CCSDS file parsing.
tolerances(T, FieldOrbit<T>, OrbitType) - Static method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Estimate tolerance vectors for integrators.
tolerances(T, T, FieldOrbit<T>, OrbitType) - Static method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Estimate tolerance vectors for integrators when propagating in orbits.
tolerances(double, AbsolutePVCoordinates) - Static method in class org.orekit.propagation.numerical.NumericalPropagator
Estimate tolerance vectors for integrators when propagating in absolute position-velocity-acceleration.
tolerances(double, Orbit, OrbitType) - Static method in class org.orekit.propagation.numerical.NumericalPropagator
Estimate tolerance vectors for integrators when propagating in orbits.
tolerances(double, double, Orbit, OrbitType) - Static method in class org.orekit.propagation.numerical.NumericalPropagator
Estimate tolerance vectors for integrators when propagating in orbits.
tolerances(double, Orbit) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
tolerances(double, double, Orbit) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
tolerances(T, FieldOrbit<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
tolerances(T, T, FieldOrbit<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
toMap() - Method in class org.orekit.utils.DoubleArrayDictionary
Create a map from the instance.
toMap() - Method in class org.orekit.utils.FieldArrayDictionary
Create a map from the instance.
ton2a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
2 / (n² * a) .
ton2a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
2 / (n² * a) .
toNonRotating(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter
Convert nutation corrections.
toOrbit() - Method in class org.orekit.orbits.FieldCartesianOrbit
 
toOrbit() - Method in class org.orekit.orbits.FieldCircularOrbit
Transforms the FieldOrbit instance into an Orbit instance.
toOrbit() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Transforms the FieldOrbit instance into an Orbit instance.
toOrbit() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Transforms the FieldOrbit instance into an Orbit instance.
toOrbit() - Method in class org.orekit.orbits.FieldOrbit
Transforms the FieldOrbit instance into an Orbit instance.
toPlane(Vector3D) - Method in class org.orekit.bodies.Ellipse
Project a point to the ellipse plane.
TopocentricFrame - Class in org.orekit.frames
Topocentric frame.
TopocentricFrame(BodyShape, GeodeticPoint, String) - Constructor for class org.orekit.frames.TopocentricFrame
Simple constructor.
toPVCoordinates() - Method in class org.orekit.utils.FieldPVCoordinates
Convert to a constant position-velocity.
toSI(double) - Method in enum org.orekit.data.PolynomialParser.Unit
Convert value from instance unit to corresponding SI unit.
toSI(double) - Method in class org.orekit.utils.units.Unit
Convert a value to SI units.
toSI(Double) - Method in class org.orekit.utils.units.Unit
Convert a value to SI units.
toSpace(Vector2D) - Method in class org.orekit.bodies.Ellipse
Create a point from its ellipse-relative coordinates.
toSpacecraftState() - Method in class org.orekit.propagation.FieldSpacecraftState
To convert a FieldSpacecraftState instance into a SpacecraftState instance.
toString() - Method in class org.orekit.bodies.FieldGeodeticPoint
 
toString() - Method in class org.orekit.bodies.GeodeticPoint
 
toString() - Method in enum org.orekit.files.ccsds.definitions.ElementsType
toString() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame
toString() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
toString() - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
toString() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
toString() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
toString() - Method in class org.orekit.frames.Frame
New definition of the java.util toString() method.
toString() - Method in class org.orekit.frames.OrphanFrame
toString() - Method in class org.orekit.gnss.metric.ntrip.GnssData
 
toString() - Method in enum org.orekit.gnss.metric.ntrip.NavigationSystem
toString() - Method in class org.orekit.models.earth.GeoMagneticElements
 
toString() - Method in class org.orekit.orbits.CartesianOrbit
Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.CircularOrbit
Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.EquinoctialOrbit
Returns a string representation of this equinoctial parameters object.
toString() - Method in class org.orekit.orbits.FieldCartesianOrbit
Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.FieldCircularOrbit
Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Returns a string representation of this equinoctial parameters object.
toString() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Returns a string representation of this Keplerian parameters object.
toString() - Method in class org.orekit.orbits.KeplerianOrbit
Returns a string representation of this Keplerian parameters object.
toString() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Get a string representation of this TLE set.
toString() - Method in class org.orekit.propagation.analytical.tle.TLE
Get a string representation of this TLE set.
toString() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event
 
toString() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
 
toString() - Method in class org.orekit.propagation.FieldSpacecraftState
 
toString() - Method in class org.orekit.propagation.SpacecraftState
 
toString() - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location with up to 16 digits of precision for the seconds value.
toString(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location in ISO-8601 format without the UTC offset and with up to 16 digits of precision for the seconds value.
toString(int) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location for a local time.
toString(int, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location for a local time.
toString(TimeZone) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location for a time zone.
toString(TimeZone, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location for a time zone.
toString() - Method in class org.orekit.time.BDTScale
toString() - Method in class org.orekit.time.DateComponents
Get a string representation (ISO-8601) of the date.
toString() - Method in class org.orekit.time.DateTimeComponents
Return a string representation of this pair.
toString(int) - Method in class org.orekit.time.DateTimeComponents
Return a string representation of this date-time, rounded to millisecond precision.
toString(int, int) - Method in class org.orekit.time.DateTimeComponents
Return a string representation of this date-time, rounded to the given precision.
toString() - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location with up to 16 digits of precision for the seconds value.
toString(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location in ISO-8601 format without the UTC offset and with up to 16 digits of precision for the seconds value.
toString(int) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location for a local time.
toString(int, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location for a local time.
toString(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location for a time zone.
toString(TimeZone, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location for a time zone.
toString() - Method in class org.orekit.time.GalileoScale
toString() - Method in class org.orekit.time.GLONASSScale
toString() - Method in class org.orekit.time.GMSTScale
toString() - Method in class org.orekit.time.GPSScale
toString() - Method in class org.orekit.time.IRNSSScale
toString() - Method in class org.orekit.time.QZSSScale
toString() - Method in class org.orekit.time.SatelliteClockScale
toString() - Method in class org.orekit.time.TAIScale
toString() - Method in class org.orekit.time.TCBScale
toString() - Method in class org.orekit.time.TCGScale
toString() - Method in class org.orekit.time.TDBScale
toString() - Method in class org.orekit.time.TimeComponents
Get a string representation of the time including the offset from UTC.
toString() - Method in class org.orekit.time.TTScale
toString() - Method in class org.orekit.time.UT1Scale
toString() - Method in class org.orekit.time.UTCScale
toString() - Method in class org.orekit.utils.DoubleArrayDictionary
Get a string representation of the dictionary.
toString() - Method in class org.orekit.utils.FieldArrayDictionary
Get a string representation of the dictionary.
toString() - Method in class org.orekit.utils.FieldPVCoordinates
Return a string representation of this position/velocity pair.
toString() - Method in class org.orekit.utils.ImmutableTimeStampedCache
toString() - Method in class org.orekit.utils.ParameterDriver
Get a text representation of the parameter.
toString() - Method in class org.orekit.utils.PVCoordinates
Return a string representation of this position/velocity pair.
toString() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Return a string representation of this date, position, velocity, and acceleration.
toString(TimeScale) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Return a string representation of this date, position, velocity, and acceleration.
toString() - Method in class org.orekit.utils.TimeStampedPVCoordinates
Return a string representation of this date, position, velocity, and acceleration.
toString(TimeScale) - Method in class org.orekit.utils.TimeStampedPVCoordinates
Return a string representation of this date, position, velocity, and acceleration.
toString() - Method in class org.orekit.utils.units.Unit
toString() - Method in class org.orekit.utils.units.UnitsConverter
toStringRfc3339(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Represent the given date as a string according to the format in RFC 3339.
toStringRfc3339() - Method in class org.orekit.time.DateTimeComponents
Represent the given date and time as a string according to the format in RFC 3339.
toStringWithoutUtcOffset(TimeScale, int) - Method in class org.orekit.time.AbsoluteDate
Return a string representation of this date-time, rounded to the given precision.
toStringWithoutUtcOffset() - Method in class org.orekit.time.DateTimeComponents
Get a string representation of the date-time without the offset from UTC.
toStringWithoutUtcOffset(int, int) - Method in class org.orekit.time.DateTimeComponents
Return a string representation of this date-time, rounded to the given precision.
toStringWithoutUtcOffset() - Method in class org.orekit.time.TimeComponents
Get a string representation of the time without the offset from UTC.
TOTAL_ELECTRON_CONTENT_UNIT - Static variable in class org.orekit.utils.units.Unit
Total Electron Content Unit.
TOTAL_ZENITH_DELAY - Static variable in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Name of the parameter of this model: the total zenith delay.
toTaylorProvider() - Method in class org.orekit.utils.AbsolutePVCoordinates
Create a local provider using simply Taylor expansion through AbsolutePVCoordinates.shiftedBy(double).
toTaylorProvider() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Create a local provider using simply Taylor expansion through FieldAbsolutePVCoordinates.shiftedBy(double).
toTaylorProvider(Frame) - Method in class org.orekit.utils.TimeStampedPVCoordinates
Create a local provider using simply Taylor expansion through TimeStampedPVCoordinates.shiftedBy(double).
toTimeStampedPVCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
toTimeStampedPVCoordinates() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Convert to a constant position-velocity.
toTLE() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
Convert FieldTLE into TLE.
toTransform() - Method in class org.orekit.propagation.FieldSpacecraftState
Compute the transform from state defining frame to spacecraft frame.
toTransform() - Method in class org.orekit.propagation.SpacecraftState
Compute the transform from state defining frame to spacecraft frame.
toUnivariateDerivative1PV() - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldPVCoordinates<FieldUnivariateDerivative1>.
toUnivariateDerivative1PV() - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldPVCoordinates<UnivariateDerivative1>.
toUnivariateDerivative1Rotation() - Method in class org.orekit.utils.AngularCoordinates
Transform the instance to a FieldRotation<UnivariateDerivative1>.
toUnivariateDerivative1Rotation() - Method in class org.orekit.utils.FieldAngularCoordinates
Transform the instance to a FieldRotation<UnivariateDerivative1>.
toUnivariateDerivative1Vector() - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldVector3D<FieldUnivariateDerivative1>.
toUnivariateDerivative1Vector() - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldVector3D<UnivariateDerivative1>.
toUnivariateDerivative2PV() - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldPVCoordinates<FieldUnivariateDerivative2>.
toUnivariateDerivative2PV() - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldPVCoordinates<UnivariateDerivative2>.
toUnivariateDerivative2Rotation() - Method in class org.orekit.utils.AngularCoordinates
Transform the instance to a FieldRotation<UnivariateDerivative2>.
toUnivariateDerivative2Rotation() - Method in class org.orekit.utils.FieldAngularCoordinates
Transform the instance to a FieldRotation<UnivariateDerivative2>.
toUnivariateDerivative2Vector() - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldVector3D<FieldUnivariateDerivative2>.
toUnivariateDerivative2Vector() - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldVector3D<UnivariateDerivative2>.
TrackingMode - Enum in org.orekit.files.ccsds.ndm.tdm
Tracking mode.
TRAJ_LINE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Trajectory line element for XML messages.
TrajectoryState - Class in org.orekit.files.ccsds.ndm.odm.ocm
Trajectory state entry.
TrajectoryState(ElementsType, AbsoluteDate, String[], int, List<Unit>) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
Simple constructor.
TrajectoryStateHistory - Class in org.orekit.files.ccsds.ndm.odm.ocm
Trajectory state history.
TrajectoryStateHistoryMetadata - Class in org.orekit.files.ccsds.ndm.odm.ocm
Metadata for trajectory state history.
TrajectoryStateHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm
transform(Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape
Transform a Cartesian point to a surface-relative point.
transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape
Transform a Cartesian point to a surface-relative point.
transform(GeodeticPoint) - Method in interface org.orekit.bodies.BodyShape
Transform a surface-relative point to a Cartesian point.
transform(FieldGeodeticPoint<T>) - Method in interface org.orekit.bodies.BodyShape
Transform a surface-relative point to a Cartesian point.
transform(GeodeticPoint) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a surface-relative point to a Cartesian point.
transform(FieldGeodeticPoint<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a surface-relative point to a Cartesian point.
transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a Cartesian point to a surface-relative point.
transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a Cartesian point to a surface-relative point.
transform(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a Cartesian point to a surface-relative point.
Transform - Class in org.orekit.frames
Transformation class in three dimensional space.
Transform(AbsoluteDate, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a translation transform.
Transform(AbsoluteDate, Rotation) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a translation transform, with its first time derivative.
Transform(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a translation transform, with its first and second time derivatives.
Transform(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.frames.Transform
Build a translation transform, with its first time derivative.
Transform(AbsoluteDate, Rotation, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, AngularCoordinates) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, Transform, Transform) - Constructor for class org.orekit.frames.Transform
Build a transform by combining two existing ones.
transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
Transform a Cartesian point to a surface-relative point.
transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid
Transform a Cartesian point to a surface-relative point.
transform(GeodeticPoint) - Method in class org.orekit.models.earth.Geoid
Transform a surface-relative point to a Cartesian point.
transform(FieldGeodeticPoint<T>) - Method in class org.orekit.models.earth.Geoid
Transform a surface-relative point to a Cartesian point.
transformFromInertial(AbsoluteDate, PVCoordinates) - Method in enum org.orekit.frames.LOFType
Get the transform from an inertial frame defining position-velocity and the local orbital frame.
transformFromInertial(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType
Get the transform from an inertial frame defining position-velocity and the local orbital frame.
TransformGenerator - Class in org.orekit.frames
Generator to use transforms in GenericTimeStampedCache.
TransformGenerator(int, TransformProvider, double) - Constructor for class org.orekit.frames.TransformGenerator
simple constructor.
transformLine(Line) - Method in class org.orekit.frames.FieldTransform
Transform a line.
transformLine(FieldLine<T>) - Method in class org.orekit.frames.FieldTransform
Transform a line.
transformLine(Line) - Method in interface org.orekit.frames.StaticTransform
Transform a line.
transformModel(double) - Method in class org.orekit.models.earth.GeoMagneticField
Time transform the model coefficients from the base year of the model using secular variation coefficients.
transformModel(GeoMagneticField, double) - Method in class org.orekit.models.earth.GeoMagneticField
Time transform the model coefficients from the base year of the model using a linear interpolation with a second model.
transformPosition(Vector3D) - Method in class org.orekit.frames.FieldTransform
Transform a position vector (including translation effects).
transformPosition(FieldVector3D<T>) - Method in class org.orekit.frames.FieldTransform
Transform a position vector (including translation effects).
transformPosition(Vector3D) - Method in interface org.orekit.frames.StaticTransform
Transform a position vector (including translation effects).
transformPosition(FieldVector3D<T>) - Method in interface org.orekit.frames.StaticTransform
Transform a position vector (including translation effects).
TransformProvider - Interface in org.orekit.frames
Interface for Transform providers.
TransformProviderUtils - Class in org.orekit.frames
Utility for Transform providers.
transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedPVCoordinates including kinematic effects.
transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.Transform
Transform PVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.Transform
Transform TimeStampedPVCoordinates including kinematic effects.
transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform
Transform FieldPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform
Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformVector(Vector3D) - Method in class org.orekit.frames.FieldTransform
Transform a vector (ignoring translation effects).
transformVector(FieldVector3D<T>) - Method in class org.orekit.frames.FieldTransform
Transform a vector (ignoring translation effects).
transformVector(Vector3D) - Method in interface org.orekit.frames.StaticTransform
Transform a vector (ignoring translation effects).
transformVector(FieldVector3D<T>) - Method in interface org.orekit.frames.StaticTransform
Transform a vector (ignoring translation effects).
TransponderConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
 
TriggerDate - Class in org.orekit.forces.maneuvers.jacobians
Generator for one column of a Jacobian matrix for special case of trigger dates.
TriggerDate(String, String, boolean, Maneuver, double) - Constructor for class org.orekit.forces.maneuvers.jacobians.TriggerDate
Simple constructor.
TroposphericGradientConverter - Class in org.orekit.estimation.measurements.modifiers
Deprecated.
as of 11.2, replaced by ModifierGradientConverter
TroposphericGradientConverter(SpacecraftState, int, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.TroposphericGradientConverter
Deprecated.
Simple constructor.
TroposphericModelUtils - Class in org.orekit.models.earth.troposphere
Utility class for tropospheric models.
TRUE_ANOM - Static variable in enum org.orekit.orbits.OrbitType
Name for mean anomaly.
TRUE_LAT_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for mean argument of latitude.
TRUE_LON_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for mean argument of longitude.
trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit
Computes the eccentric latitude argument from the true latitude argument.
trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit
Computes the eccentric longitude argument from the true longitude argument.
trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit
Computes the eccentric latitude argument from the true latitude argument.
trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
Computes the eccentric longitude argument from the true longitude argument.
trueToEllipticEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the elliptic eccentric anomaly from the true anomaly.
trueToEllipticEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the elliptic eccentric anomaly from the true anomaly.
trueToHyperbolicEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the hyperbolic eccentric anomaly from the true anomaly.
trueToHyperbolicEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the hyperbolic eccentric anomaly from the true anomaly.
tryAdvance(SpacecraftState, OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState
Try to accept the current history up to the given time.
tryAdvance(FieldSpacecraftState<T>, FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState
Try to accept the current history up to the given time.
tsi - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
tsi from SPTRCK #3.
tsi - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
tsi from SPTRCK #3.
TTScale - Class in org.orekit.time
Terrestrial Time as defined by IAU(1991) recommendation IV.
TurnAroundRange - Class in org.orekit.estimation.measurements
Class modeling a turn-around range measurement using a primary ground station and a secondary ground station.
TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.TurnAroundRange
Simple constructor.
TurnAroundRangeBuilder - Class in org.orekit.estimation.measurements.generation
Builder for TurnAroundRange measurements.
TurnAroundRangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.TurnAroundRangeBuilder
Simple constructor.
TurnAroundRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical TurnAroundRange measurement with ionospheric delay.
TurnAroundRangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier
Constructor.
TurnAroundRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical turn-around TurnAroundRange measurement with tropospheric delay.
TurnAroundRangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier
Constructor.
TWO_THIRD - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
Constant 2.0 / 3.0.
TwoBodiesBaryFrame - Class in org.orekit.frames
Class creating the inertial barycenter frame from two bodies.
TwoBodiesBaryFrame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.TwoBodiesBaryFrame
Simple constructor.
Type - Enum in org.orekit.gnss.metric.ntrip
Enumerate for messages type.

U

unableToParseLine(Throwable) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader
Deprecated.
Annotate an exception with the file context.
unFixAmbiguity(ParameterDriver) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Un-fix an integer ambiguity (typically after a phase cycle slip).
Unit - Class in org.orekit.utils.units
Basic handling of multiplicative units.
Unit(String, double, Fraction, Fraction, Fraction, Fraction, Fraction) - Constructor for class org.orekit.utils.units.Unit
Simple constructor.
Units - Class in org.orekit.files.ccsds.definitions
Units used in CCSDS messages.
UNITS - Static variable in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Name of the units attribute.
Units - Class in org.orekit.gnss.metric.parser
Units used in RTCM and IGS SSR messages.
UnitsCache - Class in org.orekit.utils.units
Cache for parsed units.
UnitsCache() - Constructor for class org.orekit.utils.units.UnitsCache
Simple constructor.
UnitsConverter - Class in org.orekit.utils.units
Converter between units.
UnitsConverter(Unit, Unit) - Constructor for class org.orekit.utils.units.UnitsConverter
Simple constructor.
unitsListToString(List<Unit>) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Convert a list of units to a bracketed string.
unitsListToString(List<Unit>) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Convert a list of units to a bracketed string.
UnivariateProcessNoise - Class in org.orekit.estimation.sequential
Provider for a temporal evolution of the process noise matrix.
UnivariateProcessNoise(RealMatrix, LOFType, PositionAngle, UnivariateFunction[], UnivariateFunction[]) - Constructor for class org.orekit.estimation.sequential.UnivariateProcessNoise
Simple constructor.
UnivariateProcessNoise(RealMatrix, LOFType, PositionAngle, UnivariateFunction[], UnivariateFunction[], UnivariateFunction[]) - Constructor for class org.orekit.estimation.sequential.UnivariateProcessNoise
Simple constructor.
UnixCompressFilter - Class in org.orekit.data
Filter for Unix compressed data.
UnixCompressFilter() - Constructor for class org.orekit.data.UnixCompressFilter
 
UNKNOWN_OBJECT - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
Default name for unknown object.
unmodifiableView() - Method in class org.orekit.utils.DoubleArrayDictionary
Get an unmodifiable view of the dictionary.
unmodifiableView() - Method in class org.orekit.utils.FieldArrayDictionary
Get an unmodifiable view of the dictionary.
UnnormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide un-normalized spherical harmonics coefficients.
UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential
Un-normalized spherical harmonics coefficients evaluated at a specific instant.
unwrap(MathRuntimeException) - Static method in exception org.orekit.errors.OrekitException
Recover a OrekitException, possibly embedded in a MathRuntimeException.
unwrap(OrekitException) - Static method in exception org.orekit.errors.TimeStampedCacheException
Recover a TimeStampedCacheException, possibly embedded in a OrekitException.
unwrap(MathRuntimeException) - Static method in exception org.orekit.errors.TimeStampedCacheException
Recover a TimeStampedCacheException, possibly embedded in a MathRuntimeException.
UpdatableFrame - Class in org.orekit.frames
Frame whose transform from its parent can be updated.
UpdatableFrame(Frame, Transform, String) - Constructor for class org.orekit.frames.UpdatableFrame
Build a non-inertial frame from its transform with respect to its parent.
UpdatableFrame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.UpdatableFrame
Build a frame from its transform with respect to its parent.
updateAdditionalConstraints(int, double[]) - Method in class org.orekit.utils.AbstractMultipleShooting
Update the array of additional constraints.
updateAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
Update state by adding all additional states.
updateAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Update state by adding all additional states.
updateAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Update state by adding all additional states.
updateAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Update state by adding all additional states.
updateFieldShortPeriodTerms(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
Update the short periodic terms for the "field" elements.
updateMass(double) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Update a spacecraft mass due to maneuver.
updateNominalSpacecraftState(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Update the nominal spacecraft state.
updateReferenceTrajectories(Propagator[], PropagationType, PropagationType) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
Update the reference trajectories using the propagators as input.
updateReferenceTrajectories(Propagator[], PropagationType, PropagationType) - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Deprecated.
Update the reference trajectories using the propagators as input.
updateReferenceTrajectories(Propagator[], PropagationType, PropagationType) - Method in class org.orekit.estimation.sequential.KalmanModel
Update the reference trajectories using the propagators as input.
updateReferenceTrajectories(Propagator[], PropagationType, PropagationType) - Method in class org.orekit.estimation.sequential.TLEKalmanModel
Deprecated.
Update the reference trajectories using the propagators as input.
updateReferenceTrajectory(DSSTPropagator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Update the reference trajectories using the propagator as input.
updateShortPeriods(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
Update the DSST short periodic terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Update the short period terms.
updateTransform(Frame, Frame, Transform, AbsoluteDate) - Method in class org.orekit.frames.UpdatableFrame
Update the transform from parent frame implicitly according to two other frames.
updateUnmanagedStates(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
Update state by adding unmanaged states.
updateUnmanagedStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Update state by adding unmanaged states.
UpperBounds - Class in org.orekit.propagation.semianalytical.dsst.utilities
Utility class to compute upper bounds for truncation algorithms.
URANUS - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Uranus.
USER_DEFINED_PREFIX - Static variable in class org.orekit.files.ccsds.ndm.odm.UserDefined
Prefix for user defined parameters keys.
USER_DEFINED_XML_ATTRIBUTE - Static variable in class org.orekit.files.ccsds.ndm.odm.UserDefined
Attribute name for user defined parameters keys.
USER_DEFINED_XML_TAG - Static variable in class org.orekit.files.ccsds.ndm.odm.UserDefined
Tag name for user defined parameters keys.
UserDefined - Class in org.orekit.files.ccsds.ndm.odm
Container for user defined data.
UserDefined() - Constructor for class org.orekit.files.ccsds.ndm.odm.UserDefined
Create an empty data set.
UserDefinedWriter - Class in org.orekit.files.ccsds.ndm.odm
Writer for user defined parameters data.
UserDefinedWriter(String, String, UserDefined) - Constructor for class org.orekit.files.ccsds.ndm.odm.UserDefinedWriter
Create a writer.
UserDefinedXmlTokenBuilder - Class in org.orekit.files.ccsds.utils.lexical
Builder for user-defined parameters.
UserDefinedXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.utils.lexical.UserDefinedXmlTokenBuilder
 
UserRangeAccuracy - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris.utils
User Range Accuracy.
UserRangeAccuracy(int) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.UserRangeAccuracy
Simple constructor.
usesInterpolation() - Method in class org.orekit.frames.EOPHistory
Check if the instance uses interpolation on tidal corrections.
UT1Scale - Class in org.orekit.time
Universal Time 1.
UT1Scale(EOPHistory, UTCScale) - Constructor for class org.orekit.time.UT1Scale
Simple constructor.
utc - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
UTC time scale.
utc - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
UTC time scale.
UTCScale - Class in org.orekit.time
Coordinated Universal Time.
UTCTAIBulletinAFilesLoader - Class in org.orekit.time
Loader for UTC-TAI extracted from bulletin A files.
UTCTAIBulletinAFilesLoader(String) - Constructor for class org.orekit.time.UTCTAIBulletinAFilesLoader
Build a loader for IERS bulletins A files.
UTCTAIBulletinAFilesLoader(String, DataProvidersManager) - Constructor for class org.orekit.time.UTCTAIBulletinAFilesLoader
Build a loader for IERS bulletins A files.
UTCTAIHistoryFilesLoader - Class in org.orekit.time
Loader for UTC versus TAI history files.
UTCTAIHistoryFilesLoader() - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader
Build a loader for UTC-TAI history file.
UTCTAIHistoryFilesLoader(DataProvidersManager) - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader
Build a loader for UTC-TAI history file.
UTCTAIHistoryFilesLoader.Parser - Class in org.orekit.time
Internal class performing the parsing.
UTCTAIOffset - Class in org.orekit.time
Offset between UTC and TAI time scales.
UTCTAIOffsetsLoader - Interface in org.orekit.time
Interface for loading UTC-TAI offsets data files.
UTCTAIOffsetsLoader.Parser - Interface in org.orekit.time
Interface for parsing UTC-TAI offsets from a stream.
UTF8Control() - Constructor for class org.orekit.errors.OrekitMessages.UTF8Control
 

V

validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmHeader
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Check is all mandatory entries have been initialized.
validate() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector
Check is all mandatory entries have been initialized.
validate() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
Validate the file message for required and forbidden entries.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.section.Header
Check is all mandatory entries have been initialized.
validate(double) - Method in class org.orekit.files.ccsds.section.Metadata
Check is all mandatory entries have been initialized.
validate(double) - Method in interface org.orekit.files.ccsds.section.Section
Check is all mandatory entries have been initialized.
validFrom() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the start of the validity period for this model.
validityEnd() - Method in interface org.orekit.gnss.attitude.GNSSAttitudeProvider
Get end of validity for this provider.
validityStart() - Method in interface org.orekit.gnss.attitude.GNSSAttitudeProvider
Get start of validity for this provider.
validTo() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the end of the validity period for this model.
value(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate a set of Poisson series.
value(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate a set of Poisson series.
value(BodiesElements) - Method in class org.orekit.data.PoissonSeries
Evaluate the value of the series.
value(FieldBodiesElements<T>) - Method in class org.orekit.data.PoissonSeries
Evaluate the value of the series.
value(double) - Method in class org.orekit.data.PolynomialNutation
Evaluate the value of the polynomial.
value(T) - Method in class org.orekit.data.PolynomialNutation
Evaluate the value of the polynomial.
value(RealVector) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
value(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the value of the gravity field.
value(double, double) - Method in interface org.orekit.gnss.antenna.PhaseCenterVariationFunction
Evaluate phase center variation in one signal direction.
value(FieldOrbit<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients
Evaluate the contributions of the short period terms.
value(T) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldIntegrableFunction
value(Orbit) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients
Evaluate the contributions of the short period terms.
value(double) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.IntegrableFunction
value(FieldOrbit<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms
Evaluate the contributions of the short period terms.
value(Orbit) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
Evaluate the contributions of the short period terms.
value(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient
Compute the value of the coefficient.
value(AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Compute the value of the coefficient.
value(AbsoluteDate) - Method in interface org.orekit.time.TimeScalarFunction
Compute a function of time.
value(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScalarFunction
Compute a function of time.
value(AbsoluteDate) - Method in interface org.orekit.time.TimeVectorFunction
Compute a function of time.
value(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeVectorFunction
Compute a function of time.
value(ParameterDriver) - Method in interface org.orekit.utils.ParameterFunction
Evaluate the function.
value(SpacecraftState) - Method in interface org.orekit.utils.StateFunction
Evaluate the function.
value(SpacecraftState) - Method in interface org.orekit.utils.StateJacobian
Evaluate the Jacobian of the function.
valueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter value has been changed.
valueOf(String) - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.data.PolynomialParser.Unit
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.errors.OrekitMessages
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.estimation.measurements.EstimatedMeasurement.Status
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.estimation.measurements.generation.SignSemantic
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.estimation.measurements.gnss.CombinationType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.CenterName
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.DutyCycleType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.ElementsType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.OdMethodType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.OnOff
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.PocMethodType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.definitions.TimeSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.AdmMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParametersKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmHeaderKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.CovarianceMethod
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.Maneuvrable
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.ODParametersKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenVolumeFrame
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenVolumeShape
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.StateVectorKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.CommonMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManBasis
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ObjectType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.Ordering
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.PhysicalPropertiesKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ShadowModel
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.OdmMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.oem.InterpolationMethod
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.odm.StateVectorKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.ParsedUnitsBehavior
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.AngleType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.CorrectionApplied
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.DataQuality
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.IntegrationReference
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.RangeMode
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.RangeUnits
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.TdmDataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.TimetagReference
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.ndm.tdm.TrackingMode
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.section.HeaderKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.section.KvnStructureKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.section.MetadataKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.section.XmlStructureKey
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.utils.FileFormat
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.utils.lexical.TokenType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ilrs.CRDHeader.RangeType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.sinex.Station.ReferenceSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.sp3.SP3.SP3FileType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.sp3.SP3.SP3OrbitType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.forces.gravity.potential.TideSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.HelmertTransformation.Predefined
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.ITRFVersion
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.LOFType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.Predefined
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.antenna.SatelliteType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.clock.RinexClock.ClockDataType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.Frequency
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.MeasurementType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.Authentication
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.CarrierPhase
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.DataFormat
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.NavigationSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.RecordType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.ntrip.Type
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrDataField
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.parser.RtcmDataField
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.metric.parser.RtcmMessageType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.ObservationType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.SatelliteSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.SignalCode
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.TimeSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.models.earth.troposphere.ViennaModelType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.orbits.LibrationOrbitFamily
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.orbits.LibrationOrbitType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.orbits.OrbitType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.orbits.PositionAngle
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.propagation.events.FilterType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.propagation.events.VisibilityTrigger
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.propagation.PropagationType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.time.Month
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.utils.AngularDerivativesFilter
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.utils.CartesianDerivativesFilter
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.utils.IERSConventions
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.utils.LagrangianPoints
Returns the enum constant of this type with the specified name.
values() - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.data.PolynomialParser.Unit
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.errors.OrekitMessages
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.estimation.measurements.EstimatedMeasurement.Status
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.estimation.measurements.generation.SignSemantic
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.estimation.measurements.gnss.CombinationType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.CenterName
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.DutyCycleType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.ElementsType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.OdMethodType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.OnOff
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.PocMethodType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.definitions.TimeSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.AdmMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParametersKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmHeaderKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.CovarianceMethod
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.Maneuvrable
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.ODParametersKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenVolumeFrame
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.ScreenVolumeShape
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.StateVectorKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.CommonMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManBasis
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ObjectType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.Ordering
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.PhysicalPropertiesKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.ShadowModel
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.OdmMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.oem.InterpolationMethod
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.odm.StateVectorKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.ParsedUnitsBehavior
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.AngleType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.CorrectionApplied
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.DataQuality
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.IntegrationReference
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.RangeMode
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.RangeUnits
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.TdmDataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.TimetagReference
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.ndm.tdm.TrackingMode
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.section.HeaderKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.section.KvnStructureKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.section.MetadataKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.section.XmlStructureKey
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.utils.FileFormat
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.utils.lexical.TokenType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ilrs.CRDHeader.RangeType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.sinex.Station.ReferenceSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.sp3.SP3.SP3FileType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.sp3.SP3.SP3OrbitType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.forces.gravity.potential.TideSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.HelmertTransformation.Predefined
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.ITRFVersion
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.LOFType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.Predefined
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.antenna.SatelliteType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.clock.RinexClock.ClockDataType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.Frequency
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.MeasurementType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.ntrip.Authentication
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.ntrip.CarrierPhase
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.ntrip.DataFormat
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.ntrip.NavigationSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.ntrip.RecordType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.ntrip.Type
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.parser.IgsSsrDataField
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.parser.RtcmDataField
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.metric.parser.RtcmMessageType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.ObservationType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.SatelliteSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.SignalCode
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.TimeSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.models.earth.troposphere.ViennaModelType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.orbits.LibrationOrbitFamily
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.orbits.LibrationOrbitType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.orbits.OrbitType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.orbits.PositionAngle
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.propagation.events.FilterType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.propagation.events.VisibilityTrigger
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.propagation.PropagationType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.time.Month
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.utils.AngularDerivativesFilter
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.utils.CartesianDerivativesFilter
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.utils.IERSConventions
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.utils.LagrangianPoints
Returns an array containing the constants of this enum type, in the order they are declared.
VEL_X - Static variable in enum org.orekit.orbits.OrbitType
Name for velocity along X.
VEL_Y - Static variable in enum org.orekit.orbits.OrbitType
Name for velocity along Y.
VEL_Z - Static variable in enum org.orekit.orbits.OrbitType
Name for velocity along Z.
VENUS - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Venus.
VersionedITRF - Class in org.orekit.frames
Specific version of International Terrestrial Reference Frame.
VERTICAL_TOTAL_ELECTRON_CONTENT - Static variable in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Name of the parameter of this model: the Vertical Total Electron Content.
verticesRadius(double, int) - Method in enum org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType
Compute radius of cone going through vertices.
ViennaModelCoefficientsLoader - Class in org.orekit.models.earth.troposphere
Loads Vienna tropospheric coefficients a given input stream.
ViennaModelCoefficientsLoader(String, double, double, ViennaModelType) - Constructor for class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Constructor with supported names given by user.
ViennaModelCoefficientsLoader(String, double, double, ViennaModelType, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Constructor with supported names and source of mapping function files given by the user.
ViennaModelCoefficientsLoader(double, double, ViennaModelType) - Constructor for class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Constructor with default supported names.
ViennaModelType - Enum in org.orekit.models.earth.troposphere
Enumerate for Vienna tropospheric model 1 and 3.
ViennaOneModel - Class in org.orekit.models.earth.troposphere
The Vienna1 tropospheric delay model for radio techniques.
ViennaOneModel(double[], double[]) - Constructor for class org.orekit.models.earth.troposphere.ViennaOneModel
Build a new instance.
ViennaOneModel(double[], double[], TimeScale) - Constructor for class org.orekit.models.earth.troposphere.ViennaOneModel
Build a new instance.
ViennaThreeModel - Class in org.orekit.models.earth.troposphere
The Vienna3 tropospheric delay model for radio techniques.
ViennaThreeModel(double[], double[]) - Constructor for class org.orekit.models.earth.troposphere.ViennaThreeModel
Build a new instance.
ViennaThreeModel(double[], double[], TimeScale) - Constructor for class org.orekit.models.earth.troposphere.ViennaThreeModel
Build a new instance.
VisibilityTrigger - Enum in org.orekit.propagation.events
Enumerate for triggering visibility of spherical bodies.
VOLT - Static variable in class org.orekit.utils.units.Unit
Volt unit.

W

W_PER_KG - Static variable in class org.orekit.files.ccsds.definitions.Units
Watt per kilograms units.
wasEndTagSeen() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Check if XML end tag has been seen.
WATT - Static variable in class org.orekit.utils.units.Unit
Watt unit.
WeatherModel - Interface in org.orekit.models.earth.weather
Defines a surface meteorology model that can be used to compute the different weather parameters (pressure, temperature, ...).
weatherParameters(double, AbsoluteDate) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
 
weatherParameters(double, AbsoluteDate) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
 
weatherParameters(double, AbsoluteDate) - Method in interface org.orekit.models.earth.weather.WeatherModel
Calculates the weather parameters of the model.
WGS84_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from WGS84 model: 7.292115e-5 rad/s.
WGS84_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from WGS84 model: .
WGS84_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from WGS84 model: 6378137.0 m.
WGS84_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from WGS84 model: 1.0 / 298.257223563.
WGS84_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from WGS84 model: 3.986004418e14 m³/s².
WideLaneCombination - Class in org.orekit.estimation.measurements.gnss
Wide-Lane combination.
WindUp - Class in org.orekit.estimation.measurements.gnss
Modifier for wind-up effect in GNSS phase measurements.
WindUpFactory - Class in org.orekit.estimation.measurements.gnss
Factory for wind-up modifiers.
WindUpFactory() - Constructor for class org.orekit.estimation.measurements.gnss.WindUpFactory
Simple constructor.
withConstantElevation(double) - Method in class org.orekit.propagation.events.ElevationDetector
Setup the minimum elevation for detection.
withConstantElevation(double) - Method in class org.orekit.propagation.events.FieldElevationDetector
Setup the minimum elevation for detection.
withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Set up IERS conventions.
withDataContext(DataContext) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Set up data context used to retrieve frames, time scales, etc..
withDefaultInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Set up the default interpolation degree.
withDefaultMass(double) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Set up the default mass.
withDoodson(int, int) - Method in class org.orekit.data.PoissonSeriesParser
Set up columns for Doodson multipliers and Doodson number.
withElevationMask(ElevationMask) - Method in class org.orekit.gnss.DOPComputer
Set the elevation mask.
withElevationMask(ElevationMask) - Method in class org.orekit.propagation.events.ElevationDetector
Setup the elevation mask for detection using the passed in mask object.
withElevationMask(ElevationMask) - Method in class org.orekit.propagation.events.FieldElevationDetector
Setup the elevation mask for detection using the passed in mask object.
withFirstDelaunay(int) - Method in class org.orekit.data.PoissonSeriesParser
Set up first column of Delaunay multiplier.
withFirstPlanetary(int) - Method in class org.orekit.data.PoissonSeriesParser
Set up first column of planetary multiplier.
withFunction(Function<FieldSpacecraftState<T>, T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector
Create a new event detector with a new g function, keeping all other attributes the same.
withFunction(ToDoubleFunction<SpacecraftState>) - Method in class org.orekit.propagation.events.FunctionalDetector
Create a new event detector with a new g function, keeping all other attributes the same.
withGamma(int) - Method in class org.orekit.data.PoissonSeriesParser
Set up column of GMST tide multiplier.
withHandler(EventHandler<? super T>) - Method in class org.orekit.propagation.events.AbstractDetector
Setup the event handler to call at event occurrences.
withHandler(FieldEventHandler<? super D, T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Setup the event handler to call at event occurrences.
withMargin(double) - Method in class org.orekit.propagation.events.GeographicZoneDetector
Setup the detector margin.
withMaxCheck(double) - Method in class org.orekit.propagation.events.AbstractDetector
Setup the maximum checking interval.
withMaxCheck(T) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Setup the maximum checking interval.
withMaxIter(int) - Method in class org.orekit.propagation.events.AbstractDetector
Setup the maximum number of iterations in the event time search.
withMaxIter(int) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Setup the maximum number of iterations in the event time search.
withMinElevation(double) - Method in class org.orekit.gnss.DOPComputer
Set the minimum elevation.
withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Set up mission reference date or Mission Elapsed Time or Mission Relative Time time systems.
withMu(double) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Set up the gravitational coefficient.
withOptionalColumn(int) - Method in class org.orekit.data.PoissonSeriesParser
Set up optional column.
withParsedUnitsBehavior(ParsedUnitsBehavior) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Set up the behavior to adopt for handling parsed units.
withPenumbra() - Method in class org.orekit.propagation.events.EclipseDetector
Setup the detector to penumbra detection.
withPenumbra() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Setup the detector to penumbra detection.
withPolynomialPart(char, PolynomialParser.Unit) - Method in class org.orekit.data.PoissonSeriesParser
Set up polynomial part parsing.
withRangeUnitsConverter(RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
Set up the converter for Range Units.
withReferenceFrame(Frame) - Method in class org.orekit.attitudes.Attitude
Get a similar attitude with a specific reference frame.
withReferenceFrame(Frame) - Method in class org.orekit.attitudes.FieldAttitude
Get a similar attitude with a specific reference frame.
withRefraction(AtmosphericRefractionModel) - Method in class org.orekit.propagation.events.ElevationDetector
Setup the elevation detector to use an atmospheric refraction model in its calculations.
withRefraction(AtmosphericRefractionModel) - Method in class org.orekit.propagation.events.FieldElevationDetector
Setup the elevation detector to use an atmospheric refraction model in its calculations.
withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Set up flag for ignoring tidal effects when interpolating EOP.
withSinCos(int, int, double, int, double) - Method in class org.orekit.data.PoissonSeriesParser
Set up columns of the sine and cosine coefficients.
withSwitch(int, int) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00
Change a switch.
withThreshold(double) - Method in class org.orekit.propagation.events.AbstractDetector
Setup the convergence threshold.
withThreshold(T) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Setup the convergence threshold.
withUmbra() - Method in class org.orekit.propagation.events.EclipseDetector
Setup the detector to full umbra detection.
withUmbra() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Setup the detector to full umbra detection.
write(Appendable, AttitudeEphemerisFile<C, S>) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AttitudeWriter
Write the passed in AttitudeEphemerisFile using the passed in Appendable.
write(Appendable, EphemerisFile<C, S>) - Method in class org.orekit.files.ccsds.ndm.odm.oem.EphemerisWriter
Write the passed in EphemerisFile using the passed in Appendable.
write(Generator) - Method in class org.orekit.files.ccsds.section.AbstractWriter
Write the section, including surrounding tags.
write(Appendable, AttitudeEphemerisFile<C, S>) - Method in interface org.orekit.files.general.AttitudeEphemerisFileWriter
Write the passed in AttitudeEphemerisFile using the passed in Appendable.
write(String, AttitudeEphemerisFile<C, S>) - Method in interface org.orekit.files.general.AttitudeEphemerisFileWriter
Write the passed in AttitudeEphemerisFile to a file at the output path specified.
write(Appendable, EphemerisFile<C, S>) - Method in interface org.orekit.files.general.EphemerisFileWriter
Write the passed in EphemerisFile using the passed in Appendable.
write(String, EphemerisFile<C, S>) - Method in interface org.orekit.files.general.EphemerisFileWriter
Write the passed in EphemerisFile to a file at the output path specified.
write(Appendable, EphemerisFile<C, S>) - Method in class org.orekit.files.ilrs.CPFWriter
Write the passed in EphemerisFile using the passed in Appendable.
write(CPFHeader, Appendable, TimeScale) - Method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter
Write a line.
writeComment(Generator, String) - Method in class org.orekit.files.ccsds.ndm.NdmWriter
Write a comment line.
writeComments(List<String>) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write comment lines.
writeComments(List<String>) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
Write comment lines.
writeComments(List<String>) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Write comment lines.
writeConstituent(Generator, F) - Method in class org.orekit.files.ccsds.ndm.NdmWriter
Write a constituent.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadataWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParametersWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadataWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.ODParametersWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovarianceWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.StateVectorWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovarianceWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadataWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParametersWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.StateVectorWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.ndm.odm.UserDefinedWriter
Write the content of the section, excluding surrounding tags.
writeContent(Generator) - Method in class org.orekit.files.ccsds.section.AbstractWriter
Write the content of the section, excluding surrounding tags.
writeEndOfFile() - Method in class org.orekit.files.ilrs.StreamingCpfWriter
Write end of file.
writeEntry(String, List<String>, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write a single key/value entry.
writeEntry(String, Enum<?>, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write a single key/value entry.
writeEntry(String, TimeConverter, AbsoluteDate, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write a single key/value entry.
writeEntry(String, double, Unit, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write a single key/value entry.
writeEntry(String, Double, Unit, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write a single key/value entry.
writeEntry(String, char, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write a single key/value entry.
writeEntry(String, int, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write a single key/value entry.
writeEntry(String, String, Unit, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, List<String>, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, Enum<?>, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, TimeConverter, AbsoluteDate, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, char, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, int, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, double, Unit, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, Double, Unit, boolean) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write a single key/value entry.
writeEntry(String, String, Unit, boolean) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
Write a single key/value entry.
writeEntry(String, String, Unit, boolean) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Write a single key/value entry.
writeEphemerisLine(TimeStampedPVCoordinates) - Method in class org.orekit.files.ilrs.StreamingCpfWriter.Segment
Write ephemeris lines.
writeFooter(Generator) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Write footer for the file.
writeFooter(Generator) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Write footer for the file.
writeFooter(Generator) - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter
Write footer for the file.
writeHeader(Generator, CdmHeader) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Write header for the file.
writeHeader(Generator, H) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Write header for the file.
writeHeader(Generator, H) - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter
Write header for the file.
writeHeader() - Method in class org.orekit.files.ilrs.StreamingCpfWriter
Writes the CPF header for the file.
writeMessage(Generator, Ndm) - Method in class org.orekit.files.ccsds.ndm.NdmWriter
Write one complete message.
writeMessage(Generator, F) - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter
Write one complete message.
writeOneAttributeElement(String, String, String, String) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Write an element with one attribute.
writeRawData(char) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write raw data.
writeRawData(CharSequence) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Write raw data.
writeRawData(char) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write raw data.
writeRawData(CharSequence) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Write raw data.
WriterBuilder - Class in org.orekit.files.ccsds.ndm
Builder for all CCSDS Message files writers.
WriterBuilder() - Constructor for class org.orekit.files.ccsds.ndm.WriterBuilder
Simple constructor.
WriterBuilder(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.WriterBuilder
Simple constructor.
writeRelativeMetadataContent(Generator, double, CdmRelativeMetadata) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Write RelativeMetadata part only once after header.
writeRelativeMetadataContent(Generator, double, CdmRelativeMetadata) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmWriter
 
writeSegment(Generator, CdmSegment) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Write one segment.
writeSegment(Generator, S) - Method in class org.orekit.files.ccsds.ndm.odm.oem.EphemerisWriter
Write one segment.
writeSegment(Generator, S) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Write one segment.
writeSegment(Generator, S) - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter
Write one segment.
writeSegmentContent(Generator, double, AemSegment) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<AdmMetadata, ApmData>) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<CdmMetadata, CdmData>) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<CdmMetadata, CdmData>) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<OcmMetadata, OcmData>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, OemSegment) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<OmmMetadata, OmmData>) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<CommonMetadata, OpmData>) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, Segment<TdmMetadata, ObservationsBlock>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmWriter
Write one segment content (without XML wrapping).
writeSegmentContent(Generator, double, S) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Write one segment content (without XML wrapping).
writeTwoAttributesElement(String, String, String, String, String, String) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
Write an element with two attributes.
writeUnits(Unit) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Check if unit must be written.

X

XJ2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
XJ3 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
XJ4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
XKE - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
xl - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
L from SPTRCK #3.
xl - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
L from SPTRCK #3.
xmdot - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
common parameter for mean anomaly (M) computation.
xmdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for mean anomaly (M) computation.
XmlGenerator - Class in org.orekit.files.ccsds.utils.generation
Generator for eXtended Markup Language CCSDS messages.
XmlGenerator(Appendable, int, String, boolean) - Constructor for class org.orekit.files.ccsds.utils.generation.XmlGenerator
Simple constructor.
XmlLexicalAnalyzer - Class in org.orekit.files.ccsds.utils.lexical
Lexical analyzer for XML CCSDS messages.
XmlLexicalAnalyzer(DataSource) - Constructor for class org.orekit.files.ccsds.utils.lexical.XmlLexicalAnalyzer
Simple constructor.
XmlStructureKey - Enum in org.orekit.files.ccsds.section
Keys for FileFormat.XML format structure.
XmlStructureProcessingState - Class in org.orekit.files.ccsds.section
ProcessingState for structure of FileFormat.XML CCSDS Messages.
XmlStructureProcessingState(String, AbstractConstituentParser<?, ?>) - Constructor for class org.orekit.files.ccsds.section.XmlStructureProcessingState
Simple constructor.
XmlSubStructureKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keywords for CDM data sub-structure in XML files.
XmlTokenBuilder - Interface in org.orekit.files.ccsds.utils.lexical
Builder for building ParseToken from XML elements.
xn0dp - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
original recovered mean motion.
xn0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original recovered mean motion.
xnodcf - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
common parameter for raan (OMEGA) computation.
xnodcf - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for raan (OMEGA) computation.
xnode - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
final RAAN.
xnode - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final RAAN.
xnodot - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
common parameter for raan (OMEGA) computation.
xnodot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for raan (OMEGA) computation.

Y

YawCompensation - Class in org.orekit.attitudes
This class handles yaw compensation attitude provider.
YawCompensation(Frame, GroundPointing) - Constructor for class org.orekit.attitudes.YawCompensation
Creates a new instance.
YawSteering - Class in org.orekit.attitudes
This class handles yaw steering law.
YawSteering(Frame, GroundPointing, PVCoordinatesProvider, Vector3D) - Constructor for class org.orekit.attitudes.YawSteering
Creates a new instance.
YEAR - Static variable in class org.orekit.utils.units.Unit
Julian year unit.
yield(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.Duration
Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate
Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider
Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(SpacecraftState) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(SpacecraftState) - Method in class org.orekit.propagation.integration.AdditionalEquationsAdapter
Deprecated.
Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.integration.FieldAdditionalEquationsAdapter
Deprecated.
Check if this provider should yield so another provider has an opportunity to add missing parts.
YUMAParser - Class in org.orekit.gnss
This class reads Yuma almanac files and provides GPS almanacs.
YUMAParser(String) - Constructor for class org.orekit.gnss.YUMAParser
Simple constructor.
YUMAParser(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.gnss.YUMAParser
Create a YUMA loader/parser with the given source for YUMA auxiliary data files.

Z

ZEL - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
ZERO - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
0 represented as a polynomial.
zero() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
Reset the value to zero.
zero() - Method in class org.orekit.utils.FieldArrayDictionary.Entry
Reset the value to zero.
ZERO - Static variable in class org.orekit.utils.PVCoordinates
Fixed position/velocity at origin (both p, v and a are zero vectors).
ZES - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
zIndex(int, int) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the index of an entry in the Z transformation matrix.
ZIP_ARCHIVE_PATTERN - Static variable in interface org.orekit.data.DataProvider
Pattern for name of zip/jar archives.
ZipJarCrawler - Class in org.orekit.data
Helper class for loading data files from a zip/jar archive.
ZipJarCrawler(File) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file on filesystem.
ZipJarCrawler(String) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file in classpath.
ZipJarCrawler(ClassLoader, String) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file in classpath.
ZipJarCrawler(URL) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file on network.
ZNL - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
ZNS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
 
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