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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.
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.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.
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.
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(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.
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.
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.
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.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.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.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.
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_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.
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.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.
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.
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.
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.
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.
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.
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.
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(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.
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
Helper class to parse line data and to raise exceptions if needed.
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, with no parameter drivers.
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.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_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
Compute the derivatives related to the additional state parameters.
derivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
Compute the derivatives related to the additional state parameters.
derivatives(SpacecraftState) - Method in class org.orekit.propagation.integration.AdditionalEquationsAdapter
Deprecated.
Compute the derivatives related to the additional state parameters.
derivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
Compute the derivatives related to the additional state parameters.
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
Compute the derivatives related to the additional state parameters.
derivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Compute the derivatives related to the additional state parameters.
derivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Deprecated.
Compute the derivatives related to the additional state parameters.
derivatives(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Deprecated.
Compute the derivatives related to the additional state parameters.
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.
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.
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_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.
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.
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.
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.
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.Fi