Index (ORbit Extrapolation KIT 11.1 API)

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

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) - 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: Bridge between measurements and least squares problems.
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 C_i^j and the S_i^j 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 U_i^j and V_i^j 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 C_i^j and the S_i^j 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 U_i^j and V_i^j 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: Deprecated.
as of 11.1, replaced by AbstractMultipleShooting.AbstractMultipleShooting(List, List, double, double, int, String)
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: Deprecated.
as of 11.1, replaced by AbstractPropagatorBuilder.addAdditionalDerivativesProvider(AdditionalDerivativesProvider)
addAdditionalEquations(AdditionalEquations) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Deprecated.
as of 11.1, replaced by AbstractIntegratedPropagator.addAdditionalDerivativesProvider(AdditionalDerivativesProvider)
addAdditionalEquations(FieldAdditionalEquations<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Deprecated.
as of 11.1, replaced by FieldAbstractIntegratedPropagator.addAdditionalDerivativesProvider(FieldAdditionalDerivativesProvider)
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.
as of 11.0.1, replaced by CPF.addSatelliteCoordinate(String, CPFCoordinate)
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: Deprecated.
as of 11.1, replaced by TimeSpanMap.addValidAfter(Object, AbsoluteDate, boolean)
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: Deprecated.
as of 11.1, replaced by TimeSpanMap.addValidBefore(Object, AbsoluteDate, boolean)
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) - 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.
as of 11.1, replaced by LibrationOrbit.applyDifferentialCorrection()
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 H_f.
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: Bridge between measurements and least squares problems.
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: Deprecated.
as of 11.1, replaced by PotentialCoefficientsReader.buildFlatArray(Flattener, double)
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: Caching wrapper for NormalizedSphericalHarmonicsProvider.
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: Keys for OPM/OMM/OCM Cartesian covariance entries.
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 S_j(k, h) and the C_j(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: C_j(k, h) and S_j(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 G_s and H_s 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 G_s and H_s 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 Q_n,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 Q_n,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 V_n,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.
as of 11.1, replaced by AbstractBatchLSModel.configureHarvester(Propagator)
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: Keys for covariance history container entries.
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: Deprecated.
as of 11.1, replaced by CR3BPDifferentialCorrection.CR3BPDifferentialCorrection(PVCoordinates, CR3BPSystem, double)
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: Deprecated.
as of 11.1, replaced by CR3BPMultipleShooter.CR3BPMultipleShooter(List, List, List, double, double, int)
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: Bridge between measurements and least squares problems.
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: Deprecated.
as of 11.1, replaced by Propagator.setupMatricesComputation(String, org.hipparchus.linear.RealMatrix, org.orekit.utils.DoubleArrayDictionary)
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: Step handler picking up measurements for the SemiAnalyticalKalmanEstimator.
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: Wrap an event detector.
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: Wrap an event detector.
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 the given loader with AbstractSelfFeedingLoader.getDataProvidersManager() and AbstractSelfFeedingLoader.getSupportedNames().
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) - 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) - 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 S_j(k, h) and the C_j(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: C_j(k, h) and S_j(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 Γ^m_n,s(γ) function from equation 2.7.1-(13).
FieldGammaMnsFunction(int, T, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction: Simple constructor.
FieldGeodeticPoint<T extends CalculusFieldElement<T>> - Class in org.orekit.bodies: Point location relative to a 2D body surface, using CalculusFieldElement.
FieldGeodeticPoint(T, T, T) - Constructor for class org.orekit.bodies.FieldGeodeticPoint: Build a new instance.
FieldGHIJjsPolynomials<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities: Compute the G_js, H_js, I_js and J_js polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
FieldGHIJjsPolynomials(T, T, T, T) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Create a set of G_js, H_js, I_js and J_js polynomials.
FieldGHmsjPolynomials<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities: Compute the G_ms^j and the H_ms^j polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
FieldGHmsjPolynomials(T, T, T, T, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Create a set of G_ms^j and H_ms^j polynomials.
FieldHansenTesseralLinear<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen: Hansen coefficients K(t,n,s) for t!=0 and n < 0.
FieldHansenTesseralLinear(int, int, int, int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear: Constructor.
FieldHansenThirdBodyLinear<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen: Hansen coefficients K(t,n,s) for t=0 and n > 0.
FieldHansenThirdBodyLinear(int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear: Constructor.
FieldHansenZonalLinear<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen: Hansen coefficients K(t,n,s) for t=0 and n < 0.
FieldHansenZonalLinear(int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear: Constructor.
FieldIntegrableFunction(FieldSpacecraftState<T>, boolean, int, T[], Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldIntegrableFunction: Build a new instance with a new field.
FieldIntegratedEphemeris<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.integration: This class stores sequentially generated orbital parameters for later retrieval.
FieldIntegratedEphemeris(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldStateMapper<T>, PropagationType, FieldDenseOutputModel<T>, Map<String, T[]>, List<FieldAdditionalStateProvider<T>>, String[]) - Constructor for class org.orekit.propagation.integration.FieldIntegratedEphemeris: Deprecated.
as of 11.1, replaced by FieldIntegratedEphemeris.FieldIntegratedEphemeris(FieldAbsoluteDate, FieldAbsoluteDate, FieldAbsoluteDate, FieldStateMapper, PropagationType, FieldDenseOutputModel, FieldArrayDictionary, List, String[])
FieldIntegratedEphemeris(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldStateMapper<T>, PropagationType, FieldDenseOutputModel<T>, FieldArrayDictionary<T>, List<FieldAdditionalStateProvider<T>>, String[]) - Constructor for class org.orekit.propagation.integration.FieldIntegratedEphemeris: Creates a new instance of IntegratedEphemeris.
FieldInterpolationGrid<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.semianalytical.dsst.utilities: Interface for interpolation grids.
FieldKeplerianOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits: This class handles traditional Keplerian orbital parameters.
FieldKeplerianOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Creates a new instance.
FieldKeplerianOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Creates a new instance.
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Constructor from Cartesian parameters.
FieldKeplerianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Constructor from Cartesian parameters.
FieldKeplerianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Constructor from any kind of orbital parameters.
FieldKeplerianPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical: Simple Keplerian orbit propagator.
FieldKeplerianPropagator(FieldOrbit<T>) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator: Build a propagator from orbit only.
FieldKeplerianPropagator(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator: Build a propagator from orbit and central attraction coefficient μ.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator: Build a propagator from orbit and attitude provider.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator: Build a propagator from orbit, attitude provider and central attraction coefficient μ.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, T, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator: Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
FieldLatitudeCrossingDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Detector for geographic latitude crossing.
FieldLatitudeCrossingDetector(Field<T>, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeCrossingDetector: Build a new detector.
FieldLatitudeCrossingDetector(T, T, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeCrossingDetector: Build a detector.
FieldLegendrePolynomials<T extends CalculusFieldElement<T>> - Class in org.orekit.utils: Computes the P_nm(t) coefficients.
FieldLegendrePolynomials(int, int, T) - Constructor for class org.orekit.utils.FieldLegendrePolynomials: Create Legendre polynomials for the given degree and order.
FieldLnsCoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities: Compute the L_n^s(γ).
FieldLnsCoefficients(int, int, T[][], TreeMap<CoefficientsFactory.NSKey, Double>, T, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients: Create a set of L_n^s(γ) coefficients.
FieldManeuverTriggersResetter<T extends CalculusFieldElement<T>> - Interface in org.orekit.forces.maneuvers.trigger: Resetter for maneuver triggers.
FieldMaxGapInterpolationGrid<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities: Interpolation grid where points obey a maximum time gap.
FieldMaxGapInterpolationGrid(Field<T>, T) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldMaxGapInterpolationGrid: Constructor.
FieldNodeDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Finder for node crossing events.
FieldNodeDetector(FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector: Build a new instance.
FieldNodeDetector(T, FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector: Build a new instance.
FieldNumericalPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.numerical: This class propagates orbits using numerical integration.
FieldNumericalPropagator(Field<T>, FieldODEIntegrator<T>) - Constructor for class org.orekit.propagation.numerical.FieldNumericalPropagator: Create a new instance of NumericalPropagator, based on orbit definition mu.
FieldNumericalPropagator(Field<T>, FieldODEIntegrator<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.numerical.FieldNumericalPropagator: Create a new instance of NumericalPropagator, based on orbit definition mu.
FieldOfView - Interface in org.orekit.geometry.fov: Interface representing a spacecraft sensor Field Of View.
FieldOfViewDetector - Class in org.orekit.propagation.events: Finder for target entry/exit events with respect to a satellite sensor Field Of View.
FieldOfViewDetector(PVCoordinatesProvider, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector: Build a new instance.
FieldOfViewDetector(PVCoordinatesProvider, double, VisibilityTrigger, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector: Build a new instance.
FieldOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits: This class handles orbital parameters.
FieldOrbit(Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldOrbit: Default constructor.
FieldOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldOrbit: Set the orbit from Cartesian parameters.
FieldOrekitFixedStepHandler<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.sampling: This interface is a space-dynamics aware fixed size step handler.
FieldOrekitStepHandler<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.sampling: This interface is a space-dynamics aware step handler.
FieldOrekitStepInterpolator<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.sampling: This interface is a space-dynamics aware step interpolator.
FieldOrekitStepNormalizer<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.sampling: This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.
FieldOrekitStepNormalizer(T, FieldOrekitFixedStepHandler<T>) - Constructor for class org.orekit.propagation.sampling.FieldOrekitStepNormalizer: Simple constructor.
FieldParameterDrivenDateIntervalDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Detector for date intervals that may be offset thanks to parameter drivers.
FieldParameterDrivenDateIntervalDetector(Field<T>, String, AbsoluteDate, double) - Constructor for class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector: Build a new instance.
FieldParameterDrivenDateIntervalDetector(Field<T>, String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector: Build a new instance.
FieldPoleCorrection<T extends CalculusFieldElement<T>> - Class in org.orekit.frames: Simple container class for pole correction parameters.
FieldPoleCorrection(T, T) - Constructor for class org.orekit.frames.FieldPoleCorrection: Simple constructor.
FieldPropagator<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation: This interface provides a way to propagate an orbit at any time.
FieldPVCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils: Simple container for Position/Velocity pairs, using CalculusFieldElement.
FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Builds a FieldPVCoordinates triplet with zero acceleration.
FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Builds a FieldPVCoordinates triplet.
FieldPVCoordinates(Field<T>, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Builds a FieldPVCoordinates from a field and a regular PVCoordinates.
FieldPVCoordinates(double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Multiplicative constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Multiplicative constructor.
FieldPVCoordinates(T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Multiplicative constructor.
FieldPVCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Subtractive constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(FieldVector3D) - Constructor for class org.orekit.utils.FieldPVCoordinates: Builds a FieldPVCoordinates triplet from a FieldVector3D<FieldDerivativeStructure>.
FieldPVCoordinatesProvider<T extends CalculusFieldElement<T>> - Interface in org.orekit.utils: Interface for PV coordinates providers.
FieldRecordAndContinue<T extends FieldEventDetector<E>,E extends CalculusFieldElement<E>> - Class in org.orekit.propagation.events.handlers: Handler that will record every time an event occurs and always return Action.CONTINUE.
FieldRecordAndContinue() - Constructor for class org.orekit.propagation.events.handlers.FieldRecordAndContinue: Create a new handler using an ArrayList to store events.
FieldRecordAndContinue(List<FieldRecordAndContinue.Event<T, E>>) - Constructor for class org.orekit.propagation.events.handlers.FieldRecordAndContinue: Create a handler using the given collection to store events.
FieldRecordAndContinue.Event<T,F extends CalculusFieldElement<F>> - Class in org.orekit.propagation.events.handlers: A single event detected during propagation.
FieldSGP4<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle: This class contains methods to compute propagated coordinates with the SGP4 model.
FieldSGP4(FieldTLE<T>, AttitudeProvider, T, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldSGP4: Constructor for a unique initial TLE.
FieldSGP4(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldSGP4: Constructor for a unique initial TLE.
FieldShortPeriodicsInterpolatedCoefficient<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities: Interpolated short periodics coefficients.
FieldShortPeriodicsInterpolatedCoefficient(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient: Simple constructor.
FieldShortPeriodTerms<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.semianalytical.dsst.forces: Additive short period terms contributing to the mean to osculating orbit mapping.
FieldSpacecraftState<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation: This class is the representation of a complete state holding orbit, attitude and mass information at a given date.
FieldSpacecraftState(FieldOrbit<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit and attitude.
FieldSpacecraftState(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Create a new instance from orbit and mass.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit, attitude and mass.
FieldSpacecraftState(FieldOrbit<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Deprecated.
as of 11.1, replacezd by FieldSpacecraftState.FieldSpacecraftState(FieldOrbit, FieldArrayDictionary)
FieldSpacecraftState(FieldOrbit<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit and additional states.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Deprecated.
as of 11.1, replaced by FieldSpacecraftState.FieldSpacecraftState(FieldOrbit, FieldAttitude, FieldArrayDictionary)
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit attitude and additional states.
FieldSpacecraftState(FieldOrbit<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Deprecated.
as of 11.1, replaced by FieldSpacecraftState.FieldSpacecraftState(FieldOrbit, CalculusFieldElement, FieldArrayDictionary)
FieldSpacecraftState(FieldOrbit<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Create a new instance from orbit, mass and additional states.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Deprecated.
as of 11.1, replaced by FieldSpacecraftState.FieldSpacecraftState(FieldOrbit, FieldAttitude, CalculusFieldElement, FieldArrayDictionary)
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit, attitude, mass and additional states.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit, attitude, mass, additional states and derivatives.
FieldSpacecraftState(Field<T>, SpacecraftState) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Convert a FieldSpacecraftState.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit and attitude.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Create a new instance from orbit and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit, attitude and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Deprecated.
as of 11.1, replaced by FieldSpacecraftState.FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldArrayDictionary)
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Deprecated.
as of 11.1, replaced by FieldSpacecraftState.FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, FieldArrayDictionary)
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit and attitude.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Deprecated.
as of 11.1, replaced by FieldSpacecraftState.FieldSpacecraftState(FieldAbsolutePVCoordinates, CalculusFieldElement, FieldArrayDictionary)
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Create a new instance from orbit and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Deprecated.
as of 11.1, replaced by FieldSpacecraftState.FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, CalculusFieldElement, FieldArrayDictionary)
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit, attitude and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T, FieldArrayDictionary<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit, attitude and mass.
FieldStateMapper<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.integration: This class maps between raw double elements and FieldSpacecraftState instances.
FieldStateMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngle, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.FieldStateMapper: Simple constructor.
FieldStepHandlerMultiplexer<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.sampling: This class gathers several OrekitStepHandler instances into one.
FieldStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer: Simple constructor.
FieldStopOnDecreasing<KK extends FieldEventDetector<T>,T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers: Handle a detection event and choose what to do next.
FieldStopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnDecreasing
FieldStopOnEvent<KK extends FieldEventDetector<T>,T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers: Event handler which will always return continue as a state.
FieldStopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnEvent
FieldStopOnIncreasing<KK extends FieldEventDetector<T>,T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers: Handle a detection event and choose what to do next.
FieldStopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnIncreasing
FieldTimeDerivativesEquations<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.numerical: Interface summing up the contribution of several forces into orbit and mass derivatives.
FieldTimeInterpolable<T extends FieldTimeInterpolable<T,KK>,KK extends CalculusFieldElement<KK>> - Interface in org.orekit.time: This interface represents objects that can be interpolated in time.
FieldTimeShiftable<T extends FieldTimeInterpolable<T,KK>,KK extends CalculusFieldElement<KK>> - Interface in org.orekit.time: This interface represents objects that can be shifted in time.
FieldTimeSpanMap<T,D extends CalculusFieldElement<D>> - Class in org.orekit.utils: Container for objects that apply to spans of time.
FieldTimeSpanMap(T, Field<D>) - Constructor for class org.orekit.utils.FieldTimeSpanMap: Create a map containing a single object, initially valid throughout the timeline.
FieldTimeSpanMap.Transition<S,D extends CalculusFieldElement<D>> - Class in org.orekit.utils: Local class holding transition times.
FieldTimeStamped<T extends CalculusFieldElement<T>> - Interface in org.orekit.time: This interface represents objects that have a AbsoluteDate date attached to them.
FieldTLE<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle: This class is a container for a single set of TLE data.
FieldTLE(Field<T>, String, String) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE: Simple constructor from unparsed two lines.
FieldTLE(Field<T>, String, String, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE: Simple constructor from unparsed two lines using the given time scale as UTC.
FieldTLE(int, char, int, int, String, int, int, FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, int, double) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE: Simple constructor from already parsed elements.
FieldTLE(int, char, int, int, String, int, int, FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, int, double, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLE: Simple constructor from already parsed elements using the given time scale as UTC.
FieldTLEPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.tle: This class provides elements to propagate TLE's.
FieldTLEPropagator(FieldTLE<T>, AttitudeProvider, T, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Protected constructor for derived classes.
FieldTLEPropagator(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Protected constructor for derived classes.
FieldTransform<T extends CalculusFieldElement<T>> - Class in org.orekit.frames: Transformation class in three dimensional space.
FieldTransform(Field<T>, Transform) - Constructor for class org.orekit.frames.FieldTransform: Build a transform from a regular transform.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a translation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a translation transform, with its first time derivative.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a translation transform, with its first and second time derivatives.
FieldTransform(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a translation transform, with its first time derivative.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldAngularCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldTransform<T>, FieldTransform<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a transform by combining two existing ones.
FieldTransformGenerator<T extends CalculusFieldElement<T>> - Class in org.orekit.frames: Generator to use field transforms in GenericTimeStampedCache.
FieldTransformGenerator(Field<T>, int, TransformProvider, double) - Constructor for class org.orekit.frames.FieldTransformGenerator: simple constructor.
FIFTIES_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
FIFTIES_EPOCH - Static variable in class org.orekit.time.DateComponents: Reference epoch for 1950 dates: 1950-01-01.
FileFormat - Enum in org.orekit.files.ccsds.utils: Enumerate for file format.
FilesListCrawler - Class in org.orekit.data: Provider for data files in an explicit list.
FilesListCrawler(File...) - Constructor for class org.orekit.data.FilesListCrawler: Build a data classpath crawler.
fillHalfRow(T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit: Fill a Jacobian half row with a single vector.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a single vector.
fillHalfRow(double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHistory(IERSConventions.NutationCorrectionConverter, SortedSet<EOPEntry>) - Method in interface org.orekit.frames.EOPHistoryLoader: Load celestial body.
filter(DataSource) - Method in interface org.orekit.data.DataFilter: Filter the data source.
filter(DataSource) - Method in class org.orekit.data.GzipFilter: Filter the data source.
filter(DataSource) - Method in class org.orekit.data.UnixCompressFilter: Filter the data source.
filter(ObservedMeasurement<T>, SpacecraftState) - Method in class org.orekit.estimation.measurements.filtering.ElevationFilter: Apply a filter to an observed measurement.
filter(ObservedMeasurement<T>, SpacecraftState) - Method in interface org.orekit.estimation.measurements.filtering.MeasurementFilter: Apply a filter to an observed measurement.
filter(ObservedMeasurement<T>, SpacecraftState) - Method in class org.orekit.estimation.measurements.filtering.ResidualFilter: Apply a filter to an observed measurement.
filter(DataSource) - Method in class org.orekit.gnss.HatanakaCompressFilter: Filter the data source.
filter(boolean) - Method in class org.orekit.utils.ParameterDriversList: Filter parameters to keep only one type of selection status.
FiltersManager - Class in org.orekit.data: Manager for data filters.
FiltersManager() - Constructor for class org.orekit.data.FiltersManager: Build an empty manager.
FilterType - Enum in org.orekit.propagation.events: Enumerate for filtering events.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Finalize data after parsing.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Finalize estimation.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Finalize estimation.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Finalize header after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Finalize metadata after parsing.
finalizeMetadata(ContextBinding) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata: Finalize the metadata.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Finalize metadata after parsing.
finalizeOperationsObservationGrid() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Finalize estimation operations on the observation grid.
findByName(String) - Method in class org.orekit.utils.ParameterDriversList: Find a delegating driver by name.
findEOP(Frame) - Static method in class org.orekit.frames.FramesFactory: Retrieve EOP from a frame hierarchy.
findSatelliteAntenna(SatelliteSystem, int) - Method in class org.orekit.gnss.antenna.AntexLoader: Find the time map for a specific satellite antenna.
finish(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter: Finalize propagation.
finish(SpacecraftState) - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter: Finalize propagation.
finish(SpacecraftState) - Method in class org.orekit.files.ilrs.StreamingCpfWriter.Segment: Finalize propagation.
finish(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler: Finalize propagation.
finish(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler: Finalize propagation.
finish(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer: Finalize propagation.
finish(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer: Finalize propagation.
finish(List<SpacecraftState>) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler: Finalize propagation.
finish(SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler: Finalize propagation.
finish(SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler: Finalize propagation.
finish(SpacecraftState) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer: Finalize propagation.
finish(SpacecraftState) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer: Finalize propagation.
finished(TaskEvent) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
FiniteDifferencePropagatorConverter - Class in org.orekit.propagation.conversion: Propagator converter using finite differences to compute the Jacobian.
FiniteDifferencePropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter: Simple constructor.
fit() - Method in class org.orekit.utils.SecularAndHarmonic: Fit parameters.
FixedFrameBuilder - Class in org.orekit.attitudes: Builder that assumes angular coordinates are given in a fixed frame.
FixedFrameBuilder(Frame) - Constructor for class org.orekit.attitudes.FixedFrameBuilder: Creates new instance.
FixedNumberInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities: Interpolation grid where a fixed number of points are evenly spaced between the start and the end of the integration step.
FixedNumberInterpolationGrid(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid: Constructor.
FixedRate - Class in org.orekit.attitudes: This class handles a simple attitude provider at constant rate around a fixed axis.
FixedRate(Attitude) - Constructor for class org.orekit.attitudes.FixedRate: Creates a new instance.
FixedStepSelector - Class in org.orekit.time: Selector generating a continuous stream of dates separated by a constant step.
FixedStepSelector(double, TimeScale) - Constructor for class org.orekit.time.FixedStepSelector: Simple constructor.
FixedTransformProvider - Class in org.orekit.frames: Transform provider using fixed transform.
FixedTransformProvider(Transform) - Constructor for class org.orekit.frames.FixedTransformProvider: Simple constructor.
FixedTroposphericDelay - Class in org.orekit.models.earth.troposphere: A static tropospheric model that interpolates the actual tropospheric delay based on values read from a configuration file (tropospheric-delay.txt) via the DataProvidersManager.
FixedTroposphericDelay(double[], double[], double[][]) - Constructor for class org.orekit.models.earth.troposphere.FixedTroposphericDelay: Creates a new FixedTroposphericDelay instance.
FixedTroposphericDelay(String) - Constructor for class org.orekit.models.earth.troposphere.FixedTroposphericDelay: Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the default data context.
FixedTroposphericDelay(String, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.FixedTroposphericDelay: Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the specified data manager.
fixIntegerAmbiguities(int, List<ParameterDriver>, RealMatrix) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver: Fix integer ambiguities.
FLOW_RATE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Parameter name for flow rate.
FLOW_RATE_SCALE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Flow rate scaling factor.
FootprintOverlapDetector - Class in org.orekit.propagation.events: Detector triggered by geographical region entering/leaving a spacecraft sensor Field Of View.
FootprintOverlapDetector(FieldOfView, OneAxisEllipsoid, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.FootprintOverlapDetector: Build a new instance.
ForceModel - Interface in org.orekit.forces: This interface represents a force modifying spacecraft motion.
ForceModelContext - Class in org.orekit.propagation.semianalytical.dsst.forces: Base class for dsst force models attributes containers.
ForceModelContext(AuxiliaryElements) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.ForceModelContext: Simple constructor.
forEach(Consumer<T>) - Method in class org.orekit.utils.TimeSpanMap: Performs an action for each non-null element of map.
format(double) - Static method in class org.orekit.utils.AccurateFormatter: Format a double number.
format(int, int, int, int, int, double) - Static method in class org.orekit.utils.AccurateFormatter: Format a date.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.Aem: Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.Apm: Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm: Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.Oem: Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.Omm: Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.tdm.Tdm: Key for format version.
formatUtcOffset() - Method in class org.orekit.time.TimeComponents: Get the UTC offset as a string in ISO8601 format.
Frame - Class in org.orekit.frames: Tridimensional references frames class.
Frame(Frame, Transform, String) - Constructor for class org.orekit.frames.Frame: Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, TransformProvider, String) - Constructor for class org.orekit.frames.Frame: Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.Frame: Build a frame from its transform with respect to its parent.
Frame(Frame, TransformProvider, String, boolean) - Constructor for class org.orekit.frames.Frame: Build a frame from its transform with respect to its parent.
FrameAncestorException - Exception in org.orekit.errors: This class is the base class for exception thrown by the UpdatableFrame.updateTransform method.
FrameAncestorException(Localizable, Object...) - Constructor for exception org.orekit.errors.FrameAncestorException: Simple constructor.
FrameFacade - Class in org.orekit.files.ccsds.definitions: Facade in front of several frames types in CCSDS messages.
FrameFacade(Frame, CelestialBodyFrame, OrbitRelativeFrame, SpacecraftBodyFrame, String) - Constructor for class org.orekit.files.ccsds.definitions.FrameFacade: Simple constructor.
Frames - Interface in org.orekit.frames: A collection of commonly used Frames.
FramesFactory - Class in org.orekit.frames: Factory for predefined reference frames.
freeze() - Method in class org.orekit.frames.FieldTransform: Get a frozen transform.
freeze() - Method in class org.orekit.frames.Transform: Get a frozen transform.
freezeColumnsNames() - Method in class org.orekit.propagation.AbstractMatricesHarvester: Freeze the names of the Jacobian columns.
freezeColumnsNames() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester: Freeze the names of the Jacobian columns.
freezeColumnsNames() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester: Freeze the names of the Jacobian columns.
Frequency - Enum in org.orekit.gnss: Enumerate for GNSS frequencies.
FrequencyPattern - Class in org.orekit.gnss.antenna: Pattern for GNSS antenna model on one frequency.
FrequencyPattern(Vector3D, PhaseCenterVariationFunction) - Constructor for class org.orekit.gnss.antenna.FrequencyPattern: Simple constructor.
fromSeconds(int, double, double, int) - Static method in class org.orekit.time.TimeComponents: Build a time from the second number within the day.
fromSI(double) - Method in class org.orekit.utils.units.Unit: Convert a value from SI units.
fromSI(Double) - Method in class org.orekit.utils.units.Unit: Convert a value from SI units.
FunctionalDetector - Class in org.orekit.propagation.events: A detector that implements the FunctionalDetector.g(SpacecraftState) function using a lambda that can be set using FunctionalDetector.withFunction(ToDoubleFunction).
FunctionalDetector() - Constructor for class org.orekit.propagation.events.FunctionalDetector: Create an event detector with the default values.
FundamentalNutationArguments - Class in org.orekit.data: Class computing the fundamental arguments for nutation and tides.
FundamentalNutationArguments(IERSConventions, TimeScale, InputStream, String) - Constructor for class org.orekit.data.FundamentalNutationArguments: Build a model of fundamental arguments from an IERS table file.
FundamentalNutationArguments(IERSConventions, TimeScale, InputStream, String, TimeScales) - Constructor for class org.orekit.data.FundamentalNutationArguments: Build a model of fundamental arguments from an IERS table file.
FundamentalNutationArguments(IERSConventions, TimeScale, List<double[]>) - Constructor for class org.orekit.data.FundamentalNutationArguments: Build a model of fundamental arguments from an IERS table file.
FundamentalNutationArguments(IERSConventions, TimeScale, List<double[]>, TimeScales) - Constructor for class org.orekit.data.FundamentalNutationArguments: Build a model of fundamental arguments from an IERS table file.
FUTURE_INFINITY - Static variable in class org.orekit.time.AbsoluteDate: Dummy date at infinity in the future direction.

G

g(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AdapterDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AlignmentDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AltitudeDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AngularSeparationDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ApsideDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.BooleanDetector
g(SpacecraftState) - Method in class org.orekit.propagation.events.DateDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EclipseDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector: Compute the value of the detection function.
g(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventShifter: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventSlopeFilter: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldApsideDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldDateDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector: Compute the value of the detection function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FieldOfViewDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FootprintOverlapDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FunctionalDetector
g(SpacecraftState) - Method in class org.orekit.propagation.events.GeographicZoneDetector: Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundAtNightDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.HaloXZPlaneCrossingDetector: Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector: Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector: Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector: Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector: Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.MagneticFieldDetector: Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.NegateDetector
g(SpacecraftState) - Method in class org.orekit.propagation.events.NodeDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.PositionAngleDetector: Compute the value of the detection function.
G0_STANDARD_GRAVITY - Static variable in interface org.orekit.utils.Constants: Standard gravity constant, used in maneuvers definition: 9.80665 m/s².
Galileo - Class in org.orekit.gnss.attitude: Attitude providers for Galileo navigation satellites.
Galileo(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Galileo: Simple constructor.
GALILEO_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants: Value of the earth's rotation rate in rad/s for Galileo user.
GALILEO_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.
GALILEO_EPOCH - Static variable in class org.orekit.time.DateComponents: Reference epoch for Galileo System Time: 1999-08-22.
GALILEO_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants: Earth's universal gravitational parameter for Galileo user in m³/s².
GALILEO_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants: Number of weeks in the Galileo cycle.
GalileoAlmanac - Class in org.orekit.propagation.analytical.gnss.data: Class for Galileo almanac.
GalileoAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac: Build a new almanac.
GalileoNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a Galileo navigation message.
GalileoNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Constructor.
GalileoScale - Class in org.orekit.time: Galileo system time scale.
GammaMnsFunction - Class in org.orekit.propagation.semianalytical.dsst.utilities: Compute the Γ^m_n,s(γ) function from equation 2.7.1-(13).
GammaMnsFunction(int, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction: Simple constructor.
generate(List<OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.ContinuousScheduler: Generate a sequence of measurements.
generate(List<OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.EventBasedScheduler: Generate a sequence of measurements.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.Generator: Generate measurements.
generate(List<OrekitStepInterpolator>) - Method in interface org.orekit.estimation.measurements.generation.Scheduler: Generate a sequence of measurements.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.FieldTransformGenerator: Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.TransformGenerator: Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedGenerator: Generate a chronologically sorted list of entries to be cached.
generateCartesianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Generate a Cartesian orbit.
generateException(Exception) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Generate a parse exception for this entry.
generateKeplerianOrbit(Frame) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Generate a keplerian orbit.
generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm: Generate a keplerian orbit.
generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Generate a keplerian orbit.
generateSpacecraftState() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm: Generate spacecraft state from the CartesianOrbit generated by generateCartesianOrbit.
generateSpacecraftState() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Generate spacecraft state from the CartesianOrbit generated by generateCartesianOrbit.
generateTLE() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm: Generate TLE from OMM file.
Generator - Class in org.orekit.estimation.measurements.generation: Main generator for observed measurements.
Generator() - Constructor for class org.orekit.estimation.measurements.generation.Generator: Build a generator with no sequences generator.
Generator - Interface in org.orekit.files.ccsds.utils.generation: Generation interface for CCSDS messages.
GenericGNSS - Class in org.orekit.gnss.attitude: Attitude providers for navigation satellites for which no specialized model is known.
GenericGNSS(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GenericGNSS: Simple constructor.
GenericTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils: Generic thread-safe cache for time-stamped data.
GenericTimeStampedCache(int, int, double, double, TimeStampedGenerator<T>) - Constructor for class org.orekit.utils.GenericTimeStampedCache: Simple constructor.
GeodeticPoint - Class in org.orekit.bodies: Point location relative to a 2D body surface.
GeodeticPoint(double, double, double) - Constructor for class org.orekit.bodies.GeodeticPoint: Build a new instance.
GeographicZoneDetector - Class in org.orekit.propagation.events: Detector for entry/exit of a zone defined by geographic boundaries.
GeographicZoneDetector(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector: Build a new detector.
GeographicZoneDetector(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector: Build a detector.
Geoid - Class in org.orekit.models.earth: A geoid is a level surface of the gravity potential of a body.
Geoid(NormalizedSphericalHarmonicsProvider, ReferenceEllipsoid) - Constructor for class org.orekit.models.earth.Geoid: Creates a geoid from the given geopotential, reference ellipsoid and the assumptions in the comment for Geoid.
GeoMagneticElements - Class in org.orekit.models.earth: Contains the elements to represent a magnetic field at a single point.
GeoMagneticElements(Vector3D) - Constructor for class org.orekit.models.earth.GeoMagneticElements: Construct a new element with the given field vector.
GeoMagneticField - Class in org.orekit.models.earth: Used to calculate the geomagnetic field at a given geodetic point on earth.
GeoMagneticField(String, double, int, int, double, double) - Constructor for class org.orekit.models.earth.GeoMagneticField: Create a new geomagnetic field model with the given parameters.
GeoMagneticFieldFactory - Class in org.orekit.models.earth: Factory for different GeoMagneticField models.
GeoMagneticFieldFactory.FieldModel - Enum in org.orekit.models.earth: The currently supported geomagnetic field models.
GeoMagneticFields - Interface in org.orekit.models.earth: Methods for obtaining geomagnetic fields.
GeoMagneticModelLoader - Class in org.orekit.models.earth: Loads geomagnetic field models from a given input stream.
GeoMagneticModelLoader() - Constructor for class org.orekit.models.earth.GeoMagneticModelLoader
GeometryFreeCombination - Class in org.orekit.estimation.measurements.gnss: Geometry-free combination.
GeometryFreeCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss: Geometry free cycle slip detectors.
GeometryFreeCycleSlipDetector(double, double, int) - Constructor for class org.orekit.estimation.measurements.gnss.GeometryFreeCycleSlipDetector: Constructor.
get(String) - Method in class org.orekit.utils.DoubleArrayDictionary: Get the value corresponding to a key.
get(String) - Method in class org.orekit.utils.FieldArrayDictionary: Get the value corresponding to a key.
get(FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap: Get the entry valid at a specified date.
get(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap: Get the entry valid at a specified date.
get24HoursKp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Get the last 24H mean geomagnetic index.
get24HoursKp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: The Kp index is derived from the Ap index.
get24HoursKp(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters: Get the last 24H mean geomagnetic index.
getA() - Method in class org.orekit.bodies.Ellipse: Get the semi major axis.
getA() - Method in class org.orekit.bodies.Ellipsoid: Get the length of the first semi-axis.
getA() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Get the orbit semi-major axis.
getA() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader: Returns the a coefficients array.
getA() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model: Returns the a coefficients array.
getA() - Method in class org.orekit.orbits.CartesianOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.CircularOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.KeplerianOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.Orbit: Get the semi-major axis.
getA() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the semi-major axis.
getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext: Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.SpacecraftState: Get the semi-major axis.
getAbscissaGrid() - Method in class org.orekit.utils.InterpolationTableLoader: Returns a copy of the abscissa grid for the interpolation function.
getAbsoluteDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition: Get the transition field absolute date.
getAbsPVA() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the absolute position-velocity-acceleration.
getAbsPVA() - Method in class org.orekit.propagation.SpacecraftState: Get the absolute position-velocity-acceleration.
getAcceleration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get acceleration.
getAcceleration(SpacecraftState, Attitude, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel: Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration(FieldSpacecraftState<T>, FieldAttitude<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel: Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration(SpacecraftState, Attitude, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration(FieldSpacecraftState<T>, FieldAttitude<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration() - Method in class org.orekit.frames.FieldTransform: Get the second time derivative of the translation.
getAcceleration() - Method in class org.orekit.frames.Transform: Get the second time derivative of the translation.
getAcceleration() - Method in class org.orekit.utils.FieldPVCoordinates: Gets the acceleration.
getAcceleration() - Method in class org.orekit.utils.PVCoordinates: Gets the acceleration.
getAccelerationDirectionSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get one σ angular off-nominal acceleration direction.
getAccelerationInterpolation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get interpolation mode between current and next acceleration line.
getAccelerationMagnitudeSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get one σ percent error on acceleration magnitude.
getAccelerationModel(AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration: Get the AccelerationModel model valid at a date.
getAccelerationModelSpan(AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration: Get the AccelerationModel TimeSpanMap.Span containing a specified date.
getAccuracy(int) - Method in class org.orekit.files.sp3.SP3: Get the formal accuracy for a satellite.
getAccuracy() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris: Get the formal accuracy for this satellite.
getAccuracy() - Method in interface org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.AccuracyProvider: Get the accuracy of the ephemeris data from an accuracy index.
getAccuracy() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.GlonassUserRangeAccuracy: Get the accuracy of the ephemeris data from an accuracy index.
getAccuracy() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.SignalInSpaceAccuracy: Get the accuracy of the ephemeris data from an accuracy index.
getAccuracy() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.UserRangeAccuracy: Get the accuracy of the ephemeris data from an accuracy index.
getAccuracyProvider() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData: Get the accuracy provider of the ephemeris message.
getAction() - Method in class org.orekit.propagation.events.EventState.EventOccurrence: Get the user requested action.
getAction() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence: Get the user requested action.
getActualOdSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get actual time span used for the OD of the object.
getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the adapted propagator.
getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the list of additional equations.
getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get an unmodifiable list of providers for additional derivatives.
getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get an unmodifiable list of providers for additional derivatives.
getAdditionalEquations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Deprecated.
as of 11.1, replaced by AbstractPropagatorBuilder.addAdditionalDerivativesProvider(AdditionalDerivativesProvider)
getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.Duration: Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate: Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate: Get the additional state.
getAdditionalState(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider: Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider: Get the additional state.
getAdditionalState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider: Get the additional state.
getAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState: Get an additional state.
getAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState: Get an additional state.
getAdditionalStateDerivative(String) - Method in class org.orekit.propagation.FieldSpacecraftState: Get an additional state derivative.
getAdditionalStateDerivative(String) - Method in class org.orekit.propagation.SpacecraftState: Get an additional state derivative.
getAdditionalStateDimension() - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper: Compute the length of the one-dimensional additional state array needed.
getAdditionalStateProviders() - Method in class org.orekit.propagation.AbstractPropagator: Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in interface org.orekit.propagation.FieldPropagator: Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in interface org.orekit.propagation.Propagator: Get an unmodifiable list of providers for additional state.
getAdditionalStates() - Method in class org.orekit.propagation.FieldSpacecraftState: Deprecated.
as of 11.1, replaced by FieldSpacecraftState.getAdditionalStatesValues()
getAdditionalStates() - Method in class org.orekit.propagation.SpacecraftState: Deprecated.
as of 11.1, replaced by SpacecraftState.getAdditionalStatesValues()
getAdditionalStatesDerivatives() - Method in class org.orekit.propagation.FieldSpacecraftState: Get an unmodifiable map of additional states derivatives.
getAdditionalStatesDerivatives() - Method in class org.orekit.propagation.SpacecraftState: Get an unmodifiable map of additional states derivatives.
getAdditionalStatesValues() - Method in class org.orekit.propagation.FieldSpacecraftState: Get an unmodifiable map of additional states.
getAdditionalStatesValues() - Method in class org.orekit.propagation.SpacecraftState: Get an unmodifiable map of additional states.
getAdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the Unique identifier of Attitude Data Message linked to this Orbit Data Message.
getADot() - Method in class org.orekit.orbits.CartesianOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.CircularOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.Orbit: Get the semi-major axis derivative.
getAe() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the value of the central body reference radius.
getAe() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the central body reference radius.
getAe() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Get the value of the central body reference radius.
getAf0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the the SV Clock Bias Correction Coefficient.
getAf0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements: Gets the Zeroth Order Clock Correction.
getAf1() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the SV Clock Drift Correction Coefficient.
getAf1() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements: Gets the First Order Clock Correction.
getAf2() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac: Getter for the Drift Rate Correction Coefficient.
getAf2() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Getter for the Drift Rate Correction Coefficient.
getAf2() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements: Gets the Second Order Clock Correction.
getAfter() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition: Get the entry valid after transition.
getAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition: Get the entry valid after transition.
getAgency() - Method in class org.orekit.files.sp3.SP3: Returns the agency that prepared this SP3 file.
getAgencyName() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the agency name.
getAgencyName() - Method in class org.orekit.gnss.navigation.RinexNavigation: Getter for the agency name.
getAgencyName() - Method in class org.orekit.gnss.RinexObservationHeader: Get name of the agency.
getAGf0() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Gets the Zeroth Order Clock Correction.
getAGf0() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Gets the Zeroth Order Clock Correction.
getAGf1() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Gets the First Order Clock Correction.
getAGf1() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Gets the First Order Clock Correction.
getAlbedoGridSize() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get albedo grid size.
getAlbedoModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get albedo model.
getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector: Get the alignment angle (rad).
getAll() - Method in class org.orekit.utils.ImmutableTimeStampedCache: Get all of the data in this cache.
getAllAmbiguityDrivers() - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver: Get all the ambiguity parameters drivers.
getAllForceModels() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder: Get the list of all force models.
getAllForceModels() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Get the list of all force models.
getAllForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Get all the force models, perturbing forces and Newtonian attraction included.
getAllForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator: Get all the force models, perturbing forces and Newtonian attraction included.
getAllForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Get all the force models, perturbing forces and Newtonian attraction included.
getAllForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Get all the force models, perturbing forces and Newtonian attraction included.
getAlmanacs() - Method in class org.orekit.gnss.SEMParser: Gets all the GPS almanacs read from the file.
getAlmanacs() - Method in class org.orekit.gnss.YUMAParser: Gets all the GPS almanacs read from the file.
getAlpha() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader: Returns the alpha coefficients array.
getAlpha(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit: Get the latitude argument.
getAlpha(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit: Get the latitude argument.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get direction cosine α for central body.
getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit: Get the latitude argument derivative.
getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit: Get the latitude argument derivative.
getAlphaE() - Method in class org.orekit.orbits.CircularOrbit: Get the eccentric latitude argument.
getAlphaE() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the eccentric latitude argument.
getAlphaEDot() - Method in class org.orekit.orbits.CircularOrbit: Get the eccentric latitude argument derivative.
getAlphaEDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the eccentric latitude argument derivative.
getAlphaM() - Method in class org.orekit.orbits.CircularOrbit: Get the mean latitude argument.
getAlphaM() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the mean latitude argument.
getAlphaMDot() - Method in class org.orekit.orbits.CircularOrbit: Get the mean latitude argument derivative.
getAlphaMDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the mean latitude argument derivative.
getAlphaV() - Method in class org.orekit.orbits.CircularOrbit: Get the true latitude argument.
getAlphaV() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the true latitude argument.
getAlphaVDot() - Method in class org.orekit.orbits.CircularOrbit: Get the true latitude argument derivative.
getAlphaVDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the true latitude argument derivative.
getAlternateNames() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the alternate names for this space object.
getAltitude() - Method in class org.orekit.bodies.FieldGeodeticPoint: Get the altitude.
getAltitude() - Method in class org.orekit.bodies.GeodeticPoint: Get the altitude.
getAltitude() - Method in class org.orekit.propagation.events.AltitudeDetector: Get the threshold altitude value.
getAltitude() - Method in class org.orekit.propagation.events.FieldAltitudeDetector: Get the threshold altitude value.
getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase: Get the driver for phase ambiguity.
getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase: Get the driver for phase ambiguity.
getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.Phase: Get the driver for phase ambiguity.
getAmplifierBandwidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the amplifier bandwidth.
getAmplifierGain() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the amplifier gain.
getAmplifierInUse() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the amplifier in use.
getAnalysisCenterID() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the analysis center ID.
getAnalysisCenterName() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the analysis center name.
getAncestor(int) - Method in class org.orekit.frames.Frame: Get the n^th ancestor of the frame.
getAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector: Get the fixed angle to be crossed (radians).
getAngle() - Method in class org.orekit.utils.units.Unit: Get the angle exponent.
getAnglesData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the angles data for the data block.
getAngleType() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for angleType.
getAngular() - Method in class org.orekit.frames.FieldTransform: Get the underlying elementary angular part.
getAngular() - Method in class org.orekit.frames.Transform: Get the underlying elementary angular part.
getAngularCoordinates() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemData: Get an unmodifiable view of the data points.
getAngularCoordinates() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment: Get an unmodifiable list of attitude data lines.
getAngularCoordinates() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment: Get an unmodifiable list of attitude data lines.
getAngularCoordinates() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment: Get an unmodifiable list of attitude data lines.
getAngularDerivativesFilter() - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType: Get the angular derivative filter corresponding to the attitude data.
getAngularVelocity() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the mean angular velocity of the Earth for the GNSS model.
getAngularVelocity() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the mean angular velocity of the Earth of the GNSS model.
getAngularVelocity() - Method in class org.orekit.utils.FieldPVCoordinates: Get the angular velocity (spin) of this point as seen from the origin.
getAngularVelocity() - Method in class org.orekit.utils.PVCoordinates: Get the angular velocity (spin) of this point as seen from the origin.
getAnomaly() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Get the orbit anomaly.
getAnomaly(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the anomaly.
getAnomaly(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit: Get the anomaly.
getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the anomaly derivative.
getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit: Get the anomaly derivative.
getAnomalyType() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Get the type of anomaly (true or mean).
getAntennaAzimuth() - Method in class org.orekit.gnss.RinexObservationHeader: Get the azimuth of the zero direction of a fixed antenna.
getAntennaBSight() - Method in class org.orekit.gnss.RinexObservationHeader: Get the antenna B.Sight.
getAntennaHeight() - Method in class org.orekit.gnss.RinexObservationHeader: Get the antenna height.
getAntennaNumber() - Method in class org.orekit.gnss.RinexObservationHeader: Get the number of the antenna.
getAntennaPhaseCenter() - Method in class org.orekit.gnss.RinexObservationHeader: Get the antenna phasecenter.
getAntennaReferencePoint() - Method in class org.orekit.gnss.RinexObservationHeader: Get the position of antenna reference point for antenna on vehicle.
getAntennaType() - Method in class org.orekit.gnss.RinexObservationHeader: Get the type of the antenna.
getAntennaZeroDirection() - Method in class org.orekit.gnss.RinexObservationHeader: Get the zero direction of antenna.
getAODC() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage: Getter for the Age Of Data Clock (AODC).
getAODE() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage: Getter for the Age Of Data Ephemeris (AODE).
getAoR3Pow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get the value of a / R3 up to power maxAR3Pow.
getAoR3Pow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get the value of a / R3 up to power maxAR3Pow.
getAp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Get the A_p geomagnetic indices.
getAp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: Get the A_p geomagnetic indices.
getAp(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters: Get the A_p geomagnetic indices.
getApAvg() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the arithmetic average of all eight Ap indices for the current entry.
getApplicableWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the applicable wavelength.
getAppliedVoltage() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the applied voltage.
getApproxPos() - Method in class org.orekit.gnss.RinexObservationHeader: Get the Approximate Marker Position.
getArbitraryEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Get an arbitrary date.
getArea() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet: Get facet area.
getAstronomicalAmplitudesMap() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader: Get astronomical amplitudes map.
getAtmosphere() - Method in class org.orekit.forces.drag.DragForce: Get the atmospheric model.
getAtmosphere() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the atmospheric model.
getAtmosphericModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get name of atmospheric model.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AttitudesSequence: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FixedRate: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.InertialProvider: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.InertialProvider: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffset: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.SpinStabilized: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedProvider: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedProvider: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the attitude corresponding to an orbital state.
getAttitude(Frame, PVCoordinatesProvider) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm: Get the attitude.
getAttitude(Frame, PVCoordinatesProvider) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion: Get the attitude.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider: Compute the attitude corresponding to an orbital state.
getAttitude() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the attitude.
getAttitude() - Method in class org.orekit.propagation.SpacecraftState: Get the attitude.
getAttitudeActuatorType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the type of actuator for attitude control.
getAttitudeControlAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the accuracy of attitude control.
getAttitudeControlMode() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the attitude control mode.
getAttitudeFromFrame(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider: Compute the attitude for DIRECTION_IN_FRAME or DIRECTION_IN_LOF types.
getAttitudeKnowledgeAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the accuracy of attitude knowledge.
getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Get the Attitude Provider to use during maneuver.
getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.Maneuver: Get the attitude override used for the maneuver.
getAttitudePointingAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the overall accuracy of spacecraft to maintain attitude.
getAttitudeProvider() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment: Get the attitude provider for this attitude ephemeris segment.
getAttitudeProvider() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment: Get the attitude provider for this attitude ephemeris segment.
getAttitudeProvider() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris: Get the attitude provider corresponding to this ephemeris, combining data from all segments.
getAttitudeProvider() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment: Get the attitude provider for this attitude ephemeris segment.
getAttitudeProvider() - Method in class org.orekit.propagation.AbstractPropagator: Get attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get attitude provider.
getAttitudeProvider() - Method in interface org.orekit.propagation.FieldPropagator: Get attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.integration.FieldStateMapper: Get the attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.integration.StateMapper: Get the attitude provider.
getAttitudeProvider() - Method in interface org.orekit.propagation.Propagator: Get attitude provider.
getAttitudeType() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get the format of the data lines in the message.
getAugmentedInitialState(int) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter: Compute the additional state from the additionalEquations.
getAugmentedInitialState(SpacecraftState, AdditionalEquations) - Method in class org.orekit.utils.AbstractMultipleShooting: Deprecated.
as of 11.1, replaced by AbstractMultipleShooting.getAugmentedInitialState(int)
getAugmentedInitialState(int) - Method in class org.orekit.utils.AbstractMultipleShooting: Compute the additional state from the additionalEquations.
getAugmentedInitialState(int) - Method in class org.orekit.utils.MultipleShooter: Compute the additional state from the additionalEquations.
getAuthentication(String) - Static method in enum org.orekit.gnss.metric.ntrip.Authentication: Get the authentication type corresponding to a keyword.
getAuthentication() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the authentication method.
getAuthentication() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord: Get the authentication method.
getAuxiliaryElements() - Method in class org.orekit.propagation.semianalytical.dsst.forces.ForceModelContext: Method to get the auxiliary elements related to the ForceModelContext.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment: Get which derivatives of angular data are available in this attitude ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState: Get which derivatives of position are available in this state.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory: Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData: Get the derivatives available in the block.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment: Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment: Get which derivatives of angular data are available in this attitude ephemeris segment.
getAvailableDerivatives() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment: Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment: Get which derivatives of angular data are available in this attitude ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment: Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris: Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
getAverageFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Get the value of the 81 day average of F10.7 solar flux centered on current day.
getAverageFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: Get the value of the 81 day average of F10.7 solar flux centered on current day.
getAverageFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters: Get the value of the 81 day average of F10.7 solar flux centered on current day.
getAx2oA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get ax2oA = 2 * a / A .
getAx2oA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get ax2oA = 2 * a / A .
getAzimuth() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement: Get the azimuth angle.
getAzimuth(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame: Get the azimuth of a point with regards to the topocentric frame center point.
getAzimuth(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame: Get the azimuth of a point with regards to the topocentric frame center point.
getAzimuthRate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement: Get the azimuth rate.
getB() - Method in class org.orekit.bodies.Ellipse: Get the semi minor axis.
getB() - Method in class org.orekit.bodies.Ellipsoid: Get the length of the second semi-axis.
getb() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get b = 1 / (1 + sqrt(1 - e²)) = 1 / (1 + B).
getb() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get b = 1 / (1 + sqrt(1 - e²)) = 1 / (1 + B).
getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get B = sqrt(1 - e²).
getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get B = sqrt(1 - e²).
getB1() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester: Get the Jacobian matrix B1 (B1 = ∂εη/∂Y).
getB2(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester: Get the Jacobian matrix B2 (B2 = ∂Y/∂Y₀).
getB3(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester: Get the Jacobian matrix B3 (B3 = ∂Y/∂P).
getB4() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester: Get the Jacobian matrix B4 (B4 = ∂εη/∂c).
getBase() - Method in class org.orekit.utils.units.PowerTerm: Get the base term.
getBaseDate() - Method in class org.orekit.utils.DateDriver: Get the base (unshifted) date.
getBaseEquipment() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame: Get the quipment on which the frame is located.
getBaseFrame() - Method in class org.orekit.estimation.measurements.GroundStation: Get the base frame associated with the station.
getBaseName(T) - Method in class org.orekit.data.AbstractListCrawler: Get the base name of an input.
getBaseName(File) - Method in class org.orekit.data.FilesListCrawler: Get the base name of an input.
getBaseName(URL) - Method in class org.orekit.data.NetworkCrawler: Get the base name of an input.
getBaseProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get a time-independent provider containing base harmonics coefficients.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the base system state at given date, without compensation.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the base system state at given date, without compensation.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the base system state at given date, without compensation.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the base system state at given date, without compensation.
getBaseWeight() - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Get the base weight associated with the measurement
getBaseWeight() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder: Get the base weight associated with the measurement
getBaseWeight() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Get the base weight associated with the measurement
getBasicDimension() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get state vector dimension without additional parameters.
getBasicDimension() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get state vector dimension without additional parameters.
getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get B².
getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get B * B.
getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get B².
getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get B * B.
getBBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get B³.
getBBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get B³.
getBDT() - Method in class org.orekit.time.LazyLoadedTimeScales
getBDT() - Method in interface org.orekit.time.TimeScales: Get the BeiDou Navigation Satellite System time scale.
getBDT() - Static method in class org.orekit.time.TimeScalesFactory: Get the BeiDou Navigation Satellite System time scale.
getBeacon() - Method in class org.orekit.propagation.events.AngularSeparationDetector: Get the beacon at the center of the proximity zone.
getBeamDivergence() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Get the beam divergence.
getBefore() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition: Get the entry valid before transition.
getBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition: Get the entry valid before transition.
getBeginDate(Frequency) - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults: Return the date of validity beginning of the detector.
getBeidouEpoch() - Method in class org.orekit.time.AbstractTimeScales
getBeidouEpoch() - Method in interface org.orekit.time.TimeScales: Reference epoch for BeiDou weeks: 2006-01-01T00:00:00 UTC.
getBeidouNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data: Get the Beidou navigation message corresponding to the current RTCM data.
getBeidouNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data: Get the Beidou navigation message corresponding to the current RTCM data.
getBeidouNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation: Get all the Beidou navigation messages contained in the file.
getBeidouNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation: Get the Beidou navigation messages for the given satellite Id.
getBeidouToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data: Get the Beidou time of clock.
getBeta() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader: Returns the beta coefficients array.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get direction cosine β for central body.
getBGDE1E5a() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Getter for the E1/E5a broadcast group delay.
getBGDE5bE1() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Getter for the the Broadcast Group Delay E5b/E1.
getBitRate() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the bit rate.
getBN() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS B_n Word.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get B / A.
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get BoABpo = B / A(1 + B).
getBody(String) - Method in interface org.orekit.bodies.CelestialBodies: Get a celestial body.
getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory: Get a celestial body.
getBody(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies: Get a celestial body.
getBody() - Method in class org.orekit.files.ccsds.definitions.BodyFacade: Get the celestial body.
getBody() - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.FootprintOverlapDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.GeographicZoneDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeExtremumDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeExtremumDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Get third body.
getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing: Get the body frame.
getBodyFrame() - Method in interface org.orekit.bodies.BodyShape: Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid: Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.models.earth.Geoid
getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody: Get a body oriented, body centered frame.
getBodyShape() - Method in class org.orekit.propagation.events.AltitudeDetector: Get the body shape.
getBodyShape() - Method in class org.orekit.propagation.events.FieldAltitudeDetector: Get the body shape.
getBolDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the total ΔV capability at beginning of life.
getBStar() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Get the SGP/SGP4 drag-like coefficient.
getBStar() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the ballistic coefficient.
getBStar() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the ballistic coefficient.
getBuilder() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler: Get the measurements builder.
getBuilders() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Getter for the propagators.
getBusModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the bus model name.
getC() - Method in class org.orekit.bodies.Ellipsoid: Get the length of the third semi-axis.
getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get C = 1 + p² + q².
getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get C = 1 + p² + q².
getC2n0(int) - Method in class org.orekit.models.earth.ReferenceEllipsoid: Get the fully normalized coefficient C_2n,0 for the normal gravity potential.
getCacheSlotsNumber() - Static method in class org.orekit.utils.OrekitConfiguration: Get the number of slots to use in caches.
getCalendarWeek() - Method in class org.orekit.time.DateComponents: Get the calendar week number.
getCalls() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the number of calls to the differential equations computation method.
getCalls() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get the number of calls to the differential equations computation method.
getCapitalizedAbbreviation() - Method in enum org.orekit.time.Month: Get the capitalized three letters abbreviation.
getCapitalizedName() - Method in enum org.orekit.time.Month: Get the capitalized full name.
getCarrierPhase(String) - Static method in enum org.orekit.gnss.metric.ntrip.CarrierPhase: Get the carrier phase corresponding to a code.
getCarrierPhase() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the carrier phase.
getCartesian() - Method in class org.orekit.frames.FieldTransform: Get the underlying elementary Cartesian part.
getCartesian() - Method in class org.orekit.frames.Transform: Get the underlying elementary Cartesian part.
getCartesianIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the intersection point of a line with the surface of the body.
getCartesianIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the intersection point of a line with the surface of the body.
getCasters() - Method in class org.orekit.gnss.metric.ntrip.SourceTable: Get the casters records.
getCatalogName() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the specification of satellite catalog source.
getCcsdsEpoch() - Method in class org.orekit.time.AbstractTimeScales
getCCSDSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4):
getCcsdsEpoch() - Method in interface org.orekit.time.TimeScales: Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).
getCdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the Unique identifier of Conjunction Data Message linked to this Orbit Data Message.
getCelestialBodies() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the instance of CelestialBodies that is called by the static methods in this class.
getCelestialBodies() - Method in class org.orekit.data.CompositeDataContext
getCelestialBodies() - Method in interface org.orekit.data.DataContext: Get a factory constructing CelestialBodys based on the auxiliary data in this context.
getCelestialBodies() - Method in class org.orekit.data.ExceptionalDataContext
getCelestialBodies() - Method in class org.orekit.data.LazyLoadedDataContext
getCelestialBody() - Method in enum org.orekit.files.ccsds.definitions.CenterName: Get the celestial body corresponding to the CCSDS constant.
getCelestialBody(CelestialBodies) - Method in enum org.orekit.files.ccsds.definitions.CenterName: Get the celestial body corresponding to the CCSDS constant.
getCelestialSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the source and version of celestial body (e.g.
getCenter() - Method in class org.orekit.bodies.Ellipse: Get the center of the 2D ellipse.
getCenter() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata: Get the body at origin of reference frame.
getCenter() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata: Get the origin of reference frame.
getCenter() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get the origin of reference frame.
getCenter() - Method in class org.orekit.geometry.fov.SmoothFieldOfView: Get the direction of the FOV center, in spacecraft frame.
getCenter() - Method in class org.orekit.models.earth.tessellation.Tile: Get the center point.
getCenterMass() - Method in class org.orekit.gnss.RinexObservationHeader: Get the current center of mass of vehicle in body fixed coordinate system.
getCenterName() - Method in class org.orekit.files.ccsds.definitions.ModifiedFrame: Get the CCSDS center name.
getCenterOfCurvature(Vector2D) - Method in class org.orekit.bodies.Ellipse: Find the center of curvature (point on the evolute) at the nadir of a point.
getCenterOfMassOffset() - Method in class org.orekit.files.ilrs.CPFHeader: Get the approximate center of mass to reflector offset.
getCentralBody() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector: Get the central body.
getCentralBodyRotation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get central body angular rotation rate.
getChi() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getChi() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getChi2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get Χ².
getChi2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get Χ².
getChildren() - Method in class org.orekit.frames.OrphanFrame: Get all children of the instance.
getCic() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac: Getter for the Cic parameter.
getCic() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Getter for the Cic parameter.
getCic() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination.
getCij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldFourierCjSjCoefficients: Get the coefficient C_i^j.
getCij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FourierCjSjCoefficients: Get the coefficient C_i^j.
getCircularEx() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the circular eccentricity vector.
getCircularEx() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the first component of the circular eccentricity vector.
getCircularExDot() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the circular eccentricity vector derivative.
getCircularExDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the first component of the circular eccentricity vector derivative.
getCircularEy() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the circular eccentricity vector.
getCircularEy() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the second component of the circular eccentricity vector.
getCircularEyDot() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the circular eccentricity vector derivative.
getCircularEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the second component of the circular eccentricity vector derivative.
getCIRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
getCIRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames: Get the CIRF2000 reference frame.
getCIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the CIRF2000 reference frame.
getCis() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac: Getter for the Cis parameter.
getCis() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Getter for the Cis parameter.
getCis() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination.
getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient: Get the C_j coefficient.
getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient: Get the C_j coefficient.
getCk0() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Get the un-normalized zonal coefficients.
getCk0() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Get the un-normalized zonal coefficients.
getClassification() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the message classification.
getClassification() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the classification.
getClassification() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the classification.
getClassificationType() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Get the classification type.
getClkOffset() - Method in class org.orekit.gnss.RinexObservationHeader: Get the realtime-derived receiver clock offset.
getClockAcceleration() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine: Getter for the clock acceleration.
getClockAccelerationSigma() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine: Getter for the clock acceleration sigma.
getClockBias() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine: Getter for the clock bias.
getClockBiasSigma() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine: Getter for the clock bias sigma.
getClockConstraint() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock: Getter for the clock constraint.
getClockCorrection() - Method in class org.orekit.files.sp3.SP3.SP3Coordinate: Returns the clock correction value.
getClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data: Get the clock correction data.
getClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data: Get the clock correction data.
getClockCount() - Method in class org.orekit.files.ccsds.utils.ContextBinding: Get clock count.
getClockData() - Method in class org.orekit.gnss.clock.RinexClock: Getter for an unmodifiable map of clock data.
getClockDataTypes() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the different clock data types.
getClockDriftDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to change station clock drift (which is related to measurement date).
getClockDriftDriver() - Method in class org.orekit.estimation.measurements.ObservableSatellite: Get the clock drift parameter driver.
getClockID() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock: Getter for the clock ID.
getClockOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to change station clock (which is related to measurement date).
getClockOffsetDriver() - Method in class org.orekit.estimation.measurements.ObservableSatellite: Get the clock offset parameter driver.
getClockRate() - Method in class org.orekit.files.ccsds.utils.ContextBinding: Get clock rate.
getClockRate() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine: Getter for the clock rate.
getClockRateChange() - Method in class org.orekit.files.sp3.SP3.SP3Coordinate: Returns the clock rate.
getClockRateSigma() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine: Getter for the clock rate sigma.
getCnm() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data: Get the cosine parameters of spherical harmonics expansion of degree N and order M.
getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext: Get co2AB = C / 2AB.
getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get Co2AB = C / 2AB.
getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext: Get co2AB = C / 2AB.
getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get Co2AB = C / 2AB.
getCodeBias() - Method in class org.orekit.gnss.metric.messages.ssr.igm.CodeBias: Get the code bias associated to the signal ID.
getCodeBias(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data: Get the code bias for a given signal ID.
getCodeBiases() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data: Get the code biases for the current satellite.
getCoefficients() - Method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients: Get the load deformation coefficients for ocean tides.
getCoefficients(String) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory: Get the coefficients for a given site.
getCoefficients(FieldAbsoluteDate<T>, Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients: Computes the coefficients involved in the contributions.
getCoefficients(AbsoluteDate, Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients: Computes the coefficients involved in the contributions.
getCoefficients(FieldAbsoluteDate<T>, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms: Computes the coefficients involved in the contributions.
getCoefficients(AbsoluteDate, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms: Computes the coefficients involved in the contributions.
getCoefficientsKeyPrefix() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients: Get the prefix for short period coefficients keys.
getCoefficientsKeyPrefix() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients: Get the prefix for short period coefficients keys.
getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms: Get the prefix for short period coefficients keys.
getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms: Get the prefix for short period coefficients keys.
getCombinationType() - Method in class org.orekit.gnss.CombinedObservationData: Get the type of the combination of measurements used to build the instance.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination: Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCombination: Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.IonosphereFreeCombination: Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.NarrowLaneCombination: Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.WideLaneCombination: Get the combined frequency of two measurements.
getCombinedMHzFrequency() - Method in class org.orekit.gnss.CombinedObservationData: Get the value of the combined frequency in MHz.
getCombinedProvider(TransformProvider, TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils: Combine two transform providers.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination: Get the combined observed value of two measurements.
getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination: Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCombination: Get the combined observed value of two measurements.
getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.GRAPHICCombination: Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.IonosphereFreeCombination: Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.NarrowLaneCombination: Get the combined observed value of two measurements.
getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCombination: Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.WideLaneCombination: Get the combined observed value of two measurements.
getComments() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData: Get the comments.
getComments() - Method in class org.orekit.files.ccsds.ndm.Ndm: Get an unmodifiable view of the comments.
getComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer: Get the comments.
getComments() - Method in class org.orekit.files.ilrs.CPF: Get the comments contained in the file.
getComments() - Method in class org.orekit.files.ilrs.CRD: Get the comments contained in the file.
getComments() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the comments.
getComments() - Method in class org.orekit.gnss.navigation.RinexNavigation: Getter for the comments.
getCompleteName(T) - Method in class org.orekit.data.AbstractListCrawler: Get the complete name of a input.
getCompleteName(File) - Method in class org.orekit.data.FilesListCrawler: Get the complete name of a input.
getCompleteName(URL) - Method in class org.orekit.data.NetworkCrawler: Get the complete name of a input.
getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate: Split the instance into date/time components.
getComponents(int) - Method in class org.orekit.time.AbsoluteDate: Split the instance into date/time components for a local time.
getComponents(int, TimeScale) - Method in class org.orekit.time.AbsoluteDate: Split the instance into date/time components for a local time.
getComponents(TimeZone) - Method in class org.orekit.time.AbsoluteDate: Split the instance into date/time components for a time zone.
getComponents(TimeZone, TimeScale) - Method in class org.orekit.time.AbsoluteDate: Split the instance into date/time components for a time zone.
getComponents(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate: Split the instance into date/time components.
getComponents(int) - Method in class org.orekit.time.FieldAbsoluteDate: Split the instance into date/time components for a local time.
getComponents(int, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate: Split the instance into date/time components for a local time.
getComponents(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate: Split the instance into date/time components for a time zone.
getComponents(TimeZone, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate: Split the instance into date/time components for a time zone.
getCompressionEncryption() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the compression/encryption algorithm applied.
getConfidence() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get confidence metric.
getConfiguration(String, int) - Method in class org.orekit.frames.ITRFVersionLoader
getConfiguration(String, int) - Method in interface org.orekit.frames.ItrfVersionProvider: Get the ITRF version configuration defined by a given file at specified date.
getConfigurationRecords() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the system configuration records.
getConsiderN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get number of consider parameters.
getConsiderParameters() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get description of consider parameters.
getConstantNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the constant gravity field coefficients provider from the first supported file.
getConstantNormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields: Get a constant gravity field normalized coefficients provider.
getConstantNormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields: Get a constant gravity field normalized coefficients provider.
getConstantProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Deprecated.
as of 11.1, not used anymore
getConstantUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the constant gravity field coefficients provider from the first supported file.
getConstantUnnormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields: Get a constant gravity field unnormalized coefficients provider.
getConstantUnnormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields: Get a constant gravity field unnormalized coefficients provider.
getConstellation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the name of the constellation this space object belongs to.
getConstituents() - Method in class org.orekit.files.ccsds.ndm.Ndm: Get an unmodifiable view of the constituents.
getConstraintsMap() - Method in class org.orekit.utils.AbstractMultipleShooting: Get the map of patch points components which are constrained.
getContentAsBoolean() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as a boolean.
getContentAsDouble() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as a double.
getContentAsEnum(Class<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as an enum.
getContentAsEnumList(Class<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as a list of enum.
getContentAsInt() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as an integer.
getContentAsNormalizedList() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as a list of free-text strings.
getContentAsNormalizedString() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry.
getContentAsUppercaseCharacter() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as an uppercase character.
getContentAsUppercaseList() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as a list of normalized and uppercased strings.
getContentAsUppercaseString() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as normalized and uppercased.
getContentAsVector() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as a vector.
getContext() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter: Get the current context.
getConventions() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder: Get the IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent: Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.utils.ContextBinding: Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Get IERS conventions.
getConventions() - Method in class org.orekit.frames.EOPHistory: Get the IERS conventions to which these EOP apply.
getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester: Get the conversion Jacobian between state parameters and parameters used for derivatives.
getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.numerical.AbsoluteJacobiansMapper: Get the conversion Jacobian between state parameters and parameters used for derivatives.
getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.numerical.JacobiansMapper: Get the conversion Jacobian between state parameters and parameters used for derivatives.
getConverter(ContextBinding) - Method in enum org.orekit.files.ccsds.definitions.TimeSystem: Get associated TimeConverter.
getConverter(ITRFVersion, ITRFVersion) - Static method in enum org.orekit.frames.ITRFVersion: Find a converter between specified ITRF frames.
getConverter(ITRFVersion, ITRFVersion, TimeScale) - Static method in enum org.orekit.frames.ITRFVersion: Find a converter between specified ITRF frames.
getCoordinates(SpacecraftState, int, int) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement: Get Cartesian coordinates as derivatives.
getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory: Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData: Get an unmodifiable view of the data points.
getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment: Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment: Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment: Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris: Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3: Returns the coordinate system of the entries in this orbit file.
getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the estimated measurement.
getCorrectedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the estimated measurement.
getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the estimated measurement.
getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the corrected spacecraft states.
getCorrectedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the corrected spacecraft states.
getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the corrected spacecraft states.
getCorrection() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.PhaseShiftCorrection: Get the Phase Shift Corrections.
getCorrection() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.ScaleFactorCorrection: Get the Scale Factor.
getCorrectionAberrationDiurnal() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the diurnal aberration correction.
getCorrectionAberrationYearly() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the yearly aberration correction.
getCorrectionAngle1() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the correctionAngle1.
getCorrectionAngle2() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the correctionAngle2.
getCorrectionDoppler() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the correctionDoppler.
getCorrectionMagnitude() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the magnitude correction.
getCorrectionRange(RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the raw correction for range in meters.
getCorrectionRcs() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the radar cross section correction.
getCorrectionReceive() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the correctionReceive.
getCorrectionsApplied() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the correctionApplied.
getCorrectionTransmit() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the correctionTransmit.
getCorrelationCoefficientsMatrix() - Method in class org.orekit.estimation.measurements.Position: Get the correlation coefficients matrix.
getCorrelationCoefficientsMatrix() - Method in class org.orekit.estimation.measurements.PV: Get the correlation coefficients matrix.
getCosparID() - Method in class org.orekit.gnss.antenna.SatelliteAntenna: Get COSPAR ID.
getCount() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the evaluations counter.
getCountry() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the name of the country where the space object owner is based.
getCountry() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Get the country.
getCountry() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the country.
getCovariance() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
getCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData: Get the covariance matrix logical block.
getCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData: Get the covariance matrix logical block.
getCovarianceBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData: Get covariance logical blocks.
getCovarianceMatrices() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData: Get an unmodifiable view of Covariance Matrices.
getCovarianceMatrices() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment: Get an unmodifiable view of Covariance Matrices.
getCovarianceMatrix() - Method in class org.orekit.estimation.measurements.Position: Get the covariance matrix.
getCovarianceMatrix() - Method in class org.orekit.estimation.measurements.PV: Get the covariance matrix.
getCovarianceMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance: Get the Position/Velocity covariance matrix.
getCovariances() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistory: Get the covariances.
getCovBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Get basis of this covariance time history data.
getCovBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Get identification number of the orbit determination or simulation upon which this covariance is based.
getCovConfidence() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Get the measure of confidence in covariance error matching reality.
getCovFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Get epoch of the covariance reference frame.
getCovID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Get covariance identification number.
getCovNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Get identification number of next covariance.
getCovOrdering() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Get covariance ordering.
getCovPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Get identification number of previous covariance.
getCovReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Get reference frame of the covariance.
getCovScaleMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Get the maximum scale factor to apply to achieve realism.
getCovScaleMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Get the minimum scale factor to apply to achieve realism.
getCovType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Get covariance element set type.
getCovUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Get covariance element set units.
getCr3bpSystem() - Method in class org.orekit.orbits.RichardsonExpansion: Get the considered CR3BP system.
getCrc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac: Getter for the Crc parameter.
getCrc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Getter for the Crc parameter.
getCrc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius.
getCreationDate() - Method in class org.orekit.files.ccsds.section.Header: Get the file creation date and time in UTC.
getCreationDate() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the creation date.
getCreationDate() - Method in class org.orekit.gnss.navigation.RinexNavigation: Getter for the creation date.
getCreationDateString() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the creation date of the file as a string.
getCreationDateString() - Method in class org.orekit.gnss.navigation.RinexNavigation: Getter for the creation date of the file as a string.
getCreationTimeString() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the creation time of the file as a string.
getCreationTimeString() - Method in class org.orekit.gnss.navigation.RinexNavigation: Getter for the creation time of the file as a string.
getCreationTimeZoneString() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the creation time zone of the file as a string.
getCreationTimeZoneString() - Method in class org.orekit.gnss.navigation.RinexNavigation: Getter for the creation time zone of the file as a string.
getCrs() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac: Getter for the Crs parameter.
getCrs() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Getter for the Crs parameter.
getCrs() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius.
getCrsIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header: Get the Global/Regional CRS Indicator.
getCrsIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header: Get the Global/Regional CRS Indicator.
getCtr81Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the centered 81-day arithmetic average of F10.7 (adjusted).
getCtr81Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the centered 81-day arithmetic average of F10.7 (observed).
getCuc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac: Getter for the Cuc parameter.
getCuc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Getter for the Cuc parameter.
getCuc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude.
getCurrent() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser: Get the current processing state.
getCurrent() - Method in class org.orekit.utils.units.Unit: Get the current exponent.
getCurrentDate() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the current date.
getCurrentDate() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the current date.
getCurrentDate() - Method in class org.orekit.estimation.sequential.KalmanEstimator: Get the current date.
getCurrentDate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator: Get the current date.
getCurrentDate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the current date.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the current measurement number.
getCurrentMeasurementNumber() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the current measurement number.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.KalmanEstimator: Get the current measurement number.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator: Get the current measurement number.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the current measurement number.
getCurrentState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator: Get the state at previous grid point date.
getCurrentState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Get the state at current grid point date.
getCus() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac: Getter for the Cus parameter.
getCus() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Getter for the Cus parameter.
getCus() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude.
getCXO2N2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get (C * χ) / ( 2 * n² * a² ).
getCXO2N2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get (C * χ) / ( 2 * n² * a² ).
getCycleDuration() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the duration of the GNSS cycle in seconds.
getCycleDuration() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements: Gets the duration of the GNSS cycle in seconds.
getCycleDuration() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the duration of the GNSS cycle in seconds.
getCycleSlipMap() - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults: Get the cycle slip Map with contains the results.
getD() - Method in class org.orekit.data.DelaunayArguments: Get the mean elongation of the Moon from the Sun.
getD() - Method in class org.orekit.data.FieldDelaunayArguments: Get the mean elongation of the Moon from the Sun.
getDailyFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Get the value of the daily F10.7 solar flux for previous day.
getDailyFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: Get the value of the daily F10.7 solar flux for previous day.
getDailyFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters: Get the value of the daily F10.7 solar flux for previous day.
getDarkCount() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the dark count.
getData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm: Get the file data.
getData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm: Get the data from the single segment.
getData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm: Get the file data.
getData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Get the file data.
getData() - Method in class org.orekit.files.ccsds.section.Segment: Get the segment data.
getData() - Method in class org.orekit.files.ilrs.CRD.Meteo: Get an unmodifiable view of the tabulated meteorological data.
getData() - Method in class org.orekit.gnss.metric.messages.rtcm.RtcmMessage: Get the data.
getData() - Method in class org.orekit.gnss.metric.messages.ssr.SsrMessage: Get the data.
getData() - Method in class org.orekit.utils.DoubleArrayDictionary: Get an unmodifiable view of the dictionary entries.
getData() - Method in class org.orekit.utils.FieldArrayDictionary: Get an unmodifiable view of the dictionary entries.
getData() - Method in class org.orekit.utils.TimeSpanMap.Span: Get the data valid during this time span.
getDataBlocks() - Method in class org.orekit.files.ilrs.CRD: Get the data blocks contain in the file.
getDataContext() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder: Get the data context.
getDataContext() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent: Get the data context.
getDataContext() - Method in class org.orekit.files.ccsds.utils.ContextBinding: Get the data context used for getting frames, time scales, and celestial bodies.
getDataContext() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Get the data context used for getting frames, time scales, and celestial bodies.
getDataFormat(String) - Static method in enum org.orekit.gnss.metric.ntrip.DataFormat: Get the message type corresponding to a keyword.
getDataProvidersManager() - Method in class org.orekit.data.AbstractSelfFeedingLoader: Get the data provider manager.
getDataProvidersManager() - Method in class org.orekit.data.LazyLoadedDataContext: Get the provider of auxiliary data for this data context.
getDataProvidersManager() - Method in class org.orekit.frames.LazyLoadedEop: Get the data providers manager for this instance.
getDataQuality() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the dataQuality.
getDataReleaseFlag() - Method in class org.orekit.files.ilrs.CRDHeader: Get the flag indicating the data release.
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader: Getter for the data set.
getDataStreams() - Method in class org.orekit.gnss.metric.ntrip.SourceTable: Get the data streams records.
getDataType() - Method in class org.orekit.files.ilrs.CRDHeader: Get the data type.
getDataType() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine: Getter for the clock data type.
getDataTypes() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get observation data types used.
getDataTypes() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the data types in the data section.
getDataUsed() - Method in class org.orekit.files.sp3.SP3: Returns the data used indicator from the SP3 file.
getDate() - Method in class org.orekit.attitudes.Attitude: Get the date of attitude parameters.
getDate() - Method in class org.orekit.attitudes.FieldAttitude: Get the date of attitude parameters.
getDate() - Method in class org.orekit.data.DelaunayArguments: Get the date.
getDate() - Method in class org.orekit.data.FieldDelaunayArguments: Get the date.
getDate() - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Get the date.
getDate() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Covariance: Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState: Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm: Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Get the date.
getDate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement: Get the date.
getDate() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement: Get the date.
getDate() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement: Get the date.
getDate() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Get the date of the maneuver.
getDate() - Method in class org.orekit.frames.EOPEntry: Get the date.
getDate() - Method in class org.orekit.frames.FieldTransform: Get the date.
getDate() - Method in class org.orekit.frames.Transform: Get the date.
getDate() - Method in class org.orekit.gnss.CombinedObservationDataSet: Get the date.
getDate() - Method in class org.orekit.gnss.DOP: Gets the calculation date of the DOP.
getDate() - Method in class org.orekit.gnss.ObservationDataSet: Get the date.
getDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
getDate() - Method in class org.orekit.orbits.FieldOrbit: Get the date of orbital parameters.
getDate() - Method in class org.orekit.orbits.Orbit: Get the date of orbital parameters.
getDate() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Getter for the reference date of the ephemeris.
getDate() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the ephemeris reference date.
getDate() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
getDate() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
getDate() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the TLE current date.
getDate() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the TLE current date.
getDate() - Method in class org.orekit.propagation.events.DateDetector: Get the current event date according to the propagator.
getDate() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent: Get the date.
getDate() - Method in class org.orekit.propagation.events.FieldDateDetector: Get the current event date according to the propagator.
getDate() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the date.
getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the date of the orbit.
getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the date of the orbit.
getDate() - Method in class org.orekit.propagation.SpacecraftState: Get the date.
getDate() - Method in class org.orekit.time.AbsoluteDate: Get the date.
getDate() - Method in class org.orekit.time.DateTimeComponents: Get the date component.
getDate() - Method in class org.orekit.time.FieldAbsoluteDate: Get the date.
getDate() - Method in interface org.orekit.time.FieldTimeStamped: Get the date.
getDate() - Method in class org.orekit.time.GLONASSDate
getDate() - Method in class org.orekit.time.GNSSDate: Get the date.
getDate() - Method in interface org.orekit.time.TimeStamped: Get the date.
getDate() - Method in class org.orekit.time.UTCTAIOffset: Get the date of the start of the leap.
getDate() - Method in class org.orekit.utils.DateDriver: Get the shifted date.
getDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition: Get the transition absolute date.
getDate() - Method in class org.orekit.utils.TimeSpanMap.Transition: Get the transition date.
getDate() - Method in class org.orekit.utils.TimeStampedAngularCoordinates: Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates: Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates: Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedPVCoordinates: Get the date.
getDateAndTime() - Method in class org.orekit.files.ilrs.CRDHeader: Get the date and time as the string value.
getDates() - Method in class org.orekit.propagation.events.DateDetector: Get all event dates currently managed, in chronological order.
getDay() - Method in class org.orekit.time.DateComponents: Get the day.
getDayFraction() - Method in class org.orekit.files.sp3.SP3: Returns the day fraction for this SP3 file.
getDayNumber() - Method in class org.orekit.time.GLONASSDate: Get the number of the current day in a four year interval.
getDayOfWeek() - Method in class org.orekit.time.DateComponents: Get the day of week.
getDayOfYear() - Method in class org.orekit.time.DateComponents: Get the day number in year.
getDcBodyFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get spacecraft body frame in which ManeuverHistoryMetadata.getDcBodyTrigger() is specified.
getDcBodyTrigger() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get direction in body frame for triggering duty cycle.
getDcExecStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get the start time of initial duty cycle-based maneuver execution.
getDcExecStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get the end time of final duty cycle-based maneuver execution.
getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient: Get the dC_j / dh coefficient.
getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient: Get the dC_j / dh coefficient.
getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient: Get the dC_j / dk coefficient.
getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient: Get the dC_j / dk coefficient.
getDcMaxCycles() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get the maximum number of "ON" duty cycles.
getDcMinCycles() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get the minimum number of "ON" duty cycles.
getDcPhaseStartAngle() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get phase angle of pulse start.
getDcPhaseStopAngle() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get phase angle of pulse stop.
getDcRefDir() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get reference direction for triggering duty cycle.
getDcRefTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get duty cycle thrust reference time.
getDcTimePulseDuration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get duty cycle pulse "ON" duration.
getDcTimePulsePeriod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get duty cycle elapsed time between start of a pulse and start of next pulse.
getDcType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get type of duty cycle.
getDcWindowClose() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get the end time of duty cycle-based maneuver window.
getDcWindowOpen() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get the start time of duty cycle-based maneuver window.
getDdEps() - Method in class org.orekit.frames.EOPEntry: Get the correction for nutation in obliquity δΔε.
getDdim() - Method in class org.orekit.bodies.CR3BPSystem: Get the CR3BP distance between the two bodies.
getDDot() - Method in class org.orekit.data.DelaunayArguments: Get the mean elongation of the Moon from the Sun time derivative.
getDDot() - Method in class org.orekit.data.FieldDelaunayArguments: Get the mean elongation of the Moon from the Sun time derivative.
getDdPsi() - Method in class org.orekit.frames.EOPEntry: Get the correction for nutation in longitude δΔΨ.
getDecimalYear(int, int, int) - Static method in class org.orekit.models.earth.GeoMagneticField: Utility function to get a decimal year for a given day.
getDeclination() - Method in class org.orekit.models.earth.GeoMagneticElements: Returns the declination of the magnetic field in radians.
getDecorrelatedReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Get the reference decorrelated ambiguities.
getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter: Get the decreasing events time shift.
getDefault() - Static method in interface org.orekit.data.DataContext: Get the default data context that is used to implement the static factories (TimeScalesFactory, FramesFactory, etc) and loaders that feed themselves (e.g.
getDefaultInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder: Get the default interpolation degree.
getDefaultLaw(Frames) - Static method in interface org.orekit.propagation.Propagator: Get a default law using the given frames.
getDefaultMass() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder: Get the default mass.
getDefaultModel() - Static method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay: Returns the default model, loading delay values from the file "tropospheric-delay.txt" via the default data context.
getDefaultTimeSystem(TimeScales) - Method in enum org.orekit.gnss.SatelliteSystem: Get default time scale for satellite system.
getDefaultVersion() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter: Get the default format version.
getDefaultYawRate(int) - Static method in class org.orekit.gnss.attitude.GPSBlockIIA: Get the default yaw rate for a satellite.
getDelaunayMultipliers() - Method in class org.orekit.models.earth.displacement.Tide: Get the multipliers for Delaunay arguments (l, l', F, D, Ω).
getDeltaClockC0() - Method in class org.orekit.gnss.metric.messages.ssr.igm.ClockCorrection: Get the delta clock C0.
getDeltaClockC1() - Method in class org.orekit.gnss.metric.messages.ssr.igm.ClockCorrection: Get the delta clock C1.
getDeltaClockC2() - Method in class org.orekit.gnss.metric.messages.ssr.igm.ClockCorrection: Get the delta clock C2.
getDeltaI() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
getDeltaI() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the correction to the mean value of inclination.
getDeltaMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get mass change.
getDeltaMass() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver: Get mass change during maneuver (value is < 0).
getDeltaOrbitAlongTrack() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection: Get the along-track orbit correction for broadcast ephemeris.
getDeltaOrbitCrossTrack() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection: Get the cross-track orbit correction for broadcast ephemeris.
getDeltaOrbitRadial() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection: Get the radial orbit correction for broadcast ephemeris.
getDeltaT() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
getDeltaT() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the correction to the mean value of Draconian period.
getDeltaTDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
getDeltaTDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the rate of change of Draconian period.
getDeltaTN() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the deltaTauN value.
getDeltaVSat() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Get the velocity increment in satellite frame.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere: Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere: Get the local density.
getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.DTM2000: Get the local density with initial entries.
getDensity(int, T, T, T, T, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.DTM2000: Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.DTM2000: Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.DTM2000: Get the local density.
getDensity(Vector3D, Vector3D) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester: Get the local density.
getDensity(Vector3D, FieldVector3D<T>) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester: Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester: Get the local density at some position.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester: Get the local density at some position.
getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.JB2008: Get the local density with initial entries.
getDensity(T, T, T, T, T, T, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.JB2008: Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.JB2008: Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.JB2008: Get the local density.
getDensity(int) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00.FieldOutput: Get one of the stored densities.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00: Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00: Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere: Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
getDeployDirSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get one σ angular off-nominal deployment vector direction.
getDeployDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get velocity increment of deployed "child" object.
getDeployDvCda() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.
getDeployDvRatio() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get ratio of child-to-host ΔV vectors.
getDeployDvSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get one σ percent error on deployment ΔV magnitude.
getDeployId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get identifier of resulting "child" object deployed from this host.
getDeployMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get decrement in host mass as a result of deployment.
getDepth() - Method in class org.orekit.frames.Frame: Get the depth of the frame.
getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction: Get Γ function derivative.
getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction: Get Γ function derivative.
getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear: Compute the value of the derivative dK_j^{-n-1, s} / de².
getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear: Compute the value of the Hansen coefficient dK₀^{n, s} / dΧ.
getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear: Get the dK₀^-n-1,s / dΧ coefficient derivative.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear: Compute the value of the derivative dK_j^{-n-1, s} / de².
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear: Compute the value of the Hansen coefficient dK₀^{n, s} / dΧ.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear: Get the dK₀^-n-1,s / dΧ coefficient derivative.
getDerivativesDrivers() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get all the drivers with set derivatives.
getDerivativesToEpoch(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttractionEpoch: Compute derivatives of the state w.r.t epoch.
getDesignator() - Method in class org.orekit.gnss.clock.RinexClock.Receiver: Getter for the designator.
getDestination() - Method in enum org.orekit.frames.HelmertTransformation.Predefined: Get the destination ITRF.
getDestination() - Method in class org.orekit.frames.ITRFVersion.Converter: Get the destination ITRF.
getDetector() - Method in class org.orekit.propagation.events.AdapterDetector: Get the wrapped detector.
getDetector() - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter: Get the wrapped raw detector.
getDetector() - Method in class org.orekit.propagation.events.EventShifter: Get the detector for the raw unshifted event.
getDetector() - Method in class org.orekit.propagation.events.EventSlopeFilter: Get the wrapped raw detector.
getDetector() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event: Get the detector.
getDetector() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event: Get the detector.
getDetectorId() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the detector configuration ID.
getDetectorRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration: Get the detector configuration record.
getDetectors() - Method in class org.orekit.propagation.events.BooleanDetector: Get the list of original detectors.
getDetectorType() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the detector type.
getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dG_js / dα coefficient.
getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dG_js / dα coefficient.
getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dG_js / dβ coefficient.
getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dG_js / dβ coefficient.
getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dG_js / dh coefficient.
getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dG_js / dh coefficient.
getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dG_js / dk coefficient.
getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dG_js / dk coefficient.
getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dG_ms^j / d_α coefficient.
getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dG_ms^j / d_α coefficient.
getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dG_ms^j / d_β coefficient.
getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dG_ms^j / d_β coefficient.
getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dG_ms^j / d_h coefficient.
getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dG_ms^j / d_h coefficient.
getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dG_ms^j / d_k coefficient.
getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dG_ms^j / d_k coefficient.
getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dH_js / dα coefficient.
getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dH_js / dα coefficient.
getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dH_js / dβ coefficient.
getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dH_js / dβ coefficient.
getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dH_js / dh coefficient.
getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dH_js / dh coefficient.
getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dH_js / dk coefficient.
getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dH_js / dk coefficient.
getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dH_ms^j / d_α coefficient.
getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dH_ms^j / d_α coefficient.
getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dH_ms^j / d_β coefficient.
getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dH_ms^j / d_β coefficient.
getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dH_ms^j / d_h coefficient.
getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dH_ms^j / d_h coefficient.
getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the dH_ms^j / d_k coefficient.
getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the dH_ms^j / d_k coefficient.
getDiagReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Get a reference to the diagonal matrix of the decomposition.
getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dI_js / dα coefficient.
getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dI_js / dα coefficient.
getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dI_js / dβ coefficient.
getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dI_js / dβ coefficient.
getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dI_js / dh coefficient.
getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dI_js / dh coefficient.
getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dI_js / dk coefficient.
getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dI_js / dk coefficient.
getDimension() - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Get the dimension of the measurement.
getDimension() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Get the dimension of the measurement.
getDimension() - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay: Get the dimension of the generated column.
getDimension() - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider: Get the dimension of the generated derivative.
getDimension() - Method in class org.orekit.propagation.integration.AdditionalEquationsAdapter: Deprecated.

Get the dimension of the generated derivative.
getDimension() - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider: Get the dimension of the generated derivative.
getDimension() - Method in class org.orekit.propagation.integration.FieldAdditionalEquationsAdapter: Deprecated.

Get the dimension of the generated derivative.
getDimension() - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations: Get the dimension of the generated derivative.
getDimension() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations: Get the dimension of the generated derivative.
getDimension() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Deprecated.

Get the dimension of the generated derivative.
getDimension() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations: Deprecated.

Get the dimension of the generated derivative.
getDirection() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the direction.
getDirection() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the thrust direction in S/C frame.
getDirection(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the thrust direction in spacecraft frame.
getDirectionFlag() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement: Get the direction flag (0 = transmit & receive ; 1 = transmit ; 2 = receive).
getDiscontinuityCounter() - Method in class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias: Get the signal phase discontinuity counter.
getDisplacements() - Method in class org.orekit.estimation.measurements.GroundStation: Get the displacement models.
getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dJ_js / dα coefficient.
getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dJ_js / dα coefficient.
getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dJ_js / dβ coefficient.
getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dJ_js / dβ coefficient.
getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dJ_js / dh coefficient.
getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dJ_js / dh coefficient.
getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the dJ_js / dk coefficient.
getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dJ_js / dk coefficient.
getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients: Get the value of dL_n^s / dγ (γ).
getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients: Get the value of dL_n^s / dγ (γ).
getDnl(double, double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds: Get the upper bound value D_n^l(Χ).
getDnl(T, T, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds: Get the upper bound value D_n^l(Χ).
getDockedWith() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the other space objects this object is docked to.
getDomes() - Method in class org.orekit.files.sinex.Station: Get the site DOMES number.
getDoodson() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave: Get the Doodson number for the wave.
getDoodsonMultipliers() - Method in class org.orekit.models.earth.displacement.Tide: Get the multipliers for Doodson arguments (τ, s, h, p, N', ps).
getDoodsonNumber() - Method in class org.orekit.models.earth.displacement.Tide: Get the Doodson number.
getDopplerCountBias() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Get the Doppler count bias.
getDopplerCountScale() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Get the Doppler count scale.
getDotOrbitDeltaAlongTrack() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection: Get the velocity of along-track orbit correction for broadcast ephemeris.
getDotOrbitDeltaCrossTrack() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection: Get the velocity of cross-track orbit correction for broadcast ephemeris.
getDotOrbitDeltaRadial() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection: Get the velocity of radial orbit correction for broadcast ephemeris.
getDrag() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get drag force.
getDragArea() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters: Get the drag area.
getDragCoeff() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters: Get the drag coefficient.
getDragCoefficient() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the nominal drag coefficient.
getDragConstantArea() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
getDragParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Get the drivers for supported parameters.
getDragParametersDrivers() - Method in interface org.orekit.forces.drag.DragSensitive: Get the drivers for supported parameters.
getDragParametersDrivers() - Method in class org.orekit.forces.drag.IsotropicDrag: Get the drivers for supported parameters.
getDragSensitive(AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce: Get the DragSensitive model valid at a date.
getDragSensitiveSpan(AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce: Get the DragSensitive TimeSpanMap.Span containing a specified date.
getDragUncertainty() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the drag coefficient 1σ uncertainty.
getDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier: Get the drivers for this modifier.
getDrivers(double, Orbit, PositionAngle) - Method in enum org.orekit.orbits.OrbitType: Get parameters drivers initialized from a reference orbit.
getDrivers() - Method in class org.orekit.utils.ParameterDriversList: Get delegating drivers for all parameters.
getDryMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the mass without propellant.
getDSDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.drag.AbstractDragForceModel: Compute density and its derivatives.
getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient: Get the dS_j / dh coefficient.
getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient: Get the dS_j / dh coefficient.
getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient: Get the dS_j / dk coefficient.
getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient: Get the dS_j / dk coefficient.
getDSTDTC(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Get the temperature change computed from Dst index.
getDuration() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver: Get duration (value is 0 for impulsive maneuver).
getDuration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get duration.
getDuration() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver: Get duration (value is 0 for impulsive maneuver).
getDuration() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the duration of the maneuver (s).
getDuration() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers: Get the duration of the maneuver (s).
getDurationDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector: Get the driver for duration.
getDurationDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector: Get the driver for duration.
getDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get velocity increment.
getDV() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver: Get velocity increment.
getDvDirSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get one σ angular off-nominal ΔV direction.
getDvMagSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get one σ percent error on ΔV magnitude.
getDx() - Method in class org.orekit.frames.EOPEntry: Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getDy() - Method in class org.orekit.frames.EOPEntry: Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getE() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Get the orbit eccentricity.
getE() - Method in class org.orekit.orbits.CartesianOrbit: Get the eccentricity.
getE() - Method in class org.orekit.orbits.CircularOrbit: Get the eccentricity.
getE() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldOrbit: Get the eccentricity.
getE() - Method in class org.orekit.orbits.KeplerianOrbit: Get the eccentricity.
getE() - Method in class org.orekit.orbits.Orbit: Get the eccentricity.
getE() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the eccentricity.
getE() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
getE() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the Eccentricity.
getE() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Eccentricity.
getE() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the eccentricity.
getE() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the eccentricity.
getE() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the eccentricity.
getE() - Method in class org.orekit.propagation.SpacecraftState: Get the eccentricity.
getE2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get ecc².
getE2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get ecc².
getEarliest() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the earliest cached entry.
getEarliest() - Method in class org.orekit.utils.ImmutableTimeStampedCache: Get the earliest entry in this cache.
getEarliest() - Method in interface org.orekit.utils.TimeStampedCache: Get the earliest entry in this cache.
getEarth() - Method in interface org.orekit.bodies.CelestialBodies: Get the Earth singleton body.
getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Earth singleton body.
getEarth() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
getEarth() - Method in class org.orekit.forces.gravity.DeSitterRelativity: Get the Earth model used to compute De Sitter effect.
getEarthMoonBarycenter() - Method in interface org.orekit.bodies.CelestialBodies: Get the Earth-Moon barycenter singleton bodies pair.
getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Earth-Moon barycenter singleton bodies pair.
getEarthMoonBarycenter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
getEarthMoonBarycenterSemiMajorAxis(AbsoluteDate, TimeScale) - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants: Get the Earth-Moon barycenter semi-major axis.
getEarthMoonCR3BP() - Static method in class org.orekit.bodies.CR3BPFactory: Get the Earth-Moon CR3BP singleton bodies pair.
getEarthOrientationAngleFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions: Get the function computing the raw Earth Orientation Angle.
getEarthOrientationAngleFunction(TimeScale, TimeScale) - Method in enum org.orekit.utils.IERSConventions: Get the function computing the raw Earth Orientation Angle.
getEast() - Method in class org.orekit.bodies.FieldGeodeticPoint: Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.bodies.GeodeticPoint: Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.frames.TopocentricFrame: Get the east direction of topocentric frame, expressed in parent shape frame.
getEastOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to change station position along East axis.
getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the eccentricity.
getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the eccentricity.
getEccentricAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the eccentric anomaly.
getEccentricAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit: Get the eccentric anomaly.
getEccentricAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the eccentric anomaly derivative.
getEccentricAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the eccentric anomaly derivative.
getEccentricities() - Method in class org.orekit.files.sinex.Station: Get the last known station antenna eccentricities.
getEccentricities(AbsoluteDate) - Method in class org.orekit.files.sinex.Station: Get the station antenna eccentricities for the given epoch.
getEccentricities(Frequency) - Method in class org.orekit.gnss.antenna.Antenna: Get the phase center eccentricities.
getEccentricities() - Method in class org.orekit.gnss.antenna.FrequencyPattern: Get the phase center eccentricities.
getEccentricities() - Method in class org.orekit.gnss.RinexObservationHeader: Get the eccentricities of antenna center.
getEccentricitiesTimeSpanMap() - Method in class org.orekit.files.sinex.Station: Get the TimeSpanMap of site antenna eccentricities.
getEccRefSystem() - Method in class org.orekit.files.sinex.Station: Get the reference system used to define the eccentricity vector (local or cartesian).
getEccRefSystem(String) - Static method in enum org.orekit.files.sinex.Station.ReferenceSystem: Get the eccentricity reference system corresponding to the given value.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator: Gets the Earth Centered Earth Fixed frame used to propagate GLONASS orbits.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator: Gets the Earth Centered Earth Fixed frame used to propagate GNSS orbits according to the Interface Control Document.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator: Gets the Earth Centered Earth Fixed frame used to propagate GNSS orbits.
getECI() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator: Gets the Earth Centered Inertial frame used to propagate the orbit.
getECI() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator: Gets the Earth Centered Inertial frame used to propagate the orbit.
getECI() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator: Gets the Earth Centered Inertial frame used to propagate the orbit.
getEclipseAngles(Vector3D, Vector3D) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Get the useful angles for eclipse computation.
getEclipseAngles(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Get the useful angles for eclipse computation.
getEcliptic(IERSConventions) - Method in class org.orekit.frames.AbstractFrames
getEcliptic(IERSConventions) - Method in interface org.orekit.frames.Frames: Get the ecliptic frame.
getEcliptic(IERSConventions) - Static method in class org.orekit.frames.FramesFactory: Get the ecliptic frame.
getEDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.CircularOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.Orbit: Get the eccentricity derivative.
getEffects() - Method in class org.orekit.propagation.analytical.AdapterPropagator: Get the differential effects.
getElem(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix: Get the value of an element.
getElementNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the element number.
getElementNumber() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the element number.
getElements() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState: Get trajectory elements.
getElementSetNumber() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Get the element set number for this satellite.
getElevation() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement: Get the elevation angle.
getElevation(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame: Get the elevation of a point with regards to the local point.
getElevation(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame: Get the elevation of a point with regards to the local point.
getElevation(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector: Get the elevation value.
getElevation(double) - Method in class org.orekit.utils.ElevationMask: Get the interpolated elevation for a given azimuth according to the mask.
getElevationMask() - Method in class org.orekit.gnss.DOPComputer: Get the elevation mask.
getElevationMask() - Method in class org.orekit.propagation.events.ElevationDetector: Returns the currently configured elevation mask.
getElevationMask() - Method in class org.orekit.propagation.events.FieldElevationDetector: Returns the currently configured elevation mask.
getElevationRate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement: Get the elevation rate.
getEllipsoid() - Method in interface org.orekit.models.earth.EarthShape: Get the underlying ellipsoid model that defines latitude and longitude.
getEllipsoid() - Method in class org.orekit.models.earth.Geoid
getEllipsoid() - Method in class org.orekit.models.earth.ReferenceEllipsoid
getEME2000() - Method in class org.orekit.frames.AbstractFrames
getEME2000() - Method in interface org.orekit.frames.Frames: Get the unique EME2000 frame.
getEME2000() - Static method in class org.orekit.frames.FramesFactory: Get the unique EME2000 frame.
getEn() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS E_n Word.
getEnd() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder: Get the end of the measurements time span.
getEnd() - Method in class org.orekit.utils.TimeSpanMap.Span: Get the end of this time span.
getEndDate(Frequency) - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults: Return the end date at the given frequency.
getEndDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the end date.
getEndDate() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers: Get the end date.
getEndDate() - Method in class org.orekit.frames.EOPHistory: Get the date of the last available Earth Orientation Parameters.
getEndDate() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock: Getter for the validity period end date.
getEndEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the ending epoch (UTC).
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get the endpoints (i.e.
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion: Get the endpoints (i.e.
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler: Get the endpoints (i.e.
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Get the endpoints (i.e.
getEndTransition() - Method in class org.orekit.utils.TimeSpanMap.Span: Get the transition at end of this time span.
getEntries() - Method in class org.orekit.frames.EOPHistory: Get a non-modifiable view of the EOP entries.
getEntries() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the total number of entries cached.
getEntry(String) - Method in class org.orekit.utils.DoubleArrayDictionary: Get a complete entry.
getEntry(String) - Method in class org.orekit.utils.FieldArrayDictionary: Get a complete entry.
getEOPHistory() - Method in interface org.orekit.frames.EOPBasedTransformProvider: Get the EOP history.
getEOPHistory(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames: Get Earth Orientation Parameters history.
getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get Earth Orientation Parameters history.
getEOPHistory() - Method in class org.orekit.frames.GTODProvider: Get the EOP history.
getEOPHistory(IERSConventions, boolean, TimeScales) - Method in class org.orekit.frames.LazyLoadedEop: Get Earth Orientation Parameters history.
getEOPHistory(IERSConventions, boolean) - Method in class org.orekit.frames.LazyLoadedFrames: Get Earth Orientation Parameters history.
getEopHistory(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales: Get the EOP history for the given conventions.
getEopHistory(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
getEOPHistory() - Method in class org.orekit.time.UT1Scale: Get the EOP history.
getEopSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the source and version of Earth Orientation Parameters.
getEOPTidalCorrection() - Method in enum org.orekit.utils.IERSConventions: Get the function computing tidal corrections for Earth Orientation Parameters.
getEOPTidalCorrection(TimeScales) - Method in enum org.orekit.utils.IERSConventions: Get the function computing tidal corrections for Earth Orientation Parameters.
getEphemeridesDataLines() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData: Get the list of Ephemerides data lines.
getEphemeridesDataLines() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris: Get the list of Ephemerides data lines.
getEphemerisData() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisMessage: Get the ephemeris data contain in the ephemeris message.
getEphemerisGenerator() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in interface org.orekit.propagation.FieldPropagator: Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in interface org.orekit.propagation.Propagator: Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisNames() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for external ephemeris names for participants.
getEphemerisType() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Get the ephemeris type.
getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the type of ephemeris.
getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the type of ephemeris.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion: Get the epoch of the data.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance: Get matrix epoch.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Get epoch of state vector, Keplerian elements and covariance matrix data.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get time tag for orbit determination solved-for state.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.StateVector: Get epoch of state vector, Keplerian elements and covariance matrix data.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation: Getter for the epoch.
getEpoch() - Method in class org.orekit.files.sinex.Station: Get the coordinates reference epoch.
getEpoch() - Method in class org.orekit.files.sp3.SP3: Returns the start epoch of the orbit file.
getEpoch() - Method in class org.orekit.frames.HelmertTransformation: Get the reference epoch of the transform.
getEpoch() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine: Get data line epoch.
getEpoch(TimeScale) - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine: Get data line epoch.
getEpoch() - Method in class org.orekit.models.earth.GeoMagneticField: Returns the epoch for this magnetic field model.
getEpochDelayCorrection() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration: Get the epoch delay correction.
getEpochEigenMaj() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get positional error ellipsoid 1σ major eigenvalue at the epoch of OD.
getEpochEigenMed() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get positional error ellipsoid 1σ intermediate eigenvalue at the epoch of OD.
getEpochEigenMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get positional error ellipsoid 1σ minor eigenvalue at the epoch of OD.
getEpochEvent() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement: Get the indicator for the time event reference.
getEpochIdentifier() - Method in class org.orekit.files.ilrs.CRDHeader: Get the epoch identifier.
getEpochIgnition() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver: Get epoch ignition.
getEpochInterval() - Method in class org.orekit.files.sp3.SP3: Returns the time interval between epochs (in seconds).
getEpochStart() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver: Get epoch start.
getEpochT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the epoch to which all relative times are referenced in data blocks.
getEpochToc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Getter for the time of clock epoch.
getEpochToc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Getter for the time of clock epoch.
getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the equatorial radius of the body.
getEquatorialRadius() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get oblate spheroid equatorial radius of central body.
getEquatorialRadius() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Getter for equatorial radius.
getEquatorialRadius() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Get the central body equatorial radius.
getEquinoctialEx() - Method in class org.orekit.orbits.CartesianOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.KeplerianOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.Orbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEx() - Method in class org.orekit.propagation.SpacecraftState: Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialExDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.Orbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.KeplerianOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.Orbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the second component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEy() - Method in class org.orekit.propagation.SpacecraftState: Get the second component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEyDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.Orbit: Get the second component of the equinoctial eccentricity vector.
getEquinoxNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the correction to the nutation parameters for equinox-based paradigm.
getEquinoxNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory: Get the correction to the nutation parameters for equinox-based paradigm.
getEstimate() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the current corrected estimate.
getEstimate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the current corrected estimate.
getEstimatedEarthFrame() - Method in class org.orekit.estimation.measurements.GroundStation: Get the estimated Earth frame, including the estimated linear models for pole and prime meridian.
getEstimatedMeasurement(int) - Method in interface org.orekit.estimation.measurements.EstimationsProvider: Get one estimated measurement.
getEstimatedMeasurements() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement: Get the underlying estimated measurements.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.KalmanEstimator: Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator: Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the list of estimated measurements parameters.
getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the list of estimated orbital parameters.
getEstimatedOrbitalParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the list of estimated orbital parameters.
getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the list of estimated orbital parameters.
getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the list of estimated propagation parameters.
getEstimatedPropagationParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the list of estimated propagation parameters.
getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the list of estimated propagation parameters.
getEstimatedPropagator() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the propagator estimated with the values set in the propagator builder.
getEstimatedPropagators() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the propagators estimated with the values set in the propagators builders.
getEstimatedUT1() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get the estimated UT1 time scale.
getEstimatedUT1() - Method in class org.orekit.estimation.measurements.GroundStation: Get the estimated UT1 scale, including the estimated linear models for prime meridian.
getEstimatedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the estimated value.
getEulerBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData: Get the Euler angles logical block.
getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get the rotation order of Euler angles.
getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler: Get the rotation order of Euler angles.
getEvaluations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the number of objective function evaluations.
getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel: Get the evaluations count.
getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Get the number of evaluations used for last estimation.
getEventDate() - Method in class org.orekit.propagation.events.EventState: Get the occurrence time of the event triggered in the current step.
getEventDate() - Method in class org.orekit.propagation.events.FieldEventState: Get the occurrence time of the event triggered in the current step.
getEventDetector() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent: Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.EventState: Get the underlying event detector.
getEventDetector() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent: Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.FieldEventState: Get the underlying event detector.
getEvents() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue: Get the events passed to this handler.
getEvents() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue: Get the events passed to this handler.
getEventsDetectors() - Method in class org.orekit.forces.drag.DragForce: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.drag.TimeSpanDragForce: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.empirical.ParametricAcceleration: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration: Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.forces.ForceModel: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.DeSitterRelativity: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.LenseThirringRelativity: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.NewtonianAttraction: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.OceanTides: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.Relativity: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.SolidTides: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.inertia.InertialForces: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.Maneuver: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers: Get the event detectors associated with the triggers.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger: Get the event detectors associated with the triggers.
getEventsDetectors() - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers: Get the event detectors associated with the triggers.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger: Get the event detectors associated with the triggers.
getEventsDetectors() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel: Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.propagation.Propagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Get the discrete events related to the model.
getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
getException() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor: Retrieve exception caught during monitoring.
getExponent() - Method in class org.orekit.utils.units.PowerTerm: Get the fractional exponent.
getExternalClockReference() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the external clock reference.
getExternalFrame() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints: Get the external frame.
getExternalSignalProcessing() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the external signal processing.
getExtrapolationThreshold() - Method in class org.orekit.propagation.analytical.Ephemeris: Get the maximum timespan outside of the stored ephemeris that is allowed for extrapolation.
getF() - Method in class org.orekit.data.DelaunayArguments: Get L - Ω where L is the mean longitude of the Moon.
getF() - Method in class org.orekit.data.FieldDelaunayArguments: Get L - Ω where L is the mean longitude of the Moon.
getF10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Get the value of the instantaneous solar flux index (1e^-22*Watt/(m²*Hertz)).
getF107Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the 10.7-cm Solar Radio Flux (F10.7) Adjusted to 1 AU.
getF107Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the observed (unadjusted) value of F10.7.
getF10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Get the value of the mean solar flux.
getFactoryKey() - Method in class org.orekit.frames.FactoryManagedFrame: Get the key of the frame within the factory.
getFallbackHostOrIPAddress() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Get the fallback host or IP address.
getFallbackPort() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Get the fallback port number.
getFDot() - Method in class org.orekit.data.DelaunayArguments: Get L - Ω where L is the mean longitude of the Moon time derivative.
getFDot() - Method in class org.orekit.data.FieldDelaunayArguments: Get L - Ω where L is the mean longitude of the Moon time derivative.
getField(int) - Method in class org.orekit.gnss.metric.ntrip.Record: Get one field from the parsed sourcetable.
getField(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory: Get the GeoMagneticField for the given model type and year.
getField(GeoMagneticFieldFactory.FieldModel, double) - Method in interface org.orekit.models.earth.GeoMagneticFields: Get the GeoMagneticField for the given model type and year.
getField(GeoMagneticFieldFactory.FieldModel, double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
getField() - Method in class org.orekit.propagation.FieldAbstractPropagator: Field getter.
getField() - Method in class org.orekit.time.FieldAbsoluteDate: Get the field.
getField() - Method in class org.orekit.utils.FieldArrayDictionary: Get the field to which elements belong.
getFieldAuxiliaryElements() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldForceModelContext: Method to get the auxiliary elementsrelated to the ForceModelContext.
getFieldDate() - Method in class org.orekit.frames.FieldTransform: Get the date.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.drag.DragForce: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.drag.TimeSpanDragForce: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.empirical.ParametricAcceleration: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.forces.ForceModel: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.DeSitterRelativity: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.LenseThirringRelativity: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.OceanTides: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.Relativity: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SolidTides: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.inertia.InertialForces: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.Maneuver: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers: Get the event detectors associated with the triggers.
getFieldEventsDetectors(Field<S>) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger: Get the event detectors associated with the triggers.
getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers: Get the event detectors associated with the triggers.
getFieldEventsDetectors(Field<S>) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger: Get the event detectors associated with the triggers.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Get the discrete events related to the model.
getFieldsNumber() - Method in class org.orekit.gnss.metric.ntrip.Record: Get the number of fields.
getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements: Returns the magnetic field vector in nTesla.
getFiftiesEpoch() - Method in class org.orekit.time.AbstractTimeScales
getFiftiesEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
getFiftiesEpoch() - Method in interface org.orekit.time.TimeScales: Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
getFileDate(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: Get the date of the file from which data at the specified date comes from.
getFileFormat() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser: Get the file format.
getFileName() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the name of the file.
getFileType() - Method in class org.orekit.gnss.navigation.RinexNavigation: Get the file type.
getFilter(int) - Static method in enum org.orekit.utils.AngularDerivativesFilter: Get the filter corresponding to a maximum derivation order.
getFilter(int) - Static method in enum org.orekit.utils.CartesianDerivativesFilter: Get the filter corresponding to a maximum derivation order.
getFiltersManager() - Method in class org.orekit.data.DataProvidersManager: Get the manager for filters.
getFiringIntervalDetector() - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger: Getter for the firing interval detector.
getFirings() - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers: Get the firings detected during last propagation.
getFirstKnownLeapSecond() - Method in class org.orekit.time.UTCScale: Get the date of the first known leap second.
getFirstSpan() - Method in class org.orekit.forces.drag.TimeSpanDragForce: Get the first time span of the drag sensitive time span map.
getFirstSpan() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration: Get the first time span of the acceleration model time span map.
getFirstSpan() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel: Get the first time span of the tropospheric model time span map.
getFirstSpan() - Method in class org.orekit.utils.TimeSpanMap: Get the first (earliest) span.
getFirstTransition() - Method in class org.orekit.utils.TimeSpanMap: Get the first (earliest) transition.
getFittedParameters() - Method in class org.orekit.utils.SecularAndHarmonic: Get a copy of the last fitted parameters.
getFixedF10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get fixed (time invariant) value of the Solar Flux Unit daily proxy F10.7.
getFixedF10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get fixed (time invariant) value of the Solar Flux Unit 81-day running center-average proxy F10.7.
getFixedGeomagneticAp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get fixed (time invariant) value of the planetary 3-hour-range geomagnetic index aₚ.
getFixedGeomagneticDst() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get fixed (time invariant) value of the planetary 1-hour-range geomagnetic index Dst.
getFixedGeomagneticKp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get fixed (time invariant) value of the planetary 3-hour-range geomagnetic index Kₚ.
getFixedM10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get fixed (time invariant) value of the Solar Flux daily proxy M10.7.
getFixedM10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy M10.7.
getFixedS10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get fixed (time invariant) value of the Solar Flux daily proxy S10.7.
getFixedS10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy S10.7.
getFixedStepHandler() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer: Get the underlying fixed step handler.
getFixedStepHandler() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer: Get the underlying fixed step handler.
getFixedTimeStep() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer: Get the fixed time step.
getFixedTimeStep() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer: Get the fixed time step.
getFixedY10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get fixed (time invariant) value of the Solar Flux daily proxy Y10.7.
getFixedY10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy Y10.7.
getFlattening() - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the flattening of the body: f = (a-b)/a.
getFlowRate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the flow rate.
getFlowRate(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the flow rate (kg/s).
getFluxQualifier() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the Flux Qualifier.
getFocus1() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView: Get first focus in spacecraft frame.
getFocus2() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView: Get second focus in spacecraft frame.
getFootprint(Transform, OneAxisEllipsoid, double) - Method in interface org.orekit.geometry.fov.FieldOfView: Get the footprint of the Field Of View on ground.
getFootprint(Transform, OneAxisEllipsoid, double) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView: Get the footprint of the Field Of View on ground.
getFootprint(Transform, OneAxisEllipsoid, double) - Method in class org.orekit.geometry.fov.SmoothFieldOfView: Get the footprint of the Field Of View on ground.
getFormat() - Method in interface org.orekit.files.ccsds.utils.generation.Generator: Get the generated file format.
getFormat() - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator: Get the generated file format.
getFormat() - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator: Get the generated file format.
getFormat() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the file format.
getFormat() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the data format.
getFormatDetails() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the format details.
getFormatVersion() - Method in class org.orekit.files.ccsds.section.Header: Get the CCSDS NDM (ADM, ODM or TDM) format version.
getFormatVersion() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the format version.
getFormatVersion() - Method in class org.orekit.gnss.navigation.RinexNavigation: Getter for the format version.
getFormatVersionKey() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser: Get the key for format version.
getFormatVersionKey() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser: Get the key for format version.
getFOV() - Method in class org.orekit.propagation.events.FieldOfViewDetector: Get the Field Of View.
getFOV() - Method in class org.orekit.propagation.events.FootprintOverlapDetector: Get the Field Of View.
getFOV() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector: Get the Field Of View.
getFrame() - Method in class org.orekit.bodies.Ellipse: Get the defining frame.
getFrame() - Method in class org.orekit.bodies.Ellipsoid: Get the ellipsoid central frame.
getFrame(IERSConventions, boolean, DataContext) - Method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame: Get the frame corresponding to the CCSDS constant.
getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata: Get the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).
getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory: Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment: Get the reference frame for this ephemeris segment.
getFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment: Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment: Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris: Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
getFrame(Predefined) - Method in class org.orekit.frames.AbstractFrames
getFrame(Predefined) - Method in interface org.orekit.frames.Frames: Get one of the predefined frames.
getFrame(Predefined) - Static method in class org.orekit.frames.FramesFactory: Get one of the predefined frames.
getFrame() - Method in class org.orekit.frames.OrphanFrame: Get the associated frame.
getFrame() - Method in class org.orekit.gnss.clock.RinexClock: Get the reference frame for the station positions.
getFrame() - Method in interface org.orekit.models.earth.atmosphere.Atmosphere: Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.DTM2000: Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester: Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.JB2008: Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00: Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere: Get the frame of the central body.
getFrame() - Method in class org.orekit.orbits.FieldOrbit: Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.orbits.Orbit: Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.propagation.AbstractPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.Ephemeris
getFrame() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the frame of the initial state.
getFrame() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.events.FieldNodeDetector: Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector: Get the sensor reference frame.
getFrame() - Method in class org.orekit.propagation.events.NodeDetector: Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in interface org.orekit.propagation.FieldPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the defining frame.
getFrame() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
getFrame() - Method in class org.orekit.propagation.integration.FieldStateMapper: Get the inertial frame.
getFrame() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
getFrame() - Method in class org.orekit.propagation.integration.StateMapper: Get the inertial frame.
getFrame() - Method in interface org.orekit.propagation.Propagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the definition frame of the orbit.
getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the definition frame of the orbit.
getFrame() - Method in class org.orekit.propagation.SpacecraftState: Get the defining frame.
getFrame() - Method in class org.orekit.utils.AbsolutePVCoordinates: Get the frame in which the coordinates are defined.
getFrame() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates: Get the frame in which the coordinates are defined.
getFrameA() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints: Get frame A.
getFrameB() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints: Get frame B.
getFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata: Get epoch of reference frame, if not intrinsic to the definition of the reference frame.
getFrameName() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the frame name.
getFrames() - Method in class org.orekit.data.CompositeDataContext
getFrames() - Method in interface org.orekit.data.DataContext: Get a factory constructing Frames based on the auxiliary data in this context.
getFrames() - Method in class org.orekit.data.ExceptionalDataContext
getFrames() - Method in class org.orekit.data.LazyLoadedDataContext
getFrames() - Static method in class org.orekit.frames.FramesFactory: Get the instance of Frames that is called by the static methods in this class.
getFreeAmbiguityDrivers() - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver: Get the ambiguity parameters drivers that have not been fixed yet.
getFreeAmbiguityIndirection(int, List<ParameterDriver>) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver: Get ambiguity indirection array for ambiguity parameters drivers that have not been fixed yet.
getFreeEpochMap() - Method in class org.orekit.utils.AbstractMultipleShooting: Get the flags representing the free epoch of patch points.
getFreePatchPointMap() - Method in class org.orekit.utils.AbstractMultipleShooting: Get the flags representing the free components of patch points.
getFreeStateParameters() - Method in class org.orekit.estimation.measurements.modifiers.IonosphericGradientConverter: Get the number of free state parameters.
getFreeStateParameters() - Method in class org.orekit.estimation.measurements.modifiers.TroposphericGradientConverter: Get the number of free state parameters.
getFreeStateParameters() - Method in class org.orekit.propagation.integration.AbstractGradientConverter: Get the number of free state parameters.
getFreqOffset() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the freqOffset.
getFrequencies() - Method in class org.orekit.gnss.antenna.Antenna: Get supported frequencies.
getFrequency(SatelliteSystem) - Method in enum org.orekit.gnss.ObservationType: Get the frequency for a specified satellite system.
getFrequencyChannel() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac: Get the frequency channel.
getFrequencyNumber() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Getter for the frequency number.
getFrequencySource() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration: Get the frequency source.
getFrom() - Method in class org.orekit.utils.units.UnitsConverter: Get the source unit.
getFrozenFrame(Frame, AbsoluteDate, String) - Method in class org.orekit.frames.Frame: Get a new version of the instance, frozen with respect to a reference frame.
getFT() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS F_T Word.
getFunction() - Method in class org.orekit.propagation.events.FieldFunctionalDetector: Get the switching function.
getFunction() - Method in class org.orekit.propagation.events.FunctionalDetector: Get the switching function.
getFutureInfinity() - Method in class org.orekit.time.AbstractTimeScales
getFutureInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Dummy date at infinity in the future direction.
getFutureInfinity() - Method in interface org.orekit.time.TimeScales: Dummy date at infinity in the future direction.
getGalileoDataValidityStatus() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data: Get the Galileo data validity status.
getGalileoEpoch() - Method in class org.orekit.time.AbstractTimeScales
getGalileoEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
getGalileoEpoch() - Method in interface org.orekit.time.TimeScales: Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.
getGalileoNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data: Get the Galileo navigation message corresponding to the current RTCM data.
getGalileoNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data: Get the Galileo navigation message corresponding to the current RTCM data.
getGalileoNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation: Get all the Galileo navigation messages contained in the file.
getGalileoNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation: Get the Galileo navigation messages for the given satellite Id.
getGalileoToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data: Get the Galileo time of clock.
getGamma(LagrangianPoints) - Method in class org.orekit.bodies.CR3BPSystem: Get the position of the Lagrangian point in the CR3BP Rotating frame.
getGamma() - Method in class org.orekit.data.DelaunayArguments: Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.data.FieldDelaunayArguments: Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get direction cosine γ for central body.
getGammaDot() - Method in class org.orekit.data.DelaunayArguments: Get the tide parameter γ = GMST + π time derivative.
getGammaDot() - Method in class org.orekit.data.FieldDelaunayArguments: Get the tide parameter γ = GMST + π time derivative.
getGammaN() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Get the relative deviation of predicted satellite carrier frequency from nominal value.
getGammaN() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the relative deviation of predicted satellite carrier frequency from nominal value.
getGASTFunction(TimeScale, EOPHistory) - Method in enum org.orekit.utils.IERSConventions: Get the function computing Greenwich apparent sidereal time, in radians.
getGASTFunction(TimeScale, EOPHistory, TimeScales) - Method in enum org.orekit.utils.IERSConventions: Get the function computing Greenwich apparent sidereal time, in radians.
getGCRF() - Method in class org.orekit.frames.AbstractFrames
getGCRF() - Method in interface org.orekit.frames.Frames: Get the unique GCRF frame.
getGCRF() - Static method in class org.orekit.frames.FramesFactory: Get the unique GCRF frame.
getGdop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get generalize Dilution Of Precision.
getGdop() - Method in class org.orekit.gnss.DOP: Gets the geometric dilution of precision.
getGeneralEclipseAngles(Vector3D, Vector3D, double, Vector3D, double) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Get the useful angles for eclipse computation.
getGeneralEclipseAngles(FieldVector3D<T>, FieldVector3D<T>, T, FieldVector3D<T>, T) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Get the useful angles for eclipse computation.
getGeneralEclipseRatio(Vector3D, Vector3D, double, Vector3D, double) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get eclipse ratio between to bodies seen from a specific object.
getGeneralEclipseRatio(FieldVector3D<T>, FieldVector3D<T>, T, FieldVector3D<T>, T) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get eclipse ratio between to bodies seen from a specific object.
getGenerateCalls() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the number of calls to the generate method.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.EphemerisGenerator: Get the ephemeris generated during the propagation.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.FieldEphemerisGenerator: Get the ephemeris generated during the propagation.
getGenerator() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the hardware or software generator.
getGenerator() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the generator.
getGeoMagneticFields() - Method in class org.orekit.data.CompositeDataContext
getGeoMagneticFields() - Method in interface org.orekit.data.DataContext: Get a factory constructing GeoMagneticFields based on the auxiliary data in this context.
getGeoMagneticFields() - Method in class org.orekit.data.ExceptionalDataContext
getGeoMagneticFields() - Method in class org.orekit.data.LazyLoadedDataContext
getGeoMagneticFields() - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory: Get the instance of GeoMagneticFields that is called by methods in this class.
getGeometryFreeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory: Get the Geometry-Free combination of measurements.
getGetNeighborsCalls() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the number of calls to the GenericTimeStampedCache.getNeighbors(AbsoluteDate) method.
getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the G_js coefficient.
getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the G_js coefficient.
getGlo2UTC() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac: Get the correction from GLONASS to UTC.
getGLONASS() - Method in class org.orekit.time.LazyLoadedTimeScales
getGLONASS() - Method in interface org.orekit.time.TimeScales: Get the GLObal NAvigation Satellite System time scale.
getGLONASS() - Static method in class org.orekit.time.TimeScalesFactory: Get the GLObal NAvigation Satellite System time scale.
getGlonassEpoch() - Method in class org.orekit.time.AbstractTimeScales
getGlonassEpoch() - Method in interface org.orekit.time.TimeScales: Reference epoch for GLONASS four-year interval number: 1996-01-01T00:00:00 GLONASS time.
getGlonassNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the Glonass navigation message corresponding to the current RTCM data.
getGlonassNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the Glonass navigation message corresponding to the current RTCM data.
getGlonassNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation: Get all the Glonass navigation messages contained in the file.
getGlonassNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation: Get the Glonass navigation messages for the given satellite Id.
getGLONASSOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator: Gets the underlying GLONASS orbital elements.
getGLONASSOrbitalElements() - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator: Gets the underlying GLONASS orbital elements.
getGloOffset() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac: Get the correction of time relative to GLONASS system time.
getGM() - Method in interface org.orekit.bodies.CelestialBody: Get the attraction coefficient of the body.
getGm() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get gravitational coefficient of attracting body.
getGM() - Method in class org.orekit.models.earth.ReferenceEllipsoid: Gets the gravitational parameter that is part of the definition of the reference ellipsoid.
getGM() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttractionContext: Get standard gravitational parameter μ for the body in m³/s².
getGM() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTNewtonianAttractionContext: Get standard gravitational parameter μ for the body in m³/s².
getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the G_ms^j coefficient.
getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the G_ms^j coefficient.
getGMST(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
getGMST() - Method in class org.orekit.time.GLONASSDate: Get the Greenwich Mean Sidereal Time.
getGMST(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
getGMST(IERSConventions, boolean) - Method in interface org.orekit.time.TimeScales: Get the Greenwich Mean Sidereal Time scale.
getGMST(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory: Get the Greenwich Mean Sidereal Time scale.
getGMSTFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions: Get the function computing Greenwich mean sidereal time, in radians.
getGMSTFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions: Get the function computing Greenwich mean sidereal time, in radians.
getGMSTRateFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions: Get the function computing Greenwich mean sidereal time rate, in radians per second.
getGMSTRateFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions: Get the function computing Greenwich mean sidereal time rate, in radians per second.
getGnssIod() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data: Get the GNSS IOD.
getGnssIod() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data: Get the GNSS IOD.
getGnssNb() - Method in class org.orekit.gnss.DOP: Gets the number of GNSS satellites taken into account for DOP computation.
getGPS() - Method in class org.orekit.time.LazyLoadedTimeScales
getGPS() - Method in interface org.orekit.time.TimeScales: Get the Global Positioning System scale.
getGPS() - Static method in class org.orekit.time.TimeScalesFactory: Get the Global Positioning System scale.
getGPS2Glo() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac: Get the correction to GPS time relative GLONASS.
getGpsCodeOnL2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data: Get the GPS code on L2.
getGpsEpoch() - Method in class org.orekit.time.AbstractTimeScales
getGPSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
getGpsEpoch() - Method in interface org.orekit.time.TimeScales: Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
getGpsFitInterval() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data: Get the GPS fit interval.
getGpsL2PDataFlag() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data: Get the GPS L2 P-Code data flag.
getGpsNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data: Get the GPS navigation message corresponding to the current RTCM data.
getGpsNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data: Get the GPS navigation message corresponding to the current RTCM data.
getGPSNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation: Get all the GPS navigation messages contained in the file.
getGPSNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation: Get the GPS navigation messages for the given satellite Id.
getGpsToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data: Get the GPS time of clock.
getGpsWeek() - Method in class org.orekit.files.sp3.SP3: Returns the GPS week as contained in the SP3 file.
getGradientConverter() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester: Get the gradient converter related to the analytical orbit propagator.
getGradientDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D<Gradient>) - Method in class org.orekit.forces.drag.AbstractDragForceModel: Compute density and its derivatives.
getGRAPHICCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory: Get the GRAPHIC combination of measurements.
getGravitationalAssist() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get the origin of gravitational assist.
getGravityDegree() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get degree of the gravity model.
getGravityFields() - Method in class org.orekit.data.CompositeDataContext
getGravityFields() - Method in interface org.orekit.data.DataContext: Get a factory constructing gravity fields based on the auxiliary data in this context.
getGravityFields() - Method in class org.orekit.data.ExceptionalDataContext
getGravityFields() - Method in class org.orekit.data.LazyLoadedDataContext
getGravityFields() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the instance of GravityFields that is called by the static methods of this class.
getGravityModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get gravity model name.
getGravityOrder() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get order of the gravity model.
getGridPoints() - Method in class org.orekit.frames.InterpolatingTransformProvider: Get the number of interpolation grid points.
getGridPoints() - Method in class org.orekit.frames.ShiftingTransformProvider: Get the number of interpolation grid points.
getGridPoints(T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldFixedNumberInterpolationGrid: Get grid points that are within the current step.
getGridPoints(T, T) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.FieldInterpolationGrid: Get grid points that are within the current step.
getGridPoints(T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldMaxGapInterpolationGrid: Get grid points that are within the current step.
getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid: Get grid points that are within the current step.
getGridPoints(double, double) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.InterpolationGrid: Get grid points that are within the current step.
getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid: Get grid points that are within the current step.
getGrs80(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid: Get the GRS80 ellipsoid, attached to the given body frame.
getGST() - Method in class org.orekit.time.LazyLoadedTimeScales
getGST() - Method in interface org.orekit.time.TimeScales: Get the Galileo System Time scale.
getGST() - Static method in class org.orekit.time.TimeScalesFactory: Get the Galileo System Time scale.
getGTOD(boolean) - Method in class org.orekit.frames.AbstractFrames
getGTOD(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
getGTOD(boolean) - Method in interface org.orekit.frames.Frames: Get the GTOD reference frame.
getGTOD(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames: Get the GTOD reference frame.
getGTOD(boolean) - Static method in class org.orekit.frames.FramesFactory: Get the GTOD reference frame.
getGTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the GTOD reference frame.
getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the y component of eccentricity vector.
getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the y component of eccentricity vector.
getHalfAperture() - Method in class org.orekit.geometry.fov.CircularFieldOfView: get the FOV half aperture angle.
getHalfApertureAlongX() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView: get the FOV half aperture angle for spreading along X_ell (i.e.
getHalfApertureAlongY() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView: get the FOV half aperture angle for spreading along Y_ell (i.e.
getHaloOrbitalPeriod(double) - Method in class org.orekit.orbits.RichardsonExpansion: Return the orbital period of the Halo Orbit.
getHandler() - Method in class org.orekit.propagation.events.AbstractDetector: Get the handler.
getHandler() - Method in class org.orekit.propagation.events.FieldAbstractDetector: Get the handler.
getHandlers() - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler: Retrieve managed handlers list.
getHandlers() - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer: Get an unmodifiable view of all handlers.
getHandlers() - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer: Get an unmodifiable view of all handlers.
getHarmonicAmplitude() - Method in class org.orekit.utils.SecularAndHarmonic: Get an upper bound of the fitted harmonic amplitude.
getHarvester() - Method in class org.orekit.propagation.AbstractPropagator: Get the harvester.
getHasCreatableBody() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata: Get boolean testing whether the body corresponding to the centerName attribute can be created through the CelestialBodies.
getHdop() - Method in class org.orekit.gnss.DOP: Gets the horizontal dilution of precision.
getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent: Get the header.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ilrs.CPF: Get the CPF file header.
getHeader() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the header of the current data block.
getHeader() - Method in class org.orekit.gnss.CombinedObservationDataSet: Get the Rinex header associated with this data set.
getHeader() - Method in class org.orekit.gnss.metric.messages.ssr.SsrMessage: Get the header.
getHeader() - Method in class org.orekit.gnss.ObservationDataSet: Get the Rinex header associated with this data set.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Getter for the health status.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac: Gets the Health status.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac: Get the Health status.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Gets the Health status.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac: Gets the Health status.
getHealthE1() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac: Gets the E1-B/C signal health status.
getHealthE5a() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac: Gets the E5a signal health status.
getHealthE5b() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac: Gets the E5b signal health status.
getHeightIonosphericLayer() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data: Get the height of the ionospheric layer.
getHighRateClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data: Get the high rate clock correction to be added to the polynomial clock correction.
getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the H_js coefficient.
getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the H_js coefficient.
getHK() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get h * k.
getHK() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get h * k.
getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials: Get the H_ms^j coefficient.
getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the H_ms^j coefficient.
getHorizontalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements: Returns the horizontal intensity of the magnetic field (= norm of the vector in the plane spanned by the x/y components of the field vector).
getHost() - Method in class org.orekit.gnss.metric.ntrip.NtripClient: Get the caster host.
getHostOrIPAddress() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Get the host or IP address.
getHour() - Method in class org.orekit.time.TimeComponents: Get the hour number.
getHumidity() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement: Get the relative humidity at the surface.
getHumiSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Get the humidity sensor manufacturer.
getHumiSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Get the humidity sensor model.
getHumiSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Get the humidity sensor serial number.
getHx() - Method in class org.orekit.orbits.CartesianOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.KeplerianOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.Orbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the first component of the inclination vector (as per equinoctial parameters).
getHx() - Method in class org.orekit.propagation.SpacecraftState: Get the first component of the inclination vector (as per equinoctial parameters).
getHxDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.Orbit: Get the first component of the inclination vector derivative.
getHXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get hXXX = h * Χ³.
getHXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get hXXX = h * Χ³.
getHy() - Method in class org.orekit.orbits.CartesianOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.KeplerianOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.Orbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the second component of the inclination vector (as per equinoctial parameters).
getHy() - Method in class org.orekit.propagation.SpacecraftState: Get the second component of the inclination vector (as per equinoctial parameters).
getHyDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.Orbit: Get the second component of the inclination vector derivative.
getI() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Get the orbit inclination.
getI() - Method in class org.orekit.orbits.CartesianOrbit: Get the inclination.
getI() - Method in class org.orekit.orbits.CircularOrbit: Get the inclination.
getI() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the inclination.
getI() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the inclination.
getI() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the inclination.
getI() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the inclination.
getI() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the inclination.
getI() - Method in class org.orekit.orbits.FieldOrbit: Get the inclination.
getI() - Method in class org.orekit.orbits.KeplerianOrbit: Get the inclination.
getI() - Method in class org.orekit.orbits.Orbit: Get the inclination.
getI() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the inclination.
getI() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the inclination.
getI() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the inclination.
getI() - Method in class org.orekit.propagation.SpacecraftState: Get the inclination.
getI0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the inclination angle at reference time.
getI0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Inclination Angle at Reference Time.
getI11() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Get the moment of Inertia about the 1-axis (N.m²).
getI12() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Get the moment of Inertia about the 1 and 2 axes (N.m²).
getI13() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Get the moment of Inertia about the 1 and 3 axes (N.m²).
getI22() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Get the moment of Inertia about the 2-axis (N.m²).
getI23() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Get the moment of Inertia about the 2 and 3 axes (N.m²).
getI33() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Get the moment of Inertia about the 3-axis (N.m²).
getICRF() - Method in class org.orekit.frames.AbstractFrames
getICRF() - Method in interface org.orekit.frames.Frames: Get the unique ICRF frame.
getICRF() - Static method in class org.orekit.frames.FramesFactory: Get the unique ICRF frame.
getId() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris: Get the satellite ID.
getId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris: Get the satellite ID.
getId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get identification number.
getId() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris: Get the satellite ID.
getId() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris: Get the satellite ID.
getId() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris: Get the satellite ID.
getId() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris: Get the satellite ID.
getId() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris: Get the satellite ID.
getId() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris: Get the satellite ID.
getId() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
getId() - Method in class org.orekit.gnss.metric.ntrip.StreamedMessage: Get message id.
getIdentifier() - Method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter: Get the regular expression for identifying line.
getIdentity(Field<T>) - Static method in class org.orekit.frames.FieldTransform: Get the identity transform.
getIdentity(Field<T>) - Static method in class org.orekit.utils.FieldAngularCoordinates: Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).
getIDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.CircularOrbit: Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldOrbit: Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.Orbit: Get the inclination derivative.
getIDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac: Getter for the rate of inclination angle.
getIDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Getter for the rate of inclination angle.
getIDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Rate of Inclination Angle.
getIers2003(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid: Get the IERS2003 ellipsoid, attached to the given body frame.
getIers2010(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid: Get the IERS2010 ellipsoid, attached to the given body frame.
getIers96(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid: Get the IERS96 ellipsoid, attached to the given body frame.
getIGRF(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory: Get the IGRF model for the given year.
getIGRF(double) - Method in interface org.orekit.models.earth.GeoMagneticFields: Get the IGRF model for the given year.
getIGRF(double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the I_js coefficient.
getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the I_js coefficient.
getIlrsSatelliteId() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the IRLS satellite ID (based on COSPAR ID).
getImaginary(int, int) - Method in class org.orekit.utils.LoveNumbers: Get the imaginary part of a nominal Love numbers.
getInclination() - Method in class org.orekit.models.earth.GeoMagneticElements: Returns the inclination of the magnetic field in radians.
getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter: Get the increasing events time shift.
getIndicator() - Method in enum org.orekit.files.ilrs.CRDHeader.RangeType: Get the range type indicator.
getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Get the inertial velocity increment of the maneuver.
getInertialFrame() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment: Get the inertial reference frame for this ephemeris segment.
getInertialFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment: Get the inertial reference frame for this ephemeris segment.
getInertialFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment: Get the inertial reference frame for this ephemeris segment.
getInertialFrame() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Get the inertial frame in which the velocity increment is defined.
getInertiallyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody: Get an inertially oriented, body centered frame.
getInertiaMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the inertia matrix.
getInertiaReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Get the coordinate system for the inertia tensor.
getInitialCovarianceMatrix(SpacecraftState) - Method in class org.orekit.estimation.sequential.AbstractCovarianceMatrixProvider: Get the initial covariance matrix.
getInitialCovarianceMatrix(SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider: Get the initial covariance matrix.
getInitialFlowrate() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
getInitialIntegrationState() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Get the initial state for integration.
getInitialJacobianColumn(String) - Method in class org.orekit.propagation.AbstractMatricesHarvester: Get the initial column of Jacobian matrix with respect to named parameter.
getInitialOrbitDate() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the date of the initial orbit.
getInitialOrbitDate() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Get the date of the initial orbit.
getInitialPV() - Method in class org.orekit.orbits.LibrationOrbit: Return the initialPV on the libration orbit.
getInitialState() - Method in class org.orekit.propagation.AbstractPropagator: Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.AdapterPropagator: Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
getInitialState() - Method in class org.orekit.propagation.analytical.Ephemeris: Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.FieldPropagator: Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.Propagator: Get the propagator initial state.
getInitialStateTransitionMatrix() - Method in class org.orekit.propagation.AbstractMatricesHarvester: Get the initial State Transition Matrix.
getInitialThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
getInitialWetMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the total mass at beginning of life.
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
getInputs() - Method in class org.orekit.data.AbstractListCrawler: Get the list of inputs supported by the instance.
getInstantFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Get the value of the instantaneous solar flux.
getInstantFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: Get the value of the instantaneous solar flux.
getInstantFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters: Get the value of the instantaneous solar flux.
getIntegrationInterval() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the integrationInterval.
getIntegrationRef() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the integrationRef.
getIntegrator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the integrator used by the propagator.
getIntegrator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get the integrator used by the propagator.
getIntegratorBuilder() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder: Get the integrator builder.
getIntegratorBuilder() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Get the integrator builder.
getInternationalDesignator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the international designator for the object.
getInterpMethodEOP() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the interpolation method for Earth Orientation Parameters.
getInterpMethodSW() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get the interpolation method for Space Weather data.
getInterpolatedPoint(double, double) - Method in class org.orekit.models.earth.tessellation.Tile: Get an interpolated point inside the tile.
getInterpolatedState(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator: Get the state at interpolated date.
getInterpolatedState(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Get the state at interpolated date.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get the interpolation degree.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get the interpolation degree.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata: Get the interpolation degree.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Get the interpolation degree.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment: Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata: Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Get the interpolation method to be used.
getInterpolationMethod() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment: Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment: Get the interpolation method to be used.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment: Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory: Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment: Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment: Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment: Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment: Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment: Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris: Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape: Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape: Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid: Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid: Get the intersection point of a line with the surface of the body.
getInterval() - Method in class org.orekit.gnss.RinexObservationHeader: Get the observation interval in seconds.
getIntervalNumber() - Method in class org.orekit.time.GLONASSDate: Get the number of the current four year interval.
getInverse() - Method in class org.orekit.frames.FieldTransform: Get the inverse transform of the instance.
getInverse() - Method in class org.orekit.frames.Transform: Get the inverse transform of the instance.
getIOD() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac: Gets the Issue of Data (IOD).
getIOD() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Gets the GLONASS Issue Of Data (IOD).
getIODC() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage: Getter for the Issue Of Data Clock (IODC).
getIODC() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage: Getter for the Issue Of Data Clock (IODC).
getIODE() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage: Getter for the Issue Of Data Ephemeris (IODE).
getIODE() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage: Getter for the Issue Of Data Ephemeris (IODE).
getIODEC() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage: Getter for the Issue Of Data Ephemeris and Clock (IODEC).
getIODN() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Gets the Issue Of Data Navigation (IODN).
getIODN() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Gets the Issue Of Data Navigation (IODN).
getIODNav() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Getter for the the Issue Of Data (IOD).
getIodSsr() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader: Get the IOD SSR.
getIonosphereFreeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory: Get the Ionosphere-Free combination of measurements.
getIonosphericCorrectionType() - Method in class org.orekit.gnss.navigation.RinexNavigation: Getter for the ionospheric correction type.
getIonosphericModel() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201: Get the ionospheric model adapted to the current IM201 message.
getIRNSS() - Method in class org.orekit.time.LazyLoadedTimeScales
getIRNSS() - Method in interface org.orekit.time.TimeScales: Get the Indian Regional Navigation Satellite System time scale.
getIRNSS() - Static method in class org.orekit.time.TimeScalesFactory: Get the Indian Regional Navigation Satellite System time scale.
getIrnssEpoch() - Method in class org.orekit.time.AbstractTimeScales
getIrnssEpoch() - Method in interface org.orekit.time.TimeScales: Reference epoch for IRNSS weeks: 1999-08-22T00:00:00 IRNSS time.
getIRNSSNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation: Get all the IRNSS navigation messages contained in the file.
getIRNSSNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation: Get the IRNSS navigation messages for the given satellite Id.
getISP() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver: Get the specific impulse.
getISP() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the specific impulse.
getIsp() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Get the specific impulse.
getIsp() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the specific impulse.
getIsp(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the specific impulse (s).
getIteration() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the iteration number.
getIterationsCount() - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel: Get the iterations count.
getIterationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Get the number of iterations used for last estimation.
getITRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
getITRF(ITRFVersion, IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
getITRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames: Get an unspecified International Terrestrial Reference Frame.
getITRF(ITRFVersion, IERSConventions, boolean) - Method in interface org.orekit.frames.Frames: Get an specific International Terrestrial Reference Frame.
getITRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get an unspecified International Terrestrial Reference Frame.
getITRF(ITRFVersion, IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get an specific International Terrestrial Reference Frame.
getITRFEquinox(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
getITRFEquinox(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames: Get the equinox-based ITRF reference frame.
getITRFEquinox(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the equinox-based ITRF reference frame.
getITRFType() - Method in class org.orekit.frames.EOPEntry: Get the ITRF version this entry defines.
getITRFVersion(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the ITRF version.
getITRFVersion(int) - Static method in enum org.orekit.frames.ITRFVersion: Find an ITRF version from its reference year.
getITRFVersion(String) - Static method in enum org.orekit.frames.ITRFVersion: Find an ITRF version from its name.
getITRFVersion() - Method in class org.orekit.frames.VersionedITRF: Get the ITRF version.
getJ2000Day() - Method in class org.orekit.time.DateComponents: Get the day number with respect to J2000 epoch.
getJ2000Epoch() - Method in class org.orekit.time.AbstractTimeScales
getJ2000Epoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
getJ2000Epoch() - Method in interface org.orekit.time.TimeScales: J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
getJacobian(Orbit, PositionAngle, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Compute the Jacobian of the orbit with respect to maneuver parameters.
getJacobian(CartesianDerivativesFilter, T[][]) - Method in class org.orekit.frames.FieldTransform: Compute the Jacobian of the FieldTransform.transformPVCoordinates(FieldPVCoordinates) method of the transform.
getJacobian(CartesianDerivativesFilter, double[][]) - Method in class org.orekit.frames.Transform: Compute the Jacobian of the Transform.transformPVCoordinates(PVCoordinates) method of the transform.
getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester: Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper: Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in interface org.orekit.propagation.MatricesHarvester: Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester: Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobiansColumnsNames() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Get the names of the parameters in the matrix returned by MatricesHarvester.getParametersJacobian(org.orekit.propagation.SpacecraftState).
getJacobianWrtCartesian(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit: Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit: Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtParameters(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit: Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJacobianWrtParameters(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit: Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJavaEpoch() - Method in class org.orekit.time.AbstractTimeScales
getJavaEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
getJavaEpoch() - Method in interface org.orekit.time.TimeScales: Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
getJD0() - Method in class org.orekit.time.GLONASSDate: Get the current Julian date JD0.
getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials: Get the J_js coefficient.
getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the J_js coefficient.
getJulianDay() - Method in class org.orekit.files.sp3.SP3: Returns the julian day for this SP3 file.
getJulianEpoch() - Method in class org.orekit.time.AbstractTimeScales
getJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
getJulianEpoch() - Method in interface org.orekit.time.TimeScales: Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
getJupiter() - Method in interface org.orekit.bodies.CelestialBodies: Get the Jupiter singleton body.
getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Jupiter singleton body.
getJupiter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
getJupiterSemiMajorAxis(AbsoluteDate, TimeScale) - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants: Get the Jupiter semi-major axis.
getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the x component of eccentricity vector.
getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the x component of eccentricity vector.
getK2MH2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get k² - h².
getK2MH2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get k² - h².
getK2MH2O2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get (k² - h²) / 2.
getK2MH2O2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get (k² - h²) / 2.
getKeplerianElementsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData: Get the Keplerian elements logical block.
getKeplerianElementsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData: Get the Keplerian elements logical block.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.FieldOrbit: Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.Orbit: Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.SpacecraftState: Get the Keplerian mean motion.
getKeplerianPeriod() - Method in class org.orekit.orbits.FieldOrbit: Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.orbits.Orbit: Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.SpacecraftState: Get the Keplerian period.
getKey() - Method in enum org.orekit.gnss.clock.RinexClock.ClockDataType: Get the key for the system.
getKey() - Method in enum org.orekit.gnss.SatelliteSystem: Get the key for the system.
getKey() - Method in enum org.orekit.gnss.TimeSystem: Get the key for the system.
getKey() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry: Get the entry key.
getKey() - Method in class org.orekit.utils.FieldArrayDictionary.Entry: Get the entry key.
getKlobucharAlpha() - Method in class org.orekit.gnss.navigation.RinexNavigation: Get the "alpha" ionospheric parameters.
getKlobucharBeta() - Method in class org.orekit.gnss.navigation.RinexNavigation: Get the "beta" ionospheric parameters.
getKpSum() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the sum of all eight Kp indices for the current entry.
getKXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get kXXX = h * Χ³.
getKXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get kXXX = h * Χ³.
getL() - Method in class org.orekit.data.DelaunayArguments: Get the mean anomaly of the Moon.
getL() - Method in class org.orekit.data.FieldDelaunayArguments: Get the mean anomaly of the Moon.
getL(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit: Get the longitude argument.
getL(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the longitude argument.
getLabel() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame: Get the frame label.
getLagrangianPoint() - Method in class org.orekit.orbits.RichardsonExpansion: Get the considered lagrangian point.
getLambda() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
getLambda() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the longitude of ascending node of orbit.
getLaserId() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Get the laser configuration ID.
getLaserRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration: Get the laser configuration record.
getLaserType() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Get the laser type.
getLastDailyPredictedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader: Gets the day (at data start) of the last daily data entry.
getLastEstimations() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Get the last estimations performed.
getLastKnownLeapSecond() - Method in class org.orekit.time.UTCScale: Get the date of the last known leap second.
getLastObservedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader: Gets the day (at data start) of the last observed data entry.
getLastSpan() - Method in class org.orekit.utils.TimeSpanMap: Get the last (latest) span.
getLastTransition() - Method in class org.orekit.utils.TimeSpanMap: Get the last (latest) transition.
getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the latest cached entry.
getLatest() - Method in class org.orekit.utils.ImmutableTimeStampedCache: Get the latest entry in this cache.
getLatest() - Method in interface org.orekit.utils.TimeStampedCache: Get the latest entry in this cache.
getLatitude() - Method in class org.orekit.bodies.FieldGeodeticPoint: Get the latitude.
getLatitude() - Method in class org.orekit.bodies.GeodeticPoint: Get the latitude.
getLatitude() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Get the latitude.
getLatitude() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the latitude.
getLatitude() - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector: Get the fixed latitude to be crossed (radians).
getLatitude() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector: Get the fixed latitude to be crossed (radians).
getLaunchNumber() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata: Get the launch number.
getLaunchNumber() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata: Get the launch number.
getLaunchNumber(String) - Method in class org.orekit.files.ccsds.section.Metadata: Get the launch number.
getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the launch number.
getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the launch number.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata: Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata: Get the piece of launch.
getLaunchPiece(String) - Method in class org.orekit.files.ccsds.section.Metadata: Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the launch piece.
getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the launch piece.
getLaunchYear() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata: Get the launch year.
getLaunchYear() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata: Get the launch year.
getLaunchYear(String) - Method in class org.orekit.files.ccsds.section.Metadata: Get the launch year.
getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the launch year.
getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the launch year.
getLDot() - Method in class org.orekit.data.DelaunayArguments: Get the mean anomaly of the Moon time derivative.
getLDot() - Method in class org.orekit.data.FieldDelaunayArguments: Get the mean anomaly of the Moon time derivative.
getLDot(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit: Get the longitude argument derivative.
getLDot(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the longitude argument derivative.
getLE() - Method in class org.orekit.data.BodiesElements: Get the mean Earth longitude.
getLE() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Earth longitude.
getLE() - Method in class org.orekit.orbits.CartesianOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.CircularOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.KeplerianOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.Orbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the eccentric latitude argument (as per equinoctial parameters).
getLe() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the eccentric longitude.
getLE() - Method in class org.orekit.propagation.SpacecraftState: Get the eccentric latitude argument (as per equinoctial parameters).
getLeap() - Method in class org.orekit.files.ilrs.CPF.CPFCoordinate: Get the leap second flag (= 0 or the value of the new leap second).
getLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale: Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale: Get the value of the previous leap.
getLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale: Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale: Get the value of the previous leap.
getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale: Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale: Get the value of the previous leap.
getLeap() - Method in class org.orekit.time.UTCTAIOffset: Get the value of the leap at offset validity start (in seconds).
getLeapSeconds() - Method in class org.orekit.gnss.RinexObservationHeader: Get the Number of leap seconds since 6-Jan-1980.
getLeapSecondsDayNum() - Method in class org.orekit.gnss.RinexObservationHeader: Get the respective leap second day number.
getLeapSecondsFuture() - Method in class org.orekit.gnss.RinexObservationHeader: Get the future or past leap seconds.
getLeapSecondsWeekNum() - Method in class org.orekit.gnss.RinexObservationHeader: Get the respective leap second week number.
getLEDot() - Method in class org.orekit.data.BodiesElements: Get the mean Earth longitude time derivative.
getLEDot() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Earth longitude time derivative.
getLEDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.CircularOrbit: Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldOrbit: Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.Orbit: Get the eccentric longitude argument derivative.
getLength() - Method in class org.orekit.utils.units.Unit: Get the length exponent.
getLf() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the eccentric longitude.
getLightingRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get the lighting ratio ([0-1]).
getLightingRatio(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get the lighting ratio ([0-1]).
getLine() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader: Get the last line read from the stream.
getLine1() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the first line.
getLine1() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the first line.
getLine2() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the second line.
getLine2() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the second line.
getLineNumber() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the number of the line in the CCSDS data message.
getLineNumber() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader: Get the line number of the last line read from the file.
getListAppliedDCBS() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the applied differential code bias corrections.
getListAppliedDCBS() - Method in class org.orekit.gnss.RinexObservationHeader: Get the list of applied differential code bias corrections.
getListAppliedPCVS() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the applied phase center variations.
getListAppliedPCVS() - Method in class org.orekit.gnss.RinexObservationHeader: Get the list of antenna center variation corrections.
getLJu() - Method in class org.orekit.data.BodiesElements: Get the mean Jupiter longitude.
getLJu() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Jupiter longitude.
getLJuDot() - Method in class org.orekit.data.BodiesElements: Get the mean Jupiter longitude time derivative.
getLJuDot() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Jupiter longitude time derivative.
getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Compute the limits in L, the true longitude, for integration.
getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Compute the limits in L, the true longitude, for integration.
getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Compute the limits in L, the true longitude, for integration.
getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Compute the limits in L, the true longitude, for integration.
getLM() - Method in class org.orekit.orbits.CartesianOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.CircularOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.KeplerianOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.Orbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the mean longitude argument (as per equinoctial parameters).
getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the mean longitude.
getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the mean longitude.
getLM() - Method in class org.orekit.propagation.SpacecraftState: Get the mean longitude argument (as per equinoctial parameters).
getLMa() - Method in class org.orekit.data.BodiesElements: Get the mean Mars longitude.
getLMa() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Mars longitude.
getLMaDot() - Method in class org.orekit.data.BodiesElements: Get the mean Mars longitude time derivative.
getLMaDot() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Mars longitude time derivative.
getLMDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.CircularOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.Orbit: Get the mean longitude argument derivative.
getLMe() - Method in class org.orekit.data.BodiesElements: Get the mean Mercury longitude.
getLMe() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Mercury longitude.
getLMeDot() - Method in class org.orekit.data.BodiesElements: Get the mean Mercury longitude time derivative.
getLMeDot() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Mercury longitude time derivative.
getLNe() - Method in class org.orekit.data.BodiesElements: Get the mean Neptune longitude.
getLNe() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Neptune longitude.
getLNeDot() - Method in class org.orekit.data.BodiesElements: Get the mean Neptune longitude time derivative.
getLNeDot() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Neptune longitude time derivative.
getLNFifthString() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS l_n Word extracted from fifth string of the subframe.
getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients: Get the value of L_n^s(γ).
getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients: Get the value of L_n^s(γ).
getLNThirdString() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS l_n Word extracted from third string of the subframe.
getLoadedAstronomicalUnit() - Method in class org.orekit.bodies.JPLEphemeridesLoader: Get astronomical unit.
getLoadedConstant(String...) - Method in class org.orekit.bodies.JPLEphemeridesLoader: Get a constant defined in the ephemerides headers.
getLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager: Get an unmodifiable view of the set of data file names that have been loaded.
getLoadedEarthMoonMassRatio() - Method in class org.orekit.bodies.JPLEphemeridesLoader: Get Earth/Moon mass ratio.
getLoadedGravitationalCoefficient(JPLEphemeridesLoader.EphemerisType) - Method in class org.orekit.bodies.JPLEphemeridesLoader: Get the gravitational coefficient of a body.
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitInternalError
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIOException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitParseException
getLocalizedString(Locale) - Method in enum org.orekit.errors.OrekitMessages
getLocalTimingId() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration: Get the local timing system configuration ID.
getLocation() - Method in class org.orekit.gnss.DOP: Gets the location with respect to the Earth where DOP was calculated.
getLOD() - Method in class org.orekit.frames.EOPEntry: Get the LoD (Length of Day) value.
getLOD(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the LoD (Length of Day) value.
getLOD(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory: Get the LoD (Length of Day) value.
getLofCartesianOrbitalParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise: Getter for the lofCartesianOrbitalParametersEvolution.
getLofType() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise: Getter for the lofType.
getLofType() - Method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame: Get the type of Local Orbital frame.
getLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger: Get an immutable copy of the logged events.
getLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger: Get an immutable copy of the logged events.
getLongitude() - Method in class org.orekit.bodies.FieldGeodeticPoint: Get the longitude.
getLongitude() - Method in class org.orekit.bodies.GeodeticPoint: Get the longitude.
getLongitude() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Get the longitude.
getLongitude() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the longitude.
getLongitude() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector: Get the fixed longitude to be crossed (radians).
getLossOfLockIndicator() - Method in class org.orekit.gnss.ObservationData: Get the Loss of Lock Indicator.
getLoveNumbers() - Method in enum org.orekit.utils.IERSConventions: Get the Love numbers.
getLowElevationThreshold() - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel: Get the low elevation threshold value for path delay computation.
getLowerCaseAbbreviation() - Method in enum org.orekit.time.Month: Get the lower case three letters abbreviation.
getLowerCaseName() - Method in enum org.orekit.time.Month: Get the lower case full name.
getLowReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Get a reference to the lower triangular matrix of the decomposition.
getLPosition(LagrangianPoints) - Method in class org.orekit.bodies.CR3BPSystem: Get the position of the Lagrangian point in the CR3BP Rotating frame.
getLPrime() - Method in class org.orekit.data.DelaunayArguments: Get the mean anomaly of the Sun.
getLPrime() - Method in class org.orekit.data.FieldDelaunayArguments: Get the mean anomaly of the Sun.
getLPrimeDot() - Method in class org.orekit.data.DelaunayArguments: Get the mean anomaly of the Sun time derivative.
getLPrimeDot() - Method in class org.orekit.data.FieldDelaunayArguments: Get the mean anomaly of the Sun time derivative.
getLSa() - Method in class org.orekit.data.BodiesElements: Get the mean Saturn longitude.
getLSa() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Saturn longitude.
getLSaDot() - Method in class org.orekit.data.BodiesElements: Get the mean Saturn longitude time derivative.
getLSaDot() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Saturn longitude time derivative.
getLst81Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the last 81-day arithmetic average of F10.7 (adjusted).
getLst81Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the last 81-day arithmetic average of F10.7 (observed).
getLUr() - Method in class org.orekit.data.BodiesElements: Get the mean Uranus longitude.
getLUr() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Uranus longitude.
getLUrDot() - Method in class org.orekit.data.BodiesElements: Get the mean Uranus longitude time derivative.
getLUrDot() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Uranus longitude time derivative.
getLv() - Method in class org.orekit.orbits.CartesianOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.CircularOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.KeplerianOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.Orbit: Get the true longitude argument.
getLv() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the true latitude argument (as per equinoctial parameters).
getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the true longitude.
getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the true longitude.
getLv() - Method in class org.orekit.propagation.SpacecraftState: Get the true latitude argument (as per equinoctial parameters).
getLvDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.CircularOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.Orbit: Get the true longitude argument derivative.
getLVe() - Method in class org.orekit.data.BodiesElements: Get the mean Venus longitude.
getLVe() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Venus longitude.
getLVeDot() - Method in class org.orekit.data.BodiesElements: Get the mean Venus longitude time derivative.
getLVeDot() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Venus longitude time derivative.
getLyapunovOrbitalPeriod(double) - Method in class org.orekit.orbits.RichardsonExpansion: Return the orbital period of the Halo Orbit.
getM() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS M Word.
getM0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the mean anomaly at reference time.
getM0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Mean Anomaly at Reference Time.
getM2() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Get the value of the M2 drag parameter.
getM2() - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Get the value of the M2 drag parameter.
getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get m2aoA = -2 * a / A.
getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get m2aoA = -2 * a / A.
getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get m2aoA = -2 * a / A.
getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get m2aoA = -2 * a / A.
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Get the differential equations to integrate (for main state only).
getManagedAdditionalStates() - Method in class org.orekit.propagation.AbstractPropagator: Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.analytical.Ephemeris: Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.FieldPropagator: Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.Propagator: Get all the names of all managed states.
getManBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get basis of this maneuver history data.
getManBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get identification number of the orbit determination or simulation upon which this maneuver is based.
getManComposition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get maneuver elements of information.
getManDeviceID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get identifier of the device used for this maneuver.
getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData: Get a maneuver.
getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Get a maneuver.
getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData: Get a maneuver.
getManeuverAttitudeProvider() - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider: Attitude provider to use.
getManeuverBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData: Get maneuvers logical blocks.
getManeuvers() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData: Get a list of all maneuvers.
getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistory: Get the maneuvers.
getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Get a list of all maneuvers.
getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData: Get a list of all maneuvers.
getManeuversFrequency() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the average frequency of orbit or attitude maneuvers (in SI units, hence per second).
getManeuversPerYear() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the average number of orbit or attitude maneuvers per year.
getManeuverTriggers() - Method in class org.orekit.forces.maneuvers.Maneuver: Get the maneuver triggers.
getManFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get epoch of the maneuver reference frame.
getManID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get maneuver identification number.
getManifolds(SpacecraftState, boolean) - Method in class org.orekit.orbits.LibrationOrbit: Return a manifold direction from one position on a libration Orbit.
getManNextEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get start time of next maneuver.
getManNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get identification number of next maneuver.
getManPredSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get prediction source on which this maneuver is based.
getManPrevEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get completion time of previous maneuver.
getManPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get identification number of previous maneuver.
getManPurpose() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get the purposes of the maneuver.
getManReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get reference frame of the maneuver.
getManufacturer() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get manufacturer name.
getManUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Get maneuver elements of information units.
getMapper() - Method in class org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations: Deprecated.

Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMapper() - Method in class org.orekit.propagation.numerical.AbsolutePartialDerivativesEquations: Deprecated.

Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMapper() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations: Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMapper() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Deprecated.

Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMapper() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations: Deprecated.

Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMappers() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Deprecated.
as of 11.1, not used anymore
getMargin() - Method in class org.orekit.geometry.fov.AbstractFieldOfView: Get the angular margin to apply (radians).
getMargin() - Method in interface org.orekit.geometry.fov.FieldOfView: Get the angular margin to apply (radians).
getMargin() - Method in class org.orekit.propagation.events.GeographicZoneDetector: Get the angular margin to apply (radians).
getMarkerName() - Method in class org.orekit.gnss.RinexObservationHeader: Get name of the antenna marker.
getMarkerNumber() - Method in class org.orekit.gnss.RinexObservationHeader: Get number of the antenna marker.
getMarkerType() - Method in class org.orekit.gnss.RinexObservationHeader: Get type of the antenna marker.
getMars() - Method in interface org.orekit.bodies.CelestialBodies: Get the Mars singleton body.
getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Mars singleton body.
getMars() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
getMass() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData: Get the mass.
getMass() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData: Get the mass.
getMass() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters: Get the spacecraft mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris: Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator: Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the mass.
getMass() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder: Get the mass.
getMass() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Get the mass.
getMass() - Method in class org.orekit.propagation.FieldSpacecraftState: Gets the current mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Get the mass.
getMass() - Method in class org.orekit.propagation.SpacecraftState: Gets the current mass.
getMass() - Method in class org.orekit.utils.units.Unit: Get the mass exponent.
getMassDepletionDelay() - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate: Get the mass depletion effect processor.
getMassDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel: Get the mass derivative (i.e.
getMassDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel: Get the mass derivative (i.e.
getMassDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the mass derivative (i.e.
getMassDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the mass derivative (i.e.
getMassRatio() - Method in class org.orekit.bodies.CR3BPSystem: Get the CR3BP mass ratio of the system mu2/(mu1+mu2).
getMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Covariance: Get the covariance matrix.
getMatrixLine(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix: Get a line of the matrix.
getMaxAlt() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester: Get the maximal altitude for the model.
getMaxAR3Pow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get the value of max power for a/R3 in the serie expansion.
getMaxAR3Pow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get the value of max power for a/R3 in the serie expansion.
getMaxAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the maximum cross-sectional area for collision probability estimation purposes.
getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the maximal degree available in the last file parsed.
getMaxAvailableOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the maximal order available in the last file parsed.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.AbstractDetector: Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.AdapterDetector: Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.EventDetector: Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.FieldAbstractDetector: Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.FieldEventDetector: Get maximal time interval between switching function checks.
getMaxChunksDuration() - Method in class org.orekit.bodies.JPLEphemeridesLoader: Get the maximal chunks duration.
getMaxDate() - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider: Get the last date of the range.
getMaxDate() - Method in interface org.orekit.attitudes.BoundedAttitudeProvider: Get the last date of the range.
getMaxDate() - Method in class org.orekit.attitudes.TabulatedLofOffset: Get the last date of the range.
getMaxDate() - Method in class org.orekit.attitudes.TabulatedProvider: Get the last date of the range.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader: Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters: Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters: Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
getMaxDate() - Method in class org.orekit.propagation.analytical.Ephemeris: Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator: Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator: Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Get the last date of the range.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the maximal supported degree.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave: Get the maximum supported degree.
getMaxDegree() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Get the maximal supported degree.
getMaxDistance() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Get the maximum of distance among the solutions found.
getMaxEccPow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get the value of max power for e in the serie expansion.
getMaxEccPow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get the value of max power for e in the serie expansion.
getMaxFreqF() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get the value of max frequency of F.
getMaxFreqF() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get the value of max frequency of F.
getMaximumObsGap() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get maximum time between observations in the OD of the object.
getMaxIterationCount() - Method in class org.orekit.propagation.events.AbstractDetector: Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.AdapterDetector: Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.EventDetector: Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.FieldAbstractDetector: Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.FieldEventDetector: Get maximal number of iterations in the event time search.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the maximal supported order.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave: Get the maximum supported order.
getMaxOrder() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Get the maximal supported order.
getMaxOrder() - Method in enum org.orekit.utils.AngularDerivativesFilter: Get the maximum derivation order.
getMaxOrder() - Method in enum org.orekit.utils.CartesianDerivativesFilter: Get the maximum derivation order.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Get the degree limit for the next file parsing.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the degree limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Get the order limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the order limit for the next file parsing.
getMaxPredictedEigenMaj() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get maximum predicted major eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
getMaxRcs() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the maximum radar cross-section.
getMaxSigma() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter: Get the value of the outlier detection limit.
getMaxSlots() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the maximum number of independent cached time slots.
getMaxSolution() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Get the maximum number of solutions seeked.
getMaxSpan() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the maximum duration span in seconds of one slot.
getMaxThrust() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the maximum composite thrust the spacecraft can accomplish.
getMaxTimeBeetween2Measurement() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector: Get the maximum time lapse between 2 measurements without considering a cycle-slip has occurring between both.
getMaxValue() - Method in class org.orekit.utils.ParameterDriver: Get maximum parameter value.
getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get mCo2AB = -C / 2AB.
getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get mCo2AB = -C / 2AB.
getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get mCo2AB = -C / 2AB.
getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get mCo2AB = -C / 2AB.
getMeanAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit: Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the mean anomaly.
getMeanAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the mean anomaly derivative.
getMeanAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the mean anomaly derivative.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState, AbstractGaussianContribution.GaussQuadrature, double, double, AbstractGaussianContributionContext, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(FieldSpacecraftState<T>, AbstractGaussianContribution.GaussQuadrature, T, T, FieldAbstractGaussianContributionContext<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementTheory() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata: Get the description of the Mean Element Theory.
getMeanFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Get the value of the mean solar flux.
getMeanFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: Get the value of the mean solar flux.
getMeanFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters: Get the value of the mean solar flux.
getMeanMotion() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Get the orbit mean motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac: Getter for the mean motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Getter for the mean motion.
getMeanMotion() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Mean Motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the mean motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext: Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext: Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the Keplerian mean motion.
getMeanMotionDot() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Get the first time derivative of the mean motion.
getMeanMotionDotDot() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Get the second time derivative of the mean motion.
getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the mean motion first derivative.
getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the mean motion first derivative.
getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the mean motion second derivative.
getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the mean motion second derivative.
getMeanObliquityFunction() - Method in enum org.orekit.utils.IERSConventions: Get the function computing mean obliquity of the ecliptic.
getMeanObliquityFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions: Get the function computing mean obliquity of the ecliptic.
getMeasurement() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation: Getter for the measurement.
getMeasurements() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement: Get the underlying measurements.
getMeasurementsParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Get the measurements parameters supported by this estimator (including measurements and modifiers).
getMeasurementsParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise: Getter for the measurementsParametersEvolution.
getMeasurementType() - Method in class org.orekit.gnss.CombinedObservationData: Get the measurement type.
getMeasurementType() - Method in enum org.orekit.gnss.ObservationType: Get the measurement type.
getMedianDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector: Get the driver for median date.
getMedianDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector: Get the driver for median date.
getMelbourneWubbenaCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory: Get the Melbourne-Wübbena combination of measurements.
getMercury() - Method in interface org.orekit.bodies.CelestialBodies: Get the Mercury singleton body.
getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Mercury singleton body.
getMercury() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
getMessage(Locale) - Method in interface org.orekit.errors.LocalizedException: Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitException: Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalArgumentException: Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalStateException: Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitInternalError: Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitInternalError
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIOException: Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitIOException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitParseException: Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitParseException
getMessageId() - Method in class org.orekit.files.ccsds.section.Header: Get the ID that uniquely identifies a message from a given originator.
getMessageType(String) - Method in class org.orekit.gnss.metric.parser.IgsSsrMessagesParser: Get the message type corresponding to the message number.
getMessageType(String) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType: Get the message type corresponding to a message number.
getMessageType(String) - Method in class org.orekit.gnss.metric.parser.MessagesParser: Get the message type corresponding to the message number.
getMessageType(String) - Method in class org.orekit.gnss.metric.parser.RtcmMessagesParser: Get the message type corresponding to the message number.
getMessageType(String) - Static method in enum org.orekit.gnss.metric.parser.RtcmMessageType: Get the message type corresponding to a message number.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm: Get the file metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistory: Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistory: Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm: Get the metadata from the single segment.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory: Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm: Get the file metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Get the file metadata.
getMetadata() - Method in class org.orekit.files.ccsds.section.Segment: Get the segment metadata.
getMeteo(AbsoluteDate) - Method in class org.orekit.files.ilrs.CRD.Meteo: Get the meteorological parameters at a given date.
getMeteoData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the meteorological data for the data block.
getMeteorologicalId() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Get the meteorological configuration ID.
getMeteorologicalRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration: Get the meteorological record.
getMethod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get orbit determination method.
getMHzFrequency() - Method in enum org.orekit.gnss.Frequency: Get the value of the frequency in MHz.
getMilliInWeek() - Method in class org.orekit.time.GNSSDate: Get the number of milliseconds since week start.
getMinAlt() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester: Get the minimal altitude for the model.
getMinAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the minimum cross-sectional area for collision probability estimation purposes.
getMinDate() - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider: Get the first date of the range.
getMinDate() - Method in interface org.orekit.attitudes.BoundedAttitudeProvider: Get the first date of the range.
getMinDate() - Method in class org.orekit.attitudes.TabulatedLofOffset: Get the first date of the range.
getMinDate() - Method in class org.orekit.attitudes.TabulatedProvider: Get the first date of the range.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader: Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters: Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters: Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
getMinDate() - Method in class org.orekit.propagation.analytical.Ephemeris: Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.BoundedPropagator: Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator: Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Get the first date of the range.
getMinElevation() - Method in class org.orekit.gnss.DOPComputer: Get the minimum elevation.
getMinElevation() - Method in class org.orekit.propagation.events.ElevationDetector: Returns the currently configured minimum valid elevation value.
getMinElevation() - Method in class org.orekit.propagation.events.FieldElevationDetector: Returns the currently configured minimum valid elevation value.
getMinMeasurementNumber() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector: Get the minimum number of measurement needed before being able to figure out cycle-slip occurrence.
getMinPredictedEigenMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get minimum predicted minor eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
getMinRcs() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the minimum radar cross-section.
getMinute() - Method in class org.orekit.time.TimeComponents: Get the minute number.
getMinutesFromUTC() - Method in class org.orekit.time.TimeComponents: Get the offset between the specified date and UTC.
getMinValue() - Method in class org.orekit.utils.ParameterDriver: Get minimum parameter value.
getMisc() - Method in class org.orekit.gnss.metric.ntrip.Record: Get miscellaneous information.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder: Get the mission reference date or Mission Elapsed Time or Mission Relative Time time systems.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.adm.AdmParser: Get reference date for Mission Elapsed Time and Mission Relative Time time systems.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser: Get reference date for Mission Elapsed Time and Mission Relative Time time systems.
getMjd() - Method in class org.orekit.frames.EOPEntry: Get the entry date (modified julian day, 00h00 UTC scale).
getMJD() - Method in class org.orekit.time.DateComponents: Get the modified julian day.
getMJD() - Method in class org.orekit.time.UTCTAIOffset: Get the date of the start of the leap as Modified Julian Day.
getMJDRef() - Method in class org.orekit.time.OffsetModel: Get the reference date of the linear model as a modified julian day.
getMoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get μ / a .
getMoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get μ / a .
getMOD(boolean) - Method in class org.orekit.frames.AbstractFrames
getMOD(IERSConventions) - Method in class org.orekit.frames.AbstractFrames
getMOD(boolean) - Method in interface org.orekit.frames.Frames: Get the MOD reference frame.
getMOD(IERSConventions) - Method in interface org.orekit.frames.Frames: Get the MOD reference frame.
getMOD(boolean) - Static method in class org.orekit.frames.FramesFactory: Get the MOD reference frame.
getMOD(IERSConventions) - Static method in class org.orekit.frames.FramesFactory: Get the MOD reference frame.
getMode() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the mode.
getModel() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the Jacobian of the function computing position/velocity at sample points.
getModel() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter: Get the Jacobian of the function computing position/velocity at sample points.
getModel() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter: Get the Jacobian of the function computing position/velocity at sample points.
getModelName() - Method in class org.orekit.models.earth.GeoMagneticField: Returns the model name.
getModels() - Method in class org.orekit.models.earth.GeoMagneticModelLoader: Returns a Collection of the GeoMagneticField models that have been successfully loaded.
getModifiedJulianEpoch() - Method in class org.orekit.time.AbstractTimeScales
getModifiedJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
getModifiedJulianEpoch() - Method in interface org.orekit.time.TimeScales: Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
getModifiedRodrigues(double) - Method in class org.orekit.utils.AngularCoordinates: Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.
getModifiedRodrigues(double) - Method in class org.orekit.utils.FieldAngularCoordinates: Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.
getModifiers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Get the modifiers that apply to a measurement.
getModifiers() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder: Get the modifiers that apply to a measurement.
getModifiers() - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder: Get the modifiers that apply to a measurement.
getModifiers() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Get the modifiers that apply to a measurement.
getMomentum() - Method in class org.orekit.utils.FieldPVCoordinates: Gets the momentum.
getMomentum() - Method in class org.orekit.utils.PVCoordinates: Gets the momentum.
getMonth() - Method in class org.orekit.time.DateComponents: Get the month.
getMonth(int) - Static method in enum org.orekit.time.Month: Get the month corresponding to a number.
getMonthEnum() - Method in class org.orekit.time.DateComponents: Get the month as an enumerate.
getMoon() - Method in interface org.orekit.bodies.CelestialBodies: Get the Moon singleton body.
getMoon() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Moon singleton body.
getMoon() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
getMoonSemiMajorAxis() - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants: Get the Moon semi-major axis.
getMountPoint() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the mount point.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Get the gravitational coefficient.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris: Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory: Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris: Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment: Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder: Get the gravitational coefficient.
getMu() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment: Get the standard gravitational parameter for the satellite.
getMu() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris: Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment: Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris: Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris: Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
getMu() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.forces.gravity.NewtonianAttraction: Get the central attraction coefficient μ.
getMu(Field<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction: Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the central body attraction coefficient.
getMu() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the central body attraction coefficient.
getMu() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Get the central body attraction coefficient.
getMu() - Method in class org.orekit.orbits.FieldOrbit: Get the central attraction coefficient used for position and velocity conversions (m³/s²).
getMu() - Method in class org.orekit.orbits.Orbit: Get the central acceleration constant.
getMu() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the Earth's universal gravitational parameter.
getMu() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Earth's universal gravitational parameter.
getMU() - Static method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator: Get the Earth gravity coefficient used for GLONASS propagation.
getMU() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator: Gets the Earth gravity coefficient used for GNSS propagation.
getMU() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator: Get the Earth gravity coefficient used for SBAS propagation.
getMU() - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Get the Earth gravity coefficient used for TLE propagation.
getMU() - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the Earth gravity coefficient used for TLE propagation.
getMu() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the central attraction coefficient (µ - m³/s²) value.
getMu() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the central attraction coefficient.
getMu() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.FieldStateMapper: Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.StateMapper: Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext: Get central attraction coefficient.
getMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext: Get central attraction coefficient.
getMu() - Method in class org.orekit.propagation.SpacecraftState: Get the central attraction coefficient.
getMultiplexer() - Method in class org.orekit.propagation.AbstractPropagator: Get the multiplexer holding all step handlers.
getMultiplexer() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get the multiplexer holding all step handlers.
getMultiplexer() - Method in interface org.orekit.propagation.FieldPropagator: Get the multiplexer holding all step handlers.
getMultiplexer() - Method in interface org.orekit.propagation.Propagator: Get the multiplexer holding all step handlers.
getMuoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get μ / a .
getMuoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get μ / a .
getMuoR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get muoR3 = mu3 / R3.
getMuoR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get muoR3 = mu3 / R3.
getMuSet() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser: Get the gravitational coefficient set at construction.
getN() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey: Get n.
getN4() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the four-year interval number starting from 1996.
getN4() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
getN4() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
getN4() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the number of the current four year interval.
getNA() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS N^A Word.
getNa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
getNa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
getNa() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the number of the current day in a four year interval.
getNadir() - Method in class org.orekit.bodies.FieldGeodeticPoint: Get the direction below the point, expressed in parent shape frame.
getNadir() - Method in class org.orekit.bodies.GeodeticPoint: Get the direction below the point, expressed in parent shape frame.
getNadir() - Method in class org.orekit.frames.TopocentricFrame: Get the nadir direction of topocentric frame, expressed in parent shape frame.
getName() - Method in interface org.orekit.bodies.CelestialBody: Get the name of the body.
getName() - Method in class org.orekit.bodies.CR3BPSystem: Get the name of the CR3BP system.
getName() - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
getName() - Method in class org.orekit.data.DataSource: Get the name of the data.
getName() - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination: Get the name of the combination of measurements.
getName() - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination: Get the name of the combination of measurements.
getName() - Method in enum org.orekit.estimation.measurements.gnss.CombinationType: Get the name of the combination of measurements.
getName() - Method in interface org.orekit.estimation.measurements.gnss.MeasurementCombination: Get the name of the combination of measurements.
getName() - Method in class org.orekit.estimation.measurements.gnss.MelbourneWubbenaCombination: Get the name of the combination of measurements.
getName() - Method in class org.orekit.files.ccsds.definitions.BodyFacade: Get the CCSDS name for the body.
getName() - Method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame: Get the name of celestial body frame.
getName() - Method in class org.orekit.files.ccsds.definitions.FrameFacade: Get the CCSDS name for the frame.
getName() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade: Get the name of the method.
getName() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the name of the block or entry.
getName() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the satellite target name.
getName() - Method in enum org.orekit.files.sinex.Station.ReferenceSystem: Get the name used to define the reference system in SINEX file.
getName() - Method in class org.orekit.forces.maneuvers.jacobians.Duration: Get the name of the additional state.
getName() - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay: Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate: Get the name of the additional state.
getName() - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate: Get the name of the additional state.
getName() - Method in class org.orekit.forces.maneuvers.Maneuver: Get the name of the maneuver.
getName() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the maneuver name.
getName() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel: Get the maneuver name.
getName() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers: Get the maneuver name.
getName() - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers: Get the maneuver name.
getName() - Method in class org.orekit.frames.Frame: Get the name.
getName() - Method in enum org.orekit.frames.ITRFVersion: Get the name the frame version.
getName() - Method in enum org.orekit.frames.Predefined: Get the name of the frame.
getName() - Method in enum org.orekit.gnss.antenna.SatelliteType: Get the IGS name for the antenna code.
getName() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine: Getter for the receiver/satellite name.
getName() - Method in enum org.orekit.gnss.Frequency: Get the RINEX name for the frequency.
getName() - Method in interface org.orekit.propagation.AdditionalStateProvider: Get the name of the additional state.
getName() - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider: Get the name of the additional state.
getName() - Method in class org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations: Deprecated.

Get the name of the additional state.
getName() - Method in interface org.orekit.propagation.FieldAdditionalStateProvider: Get the name of the additional state.
getName() - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper: Get the name of the partial Jacobians.
getName() - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider: Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in interface org.orekit.propagation.integration.AdditionalEquations: Deprecated.

Get the name of the additional state.
getName() - Method in class org.orekit.propagation.integration.AdditionalEquationsAdapter: Deprecated.

Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider: Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations: Deprecated.

Get the name of the additional state.
getName() - Method in class org.orekit.propagation.integration.FieldAdditionalEquationsAdapter: Deprecated.

Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations: Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations: Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Deprecated.

Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations: Deprecated.

Get the name of the additional derivatives (which will become state once integrated).
getName() - Method in class org.orekit.time.BDTScale: Get the name time scale.
getName() - Method in class org.orekit.time.GalileoScale: Get the name time scale.
getName() - Method in class org.orekit.time.GLONASSScale: Get the name time scale.
getName() - Method in class org.orekit.time.GMSTScale: Get the name time scale.
getName() - Method in class org.orekit.time.GPSScale: Get the name time scale.
getName() - Method in class org.orekit.time.IRNSSScale: Get the name time scale.
getName() - Method in class org.orekit.time.QZSSScale: Get the name time scale.
getName() - Method in class org.orekit.time.SatelliteClockScale: Get the name time scale.
getName() - Method in class org.orekit.time.TAIScale: Get the name time scale.
getName() - Method in class org.orekit.time.TCBScale: Get the name time scale.
getName() - Method in class org.orekit.time.TCGScale: Get the name time scale.
getName() - Method in class org.orekit.time.TDBScale: Get the name time scale.
getName() - Method in interface org.orekit.time.TimeScale: Get the name time scale.
getName() - Method in class org.orekit.time.TTScale: Get the name time scale.
getName() - Method in class org.orekit.time.UT1Scale: Get the name time scale.
getName() - Method in class org.orekit.time.UTCScale: Get the name time scale.
getName() - Method in class org.orekit.utils.ParameterDriver: Get name.
getName() - Method in class org.orekit.utils.units.Unit: Get the name of the unit.
getNarrowLaneCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory: Get the Narrow-Lane combination of measurements.
getNavigationSystem(String) - Static method in enum org.orekit.gnss.metric.ntrip.NavigationSystem: Get the navigation system corresponding to a keyword.
getNavigationSystems() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the navigation systems.
getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData: Get the number of maneuvers present in the APM.
getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Get the number of maneuvers present in the OPM.
getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData: Get the number of maneuvers present in the APM.
getNBodyPerturbations() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get n-body perturbation bodies.
getNbParams() - Method in class org.orekit.utils.ParameterDriversList: Get the number of parameters with different names.
getNbSpecies() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients: Get the number of species.
getNbTides(int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients: Get the number of tides for one species.
getNeighbors(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in class org.orekit.utils.GenericTimeStampedCache: Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in class org.orekit.utils.ImmutableTimeStampedCache: Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedCache: Get the entries surrounding a central date.
getNeighborsSize() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the fixed size of the arrays to be returned by GenericTimeStampedCache.getNeighbors(AbsoluteDate).
getNeighborsSize() - Method in class org.orekit.utils.ImmutableTimeStampedCache: Get the fixed size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate).
getNeighborsSize() - Method in interface org.orekit.utils.TimeStampedCache: Get the fixed size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate).
getNeptune() - Method in interface org.orekit.bodies.CelestialBodies: Get the Neptune singleton body.
getNeptune() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Neptune singleton body.
getNeptune() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
getNeQuickAlpha() - Method in class org.orekit.gnss.navigation.RinexNavigation: Get the "alpha" ionospheric parameters.
getNetwork() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the network.
getNetworkIdentifier() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord: Get the network identifier.
getNetworkInfoAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord: Get the web address for network information.
getNetworks() - Method in class org.orekit.gnss.metric.ntrip.SourceTable: Get the networks records.
getNewSlotQuantumGap() - Method in class org.orekit.utils.GenericTimeStampedCache: Get quantum gap above which a new slot is created instead of extending an existing one.
getNewState() - Method in class org.orekit.propagation.events.EventState.EventOccurrence: Get the new state for a reset action.
getNewState() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence: Get the new state for a reset action.
getNextMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the creation date of next message from a given originator.
getNextMessageID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the unique ID identifying next message from a given originator.
getNode(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole: Get the body Q Node direction in ICRF frame.
getNode(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole: Get the body Q Node direction in ICRF frame.
getNoise() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder: Generate a noise vector.
getNominalFireRate() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Get the nominal fire rate.
getNominalTidalDisplacement() - Method in enum org.orekit.utils.IERSConventions: Get the nominal values of the displacement numbers.
getNonInterpolatingEOPHistory() - Method in class org.orekit.frames.EOPHistory: Get non-interpolating version of the instance.
getNonInterpolatingProvider() - Method in interface org.orekit.frames.EOPBasedTransformProvider: Get a version of the provider that does not cache tidal corrections.
getNonInterpolatingProvider() - Method in class org.orekit.frames.GTODProvider: Get a version of the provider that does not cache tidal corrections.
getNonInterpolatingTransform(Frame, Frame, AbsoluteDate) - Static method in class org.orekit.frames.FramesFactory: Get the transform between two frames, suppressing all interpolation.
getNonInterpolatingTransform(Frame, Frame, FieldAbsoluteDate<T>) - Static method in class org.orekit.frames.FramesFactory: Get the transform between two frames, suppressing all interpolation.
getNonPolynomialSize() - Method in class org.orekit.data.PoissonSeries: Get the number of different terms in the non-polynomial part.
getNonRotatinOriginNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the correction to the nutation parameters for Non-Rotating Origin paradigm.
getNonRotatinOriginNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory: Get the correction to the nutation parameters for Non-Rotating Origin paradigm.
getNoradID() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Get the NORAD Catalog Number ("Satellite Number").
getNoradId() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the satellite NORAD ID (i.e.
getNormal() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet: Get unit normal vector.
getNormal(AbsoluteDate, Frame, Vector3D, Rotation) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Get solar array normal in spacecraft frame.
getNormal(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Get solar array normal in spacecraft frame.
getNormalGravity(double) - Method in class org.orekit.models.earth.ReferenceEllipsoid: Gets the normal gravity, that is gravity just due to the reference ellipsoid's potential.
getNormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics: Get a spherical harmonic cosine coefficient.
getNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the gravity field coefficients provider from the first supported file.
getNormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Create a time-independent NormalizedSphericalHarmonicsProvider from canonical coefficients.
getNormalizedProvider(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Create a NormalizedSphericalHarmonicsProvider from an UnnormalizedSphericalHarmonicsProvider.
getNormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields: Get a gravity field normalized coefficients provider.
getNormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields: Get a gravity field normalized coefficients provider.
getNormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics: Get a spherical harmonic sine coefficient.
getNormalizedValue() - Method in class org.orekit.utils.ParameterDriver: Get normalized value.
getNorth() - Method in class org.orekit.bodies.FieldGeodeticPoint: Get the direction to the north of point, expressed in parent shape frame.
getNorth() - Method in class org.orekit.bodies.GeodeticPoint: Get the direction to the north of point, expressed in parent shape frame.
getNorth() - Method in class org.orekit.frames.TopocentricFrame: Get the north direction of topocentric frame, expressed in parent shape frame.
getNorthOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to change station position along North axis.
getNt() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the current date.
getNtripFlags() - Method in class org.orekit.gnss.metric.ntrip.SourceTable: Get the flags set by server.
getNumber() - Method in interface org.orekit.estimation.measurements.EstimationsProvider: Get the number of evaluations available.
getNumber() - Method in enum org.orekit.time.Month: Get the month number.
getNumberOfBiasesProcessed() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data: Get the number of biases processed for the current satellite.
getNumberOfBiasesProcessed() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data: Get the number of biases processed for the current satellite.
getNumberOfClockDataTypes() - Method in class org.orekit.gnss.clock.RinexClock: Get the number of different clock data types in the file.
getNumberOfConstraints() - Method in class org.orekit.utils.AbstractMultipleShooting: Get the number of constraints.
getNumberOfEpochs() - Method in class org.orekit.files.sp3.SP3: Returns the number of epochs contained in this orbit file.
getNumberOfFreeEpoch() - Method in class org.orekit.utils.AbstractMultipleShooting: Get the number of free epoch.
getNumberOfFreeVariables() - Method in class org.orekit.utils.AbstractMultipleShooting: Get the number of free variables.
getNumberOfIonosphericLayers() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header: Get the number of ionospheric layers.
getNumberOfLeapSeconds() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the number of leap seconds.
getNumberOfLeapSeconds() - Method in class org.orekit.gnss.navigation.RinexNavigation: Getter for the current number of leap seconds.
getNumberOfLeapSecondsGNSS() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the number of leap second for GNSS time scales.
getNumberOfReceivers() - Method in class org.orekit.gnss.clock.RinexClock: Get the number of receivers that are considered in the file.
getNumberOfSatellites() - Method in class org.orekit.gnss.clock.RinexClock: Get the number of satellites that are considered in the file.
getNumberOfSatellites() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader: Get the number of satellites for the current IGM message.
getNumberOfValues() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine: Getter for the number of values to follow.
getNutation() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Get the nutation angle of spin axis (rad).
getNutationArguments(TimeScales) - Method in enum org.orekit.utils.IERSConventions: Get the fundamental nutation arguments.
getNutationArguments(TimeScale) - Method in enum org.orekit.utils.IERSConventions: Get the fundamental nutation arguments.
getNutationArguments(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions: Get the fundamental nutation arguments.
getNutationCorrectionConverter() - Method in enum org.orekit.utils.IERSConventions: Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.
getNutationCorrectionConverter(TimeScales) - Method in enum org.orekit.utils.IERSConventions: Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.
getNutationFunction() - Method in enum org.orekit.utils.IERSConventions: Get the function computing the nutation angles.
getNutationFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions: Get the function computing the nutation angles.
getNutationPeriod() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Get the body nutation period of the spin axis (s).
getNutationPhase() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Get the inertial nutation phase (rad).
getNutationReferenceEpoch() - Method in enum org.orekit.utils.IERSConventions: Get the reference epoch for fundamental nutation arguments.
getNutationReferenceEpoch(TimeScales) - Method in enum org.orekit.utils.IERSConventions: Get the reference epoch for fundamental nutation arguments.
getObjectDesignator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the unique satellite identification designator for the object.
getObjectID() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata: Get the spacecraft ID for which the attitude data are provided.
getObjectID() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata: Get the spacecraft ID for which the orbit state is provided.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the function computing position/velocity at sample points.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter: Get the function computing position/velocity at sample points.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter: Get the function computing position/velocity at sample points.
getObjectName() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata: Get the spacecraft name for which the attitude data are provided.
getObjectName() - Method in class org.orekit.files.ccsds.ndm.odm.OdmMetadata: Get the spacecraft name for which the orbit state is provided.
getObjectType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the type of object.
getOblateFlattening() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get central body oblate spheroid oblateness.
getObsAvailable() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get number of observations available within the actual OD span.
getObservationCode() - Method in class org.orekit.gnss.RinexObservationHeader: Get the observation code of the average phasecenter position w/r to antenna reference point.
getObservationData() - Method in class org.orekit.gnss.CombinedObservationDataSet: Get list of observation data.
getObservationData() - Method in class org.orekit.gnss.ObservationDataSet: Get list of observation data.
getObservationDataSets() - Method in class org.orekit.gnss.RinexObservationLoader: Get parsed rinex observations data sets.
getObservations() - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock: Get the list of Observations data lines.
getObservationType() - Method in class org.orekit.gnss.ObservationData: Get the observation type.
getObservedMeasurement() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the associated observed measurement.
getObservedMeasurement() - Method in class org.orekit.estimation.sequential.MeasurementDecorator: Get the observed measurement.
getObservedValue() - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Get the observed value.
getObservedValue() - Method in interface org.orekit.estimation.measurements.ComparableMeasurement: Get the observed value.
getObservedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the observed value.
getObserver() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the observer for Kalman Filter estimations.
getObserver() - Method in class org.orekit.propagation.events.AngularSeparationDetector: Get the observer for the spacecraft.
getObserverName() - Method in class org.orekit.gnss.RinexObservationHeader: Get name of the observer.
getObservers() - Method in class org.orekit.utils.ParameterDriver: Get the observers for this driver.
getObsUsed() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get number of observations accepted within the actual OD span.
getOcculted() - Method in class org.orekit.propagation.events.EclipseDetector: Getter for the occulted body.
getOcculted() - Method in class org.orekit.propagation.events.FieldEclipseDetector: Get the occulted body.
getOccultedRadius() - Method in class org.orekit.propagation.events.EclipseDetector: Getter for the occultedRadius.
getOccultedRadius() - Method in class org.orekit.propagation.events.FieldEclipseDetector: Get the occulted body radius (m).
getOcculting() - Method in class org.orekit.propagation.events.EclipseDetector: Getter for the occulting body.
getOcculting() - Method in class org.orekit.propagation.events.FieldEclipseDetector: Get the occulting body.
getOccultingRadius() - Method in class org.orekit.propagation.events.FieldEclipseDetector: Get the occulting body radius (m).
getOceanLoadDeformationCoefficients() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the configured ocean load deformation coefficients.
getOceanLoadDeformationCoefficients() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields: Get the configured ocean load deformation coefficients.
getOceanPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions: Get the function computing ocean pole tide (ΔC₂₁, ΔS₂₁).
getOceanTidesModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get ocean tides model.
getOceanTidesWaves(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the ocean tides waves from the first supported file.
getOceanTidesWaves(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields: Get the ocean tides waves.
getOceanTidesWaves(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields: Get the ocean tides waves.
getOcmDataElements() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the list of elements of information data blocks included in this message.
getOebAreaAlongIntermediate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the cross-sectional area of Optimally Enclosing Box along Y-OEB.
getOebAreaAlongMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the cross-sectional area of Optimally Enclosing Box along X-OEB.
getOebAreaAlongMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the cross-sectional area of Optimally Enclosing Box along Z-OEB.
getOebIntermediate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
getOebMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the dimensions of Optimally Enclosing Box along X-OEB (i.e max).
getOebMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the dimensions of Optimally Enclosing Box along Z-OEB (i.e min).
getOebParentFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the Optimally Enclosing Box parent reference frame.
getOebParentFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the Optimally Enclosing Box parent reference frame epoch.
getOebQ() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the quaternion defining Optimally Enclosing Box.
getOffset(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Deprecated.
getOffset(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Deprecated.
as of 11.1, this method is only called by deprecated methods
getOffset() - Method in class org.orekit.time.OffsetModel: Offset at reference date in seconds (TAI minus UTC).
getOffset(AbsoluteDate) - Method in class org.orekit.time.UTCTAIOffset: Get the TAI - UTC offset in seconds.
getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCTAIOffset: Get the TAI - UTC offset in seconds.
getOffset(DateComponents, TimeComponents) - Method in class org.orekit.time.UTCTAIOffset: Get the TAI - UTC offset in seconds.
getOffsetGeodeticPoint(AbsoluteDate) - Method in class org.orekit.estimation.measurements.GroundStation: Get the geodetic point at the center of the offset frame.
getOffsetToInertial(Frame, AbsoluteDate) - Method in class org.orekit.estimation.measurements.GroundStation: Get the transform between offset frame and inertial frame.
getOffsetToInertial(Frame, AbsoluteDate, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation: Get the transform between offset frame and inertial frame with derivatives.
getOffsetToInertial(Frame, FieldAbsoluteDate<Gradient>, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation: Get the transform between offset frame and inertial frame with derivatives.
getOmega() - Method in class org.orekit.data.DelaunayArguments: Get the mean longitude of the ascending node of the Moon.
getOmega() - Method in class org.orekit.data.FieldDelaunayArguments: Get the mean longitude of the ascending node of the Moon.
getOmega0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the longitude of ascending node of orbit plane at weekly epoch.
getOmega0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Longitude of Ascending Node of Orbit Plane at Weekly Epoch.
getOmegaDot() - Method in class org.orekit.data.DelaunayArguments: Get the mean longitude of the ascending node of the Moon time derivative.
getOmegaDot() - Method in class org.orekit.data.FieldDelaunayArguments: Get the mean longitude of the ascending node of the Moon time derivative.
getOmegaDot() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the rate of right ascension.
getOmegaDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Rate of Right Ascension.
getOOA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext: Get ooA = 1 / A.
getOOA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext: Get ooA = 1 / A.
getOOAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext: Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get ooAB = 1 / (A * B).
getOOAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext: Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get ooAB = 1 / (A * B).
getOoBpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext: Get ooBpo = 1 / (B + 1).
getOoBpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext: Get ooBpo = 1 / (B + 1).
getOoMU() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext: Get ooMu = 1 / mu.
getOoMU() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext: Get ooMu = 1 / mu.
getOON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get 1 / (n² * a²).
getOON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get 1 / (n² * a²).
getOpener() - Method in class org.orekit.data.DataSource: Get the data stream opener.
getOperator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the operator of the space object.
getOperator() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Get the institution/agency/company operating the caster.
getOperator() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord: Get the institution/agency/company operating the caster.
getOpsStatus() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the operational status.
getOptimum() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Get the optimum found.
getOrbAveraging() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get type of averaging (Osculating, mean Brouwer, other.
getOrbit() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the current orbit.
getOrbit() - Method in class org.orekit.propagation.SpacecraftState: Get the current orbit.
getOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator: Get the underlying GNSS orbital elements.
getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Get the orbital parameters supported by this estimator.
getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.KalmanEstimator: Get the orbital parameters supported by this estimator.
getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator: Get the orbital parameters supported by this estimator.
getOrbitalParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the drivers for the configurable orbital parameters.
getOrbitalParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Get the drivers for the configurable orbital parameters.
getOrbitalPeriod() - Method in class org.orekit.orbits.CR3BPDifferentialCorrection: Get the orbital period of the required orbit.
getOrbitalPeriod() - Method in class org.orekit.orbits.LibrationOrbit: Return the orbital period of the libration orbit.
getOrbitCategory() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the orbit category.
getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data: Get the orbit correction data.
getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data: Get the orbit correction data.
getOrbitDeterminationBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData: Get orbit determination logical block.
getOrbitPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get the Keplerian period.
getOrbitPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get the Keplerian period.
getOrbitType() - Method in class org.orekit.files.sp3.SP3: Returns the SP3.SP3OrbitType for this SP3 file.
getOrbitType() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getOrbitType() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getOrbitType() - Method in class org.orekit.propagation.events.PositionAngleDetector: Get the orbit type defining the angle type.
getOrbitType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.integration.FieldStateMapper: Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.integration.StateMapper: Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.numerical.NumericalPropagator: Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Get propagation parameter type.
getOrbitTypeKey() - Method in class org.orekit.files.sp3.SP3: Returns the orbit type key for this SP3 file.
getOrbRevNum() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get the integer orbit revolution number.
getOrbRevNumBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get the basis for orbit revolution number.
getOrdinateGrid() - Method in class org.orekit.utils.InterpolationTableLoader: Returns a copy of the ordinate grid for the interpolation function.
getOrientation() - Method in class org.orekit.attitudes.Attitude: Get the complete orientation including spin.
getOrientation() - Method in class org.orekit.attitudes.FieldAttitude: Get the complete orientation including spin.
getOrigin() - Method in enum org.orekit.frames.HelmertTransformation.Predefined: Get the origin ITRF.
getOrigin() - Method in class org.orekit.frames.ITRFVersion.Converter: Get the origin ITRF.
getOriginal() - Method in class org.orekit.propagation.events.NegateDetector: Get the delegate event detector.
getOriginator() - Method in class org.orekit.files.ccsds.section.Header: Get the file originator.
getOriginatorAddress() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the address of Programmatic Point Of Contact at originator.
getOriginatorPhone() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the phone number of Programmatic Point Of Contact at originator.
getOriginatorPOC() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the programmatic Point Of Contact at originator.
getOriginatorPosition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the position of Programmatic Point Of Contact at originator.
getOriginIndicator() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement: Get the angle origin indicator.
getOtherOccultingBodies() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Getter for other occulting bodies to consider.
getOTrajectoryBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData: Get trajectory state histories logical blocks.
getOutputName() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator: Get the name of the output (for error messages).
getOutputName() - Method in interface org.orekit.files.ccsds.utils.generation.Generator: Get the name of the output (for error messages).
getOutputPulseType() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the output pulse type.
getOutputPulseWidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the output pulse width.
getOwner() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the owner of the space object.
getP() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS P Word.
getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the y component of inclination vector.
getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the y component of inclination vector.
getP1() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS P1 Word.
getP2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS P2 Word.
getP3() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS P3 Word.
getP4() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS P4 Word.
getPa() - Method in class org.orekit.data.BodiesElements: Get the general accumulated precession in longitude.
getPa() - Method in class org.orekit.data.FieldBodiesElements: Get the general accumulated precession in longitude.
getPa() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Get the orbit argument of pericenter.
getPa() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the argument of perigee.
getPa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
getPa() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the Argument of Perigee.
getPa() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Argument of Perigee.
getPaDot() - Method in class org.orekit.data.BodiesElements: Get the general accumulated precession in longitude time derivative.
getPaDot() - Method in class org.orekit.data.FieldBodiesElements: Get the general accumulated precession in longitude time derivative.
getParameterDerivatives(ParameterDriver) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the partial derivatives of the simulated measurement with respect to a parameter.
getParameterDriver(String) - Method in class org.orekit.forces.AbstractForceModel: Get parameter value from its name.
getParameterDriver(String) - Method in interface org.orekit.forces.ForceModel: Get parameter value from its name.
getParameterDriver(String) - Method in class org.orekit.forces.inertia.InertialForces: Get parameter value from its name.
getParameterDriver(String) - Method in class org.orekit.propagation.analytical.tle.TLE: Get parameter driver from its name.
getParameters(FieldSpacecraftState<Gradient>, IonosphericModel) - Method in class org.orekit.estimation.measurements.modifiers.IonosphericGradientConverter: Get the ionospheric model parameters.
getParameters(FieldSpacecraftState<Gradient>, DiscreteTroposphericModel) - Method in class org.orekit.estimation.measurements.modifiers.TroposphericGradientConverter: Get the tropospheric model parameters.
getParameters() - Method in class org.orekit.files.ccsds.ndm.odm.UserDefined: Get all user defined parameters.
getParameters() - Method in interface org.orekit.forces.ForceModel: Get force model parameters.
getParameters(Field<T>) - Method in interface org.orekit.forces.ForceModel: Get force model parameters.
getParameters() - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel: Get ionospheric model parameters.
getParameters(Field<T>) - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel: Get ionospheric model parameters.
getParameters() - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel: Get tropospheric model parameters.
getParameters(Field<T>) - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel: Get tropospheric model parameters.
getParameters(FieldSpacecraftState<Gradient>) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter: Get the model parameters.
getParameters(Field<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Get model parameters.
getParameters(Field<T>) - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get model parameters.
getParameters() - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper: Get the number of parameters.
getParameters() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Get force model parameters.
getParameters(Field<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Get force model parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Get the drivers for this measurement parameters, including its modifiers parameters.
getParametersDrivers() - Method in interface org.orekit.estimation.measurements.EstimationModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.gnss.WindUp: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.Bias: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesPhaseModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSPhaseModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSRangeModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaPhaseModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaRangeModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesPhaseModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesRangeModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSPhaseModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockPhaseModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeRateModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Get the drivers for this measurement parameters, including its modifiers parameters.
getParametersDrivers() - Method in class org.orekit.forces.drag.DragForce: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.drag.TimeSpanDragForce: Get the drivers for force model parameters.
getParametersDrivers() - Method in interface org.orekit.forces.empirical.AccelerationModel: Get the drivers for acceleration model parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel: Get the drivers for acceleration model parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.ParametricAcceleration: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel: Get the drivers for acceleration model parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration: Get the drivers for force model parameters.
getParametersDrivers() - Method in interface org.orekit.forces.ForceModel: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.DeSitterRelativity: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.LenseThirringRelativity: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.NewtonianAttraction: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.OceanTides: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.Relativity: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.SolidTides: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.inertia.InertialForces: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.Maneuver
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Get the propulsion model parameter drivers.
getParametersDrivers() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel: Get the propulsion model parameter drivers.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel: Get the propulsion model parameter drivers.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers: Get the maneuver triggers parameter drivers.
getParametersDrivers() - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers: Get the maneuver triggers parameter drivers.
getParametersDrivers() - Method in class org.orekit.forces.radiation.ECOM2: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
getParametersDrivers() - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel: Get the drivers for ionospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel: Get the drivers for ionospheric model parameters.
getParametersDrivers() - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel: Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel: Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay: Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel: Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel: Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel: Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel: Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ViennaOneModel: Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel: Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter: Get the parameter drivers related to the analytical propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator: Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the drivers for TLE propagation SGP4 and SDP4.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the drivers for TLE propagation SGP4 and SDP4.
getParametersDrivers() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Get the drivers for force model parameters.
getParametersDrivers() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Get the drivers for force model parameters.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester: Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester: Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.analytical.tle.TLEJacobiansMapper: Get the Jacobian with respect to parameters from a one-dimensional additional state array.
getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper: Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper: Get the Jacobian with respect to parameters from a one-dimensional additional state array.
getParametersJacobian(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester: Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper: Get the Jacobian with respect to parameters from a one-dimensional additional state array.
getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester: Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper: Get the Jacobian with respect to parameters from a one-dimensional additional state array.
getParent() - Method in class org.orekit.frames.Frame: Get the parent frame.
getParentShape() - Method in class org.orekit.frames.TopocentricFrame: Get the body shape on which the local point is defined.
getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder: Get the behavior to adopt for handling parsed units.
getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.utils.ContextBinding: Get the behavior to adopt for handling parsed units.
getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Get the behavior to adopt for handling parsed units.
getParser(List<Integer>) - Method in enum org.orekit.gnss.metric.ntrip.Type: Get the message parser associated to the SSR type.
getParticipants() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the coordinates of the measurements participants in signal travel order.
getParticipants() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the participants.
getParts() - Method in interface org.orekit.errors.LocalizedException: Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitException: Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitIllegalArgumentException: Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitIllegalStateException: Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitInternalError: Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitIOException: Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitParseException: Get the variable parts of the error message.
getPastInfinity() - Method in class org.orekit.time.AbstractTimeScales
getPastInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Dummy date at infinity in the past direction.
getPastInfinity() - Method in interface org.orekit.time.TimeScales: Dummy date at infinity in the past direction.
getPatchedSpacecraftState() - Method in class org.orekit.utils.AbstractMultipleShooting: Get the list of patched spacecraft states.
getPatchPoint(int) - Method in class org.orekit.utils.AbstractMultipleShooting: Get a patch point.
getPath() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the path.
getPath1() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the path1.
getPath2() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the path2.
getPattern() - Method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType: Get the message number.
getPattern() - Method in enum org.orekit.gnss.metric.parser.RtcmMessageType: Get the message number.
getPdop() - Method in class org.orekit.gnss.DOP: Gets the position dilution of precision.
getPendingEvent() - Method in class org.orekit.propagation.events.FieldEventState: Get PendingEvent.
getPerigeeArgument() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the perigee argument.
getPerigeeArgument() - Method in class org.orekit.orbits.KeplerianOrbit: Get the perigee argument.
getPerigeeArgument() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the argument of perigee.
getPerigeeArgument() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the argument of perigee.
getPerigeeArgumentDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the perigee argument derivative.
getPerigeeArgumentDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the perigee argument derivative.
getPermanentTide() - Method in enum org.orekit.utils.IERSConventions: Get the permanent tide to be removed from ΔC₂₀ when zero-tide potentials are used.
getPerturbationsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData: Get perturbations logical block.
getPhase(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide: Get the phase of the tide.
getPhaseBias() - Method in class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias: Get the phase bias associated to the signal ID.
getPhaseBias(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data: Get the phase bias for a given signal ID.
getPhaseBiases() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data: Get the phase biases for the current satellite.
getPhaseCenterVariation(Frequency, Vector3D) - Method in class org.orekit.gnss.antenna.Antenna: Get the value of the phase center variation in a signal direction.
getPhaseCenterVariation(Vector3D) - Method in class org.orekit.gnss.antenna.FrequencyPattern: Get the value of the phase center variation in a signal direction.
getPhaseMinusCodeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory: Get the phase minus code combination of measurements.
getPhaseShiftCorrections() - Method in class org.orekit.gnss.RinexObservationHeader: Get the list of phase shift correction used to generate phases consistent w/r to cycle shifts.
getPhysicalCovariances(double) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Get the covariances matrix in space flight dynamics physical units.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.KalmanEstimator: Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator: Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.KalmanEstimator: Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator: Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the "physical" estimated state (i.e.
getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the physical innovation covariance matrix.
getPhysicalInnovationCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the physical innovation covariance matrix.
getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the physical innovation covariance matrix.
getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the physical Kalman gain matrix.
getPhysicalKalmanGain() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the physical Kalman gain matrix.
getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the physical Kalman gain matrix.
getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the physical Jacobian of the measurement with respect to the state (H matrix).
getPhysicalMeasurementJacobian() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the physical Jacobian of the measurement with respect to the state (H matrix).
getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the physical Jacobian of the measurement with respect to the state (H matrix).
getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
getPhysicalStateTransitionMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
getPhysicBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData: Get physical properties logical block.
getPlaneSection(Vector3D, Vector3D) - Method in class org.orekit.bodies.Ellipsoid: Compute the 2D ellipse at the intersection of the 3D ellipsoid and a plane.
getPlus(int, int) - Method in class org.orekit.utils.LoveNumbers: Get the real part of a nominal Love numbers.
getPluto() - Method in interface org.orekit.bodies.CelestialBodies: Get the Pluto singleton body.
getPluto() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Pluto singleton body.
getPluto() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
getPnm(int, int) - Method in class org.orekit.utils.FieldLegendrePolynomials: Return the coefficient P_nm.
getPnm(int, int) - Method in class org.orekit.utils.LegendrePolynomials: Return the coefficient P_nm.
getPoint() - Method in class org.orekit.frames.TopocentricFrame: Get the surface point defining the origin of the frame.
getPoint(Field<T>) - Method in class org.orekit.frames.TopocentricFrame: Get the surface point defining the origin of the frame.
getPolarDriftXDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get a driver allowing to add a polar drift along X.
getPolarDriftXDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to add a polar drift along X.
getPolarDriftYDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get a driver allowing to add a polar drift along Y.
getPolarDriftYDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to add a polar drift along Y.
getPolarOffsetXDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get a driver allowing to add a polar offset along X.
getPolarOffsetXDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to add a polar offset along X.
getPolarOffsetYDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get a driver allowing to add a polar offset along Y.
getPolarOffsetYDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to add a polar offset along Y.
getPolarRadius() - Method in class org.orekit.models.earth.ReferenceEllipsoid: Get the radius of this ellipsoid at the poles.
getPole(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole: Get the body North pole direction in ICRF frame.
getPole(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole: Get the body North pole direction in ICRF frame.
getPoleCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the pole IERS Reference Pole correction.
getPoleCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory: Get the pole IERS Reference Pole correction.
getPolynomial() - Method in class org.orekit.data.PoissonSeries: Get the polynomial part of the series.
getPort() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Get the port number.
getPort() - Method in class org.orekit.gnss.metric.ntrip.NtripClient: Get the port to use for connection.
getPosition() - Method in class org.orekit.estimation.measurements.Position: Get the position.
getPosition() - Method in class org.orekit.estimation.measurements.PV: Get the position.
getPosition() - Method in class org.orekit.files.sinex.Station: Get the station position.
getPosition() - Method in class org.orekit.utils.FieldPVCoordinates: Gets the position.
getPosition() - Method in class org.orekit.utils.PVCoordinates: Gets the position.
getPositionAngle() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise: Getter for the positionAngle.
getPositionAngle() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getPositionAngle() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getPositionAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector: Get the type of position angle.
getPositionAngleType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper: Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.StateMapper: Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.numerical.NumericalPropagator: Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Get propagation parameter type.
getPositionScale() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the position scale.
getPotential(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel: Calculate spacecraft potential.
getPotential(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel: Calculate spacecraft potential.
getPrecessionFunction() - Method in enum org.orekit.utils.IERSConventions: Get the function computing the precession angles.
getPrecessionFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions: Get the function computing the precession angles.
getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the predicted measurement.
getPredictedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the predicted measurement.
getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the predicted measurement.
getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Get the predicted spacecraft states.
getPredictedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the predicted spacecraft states.
getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the predicted spacecraft states.
getPredictionProvider() - Method in class org.orekit.files.ilrs.CRDHeader: Get the prediction provider.
getPredictionType() - Method in class org.orekit.files.ilrs.CRDHeader: Get the prediction type (CPF or TLE).
getPressSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Get the pressure sensor manufacturer.
getPressSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Get the pressure sensor model.
getPressSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Get the pressure sensor serial number.
getPressure() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement: Get the surface pressure.
getPressure() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Get the local pressure at the evaluation location.
getPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model: Returns the pressure at the station [hPa].
getPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel: Get the atmospheric pressure of the station depending its position.
getPrevId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get identification of previous orbit determination.
getPreviousMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the creation date of previous message from a given originator.
getPreviousMessageID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the unique ID identifying previous message from a given originator.
getPreviousState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator: Get the state at previous grid point date.
getPreviousState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Get the state at previous grid point date.
getPrf() - Method in class org.orekit.files.ilrs.CPFHeader: Get the Pulse Repetition Frequency (PRF).
getPrimary() - Method in class org.orekit.bodies.CR3BPSystem: Get the primary CelestialBody.
getPrimaryObject() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector: Get the primaryObject, at the center of the proximity zone.
getPrimaryStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange: Get the primary ground station from which measurement is performed.
getPrimaryWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Get the primary wavelength.
getPrimeMeridianAngle(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole: Get the prime meridian angle.
getPrimeMeridianAngle(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole: Get the prime meridian angle.
getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get a driver allowing to add a prime meridian rotation rate.
getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to add a prime meridian rotation rate.
getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get a driver allowing to add a prime meridian rotation.
getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to add a prime meridian rotation.
getPrmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the Unique identifier of Pointing Request Message linked to this Orbit Data Message.
getPRN() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Getter for the PRN number of the satellite.
getPRN() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the PRN number of the satellite.
getPRN() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the PRN number of the GNSS satellite.
getPRN() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Gets the PRN number of the SBAS satellite.
getPrnNumber() - Method in class org.orekit.gnss.antenna.SatelliteAntenna: Get PRN number.
getPrnNumber() - Method in class org.orekit.gnss.CombinedObservationDataSet: Get PRN number.
getPrnNumber() - Method in class org.orekit.gnss.ObservationDataSet: Get PRN number.
getPRNNumbers() - Method in class org.orekit.gnss.SEMParser: Gets the PRN numbers of all the GPS almanacs read from the file.
getPRNNumbers() - Method in class org.orekit.gnss.YUMAParser: Gets the PRN numbers of all the GPS almanacs read from the file.
getProcessingSoftwares() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Get the processing softwares.
getProcessingSoftwareVersions() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Get the processing software versions.
getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in class org.orekit.estimation.sequential.ConstantProcessNoise: Get the process noise matrix between previous and current states.
getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider: Get the process noise matrix between previous and current states.
getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise: Get the process noise matrix between previous and current states.
getProductionEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the date component of the ephemeris production.
getProductionHour() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the hour of ephemeris production (UTC).
getProgDCBS() - Method in class org.orekit.gnss.AppliedDCBS: Get the program name used to apply DCBs.
getProgPCVS() - Method in class org.orekit.gnss.AppliedPCVS: Get the program name used to apply PCVs.
getProgramName() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the program name.
getProgramName() - Method in class org.orekit.gnss.navigation.RinexNavigation: Getter for the program name.
getPropagationParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.KalmanEstimator: Get the propagator parameters supported by this estimator.
getPropagationParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator: Get the propagator parameters supported by this estimator.
getPropagationParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the drivers for the configurable propagation parameters.
getPropagationParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Get the drivers for the configurable propagation parameters.
getPropagationParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise: Getter for the propagationParametersEvolution.
getPropagationType() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder: Get the type of the orbit used for the propagation (mean or osculating).
getPropagationType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the propagation type.
getPropagator(ObservableSatellite) - Method in class org.orekit.estimation.measurements.generation.Generator: Get a registered propagator.
getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment: View this ephemeris segment as a propagator.
getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris: View this ephemeris as a propagator, combining data from all segments.
getPropagator() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris: View this ephemeris as a propagator, combining data from all segments.
getPropagator() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
getPropagator(FieldSpacecraftState<Gradient>, Gradient[]) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter: Get the converted analytical orbit propagator.
getPropagator() - Method in class org.orekit.propagation.analytical.AdapterPropagator: Get the reference propagator.
getPropagatorIndex() - Method in class org.orekit.estimation.measurements.ObservableSatellite: Get the index of the propagator related to this satellite.
getPropagatorList() - Method in class org.orekit.utils.AbstractMultipleShooting: Get the list of propagators.
getPropagatorParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Get the propagator parameters supported by this estimator.
getPropagators() - Method in class org.orekit.propagation.PropagatorsParallelizer: Get an unmodifiable list of the underlying mono-satellite propagators.
getPropulsionModel() - Method in class org.orekit.forces.maneuvers.Maneuver: Get the propulsion model.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader: Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader: Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader: Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader: Get a provider for read spherical harmonics coefficients.
getProvider() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Get the spherical harmonics provider.
getProviders() - Method in class org.orekit.data.DataProvidersManager: Get an unmodifiable view of the list of supported providers.
getProximityAngle() - Method in class org.orekit.propagation.events.AngularSeparationDetector: Get the proximity angle (rad).
getProximityAngle() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector: Get the proximity angle (rad).
getProxy() - Method in class org.orekit.gnss.metric.ntrip.NtripClient: Get proxy.
getPulseEnergy() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Get the pulse energy.
getPulseInOutgoingSemiTrain() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Get the number of pulses in outgoing semi-train.
getPulseWidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Get the pulse width (FWHM in ps).
getPVCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Get the position/velocity coordinates contained in the OPM.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame: Get the PVCoordinates of the topocentric frame origin in the selected frame.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.FieldOrbit: Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.orbits.FieldOrbit: Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit: Get the TimeStampedPVCoordinates in definition frame.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.Orbit: Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.orbits.Orbit: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.orbits.Orbit: Get the TimeStampedPVCoordinates in definition frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.AbstractPropagator: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.Ephemeris: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Get the extrapolated position and velocity from an initial TLE.
getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the extrapolated position and velocity from an initial TLE.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.FieldAbstractPropagator: Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the TimeStampedFieldPVCoordinates in orbit definition frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.FieldSpacecraftState: Get the TimeStampedFieldPVCoordinates in given output frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.propagation.SpacecraftState: Get the TimeStampedPVCoordinates in orbit definition frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.SpacecraftState: Get the TimeStampedPVCoordinates in given output frame.
getPVCoordinates() - Method in class org.orekit.utils.AbsolutePVCoordinates: Get the TimeStampedPVCoordinates.
getPVCoordinates(Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates: Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider: Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates: Get the TimeStampedFieldPVCoordinates.
getPVCoordinates(Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates: Get the TimeStampedFieldPVCoordinates in a specified frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.FieldPVCoordinatesProvider: Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider: Get the PVCoordinates of the body in the selected frame.
getPVCoordinatesProvider() - Method in class org.orekit.propagation.events.AlignmentDetector: Get the body to align.
getPvProvider() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Get PV coordinates provider.
getPvProvider() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Get PV coordinates provider.
getPVTarget() - Method in class org.orekit.propagation.events.FieldOfViewDetector: Get the position/velocity provider of the target .
getPZ9011(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
getPZ9011(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames: Get the PZ-90.11 (Parametry Zemly – 1990.11) reference frame.
getPZ9011(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the PZ-90.11 (Parametry Zemly – 1990.11) reference frame.
getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the x component of inclination vector.
getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the x component of inclination vector.
getQns() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get the value of Qns coefficients.
getQns() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get the value of Qns coefficients.
getQualityIndicator() - Method in class org.orekit.files.ilrs.CRDHeader: Get the data quality indicator.
getQuantumEfficiency() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the quantum efficiency at applicable wavelength.
getQuaternion() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion: Get the quaternion.
getQuaternionBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData: Get the quaternion logical block.
getQuaternionDot() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion: Get the quaternion derivative.
getQZSS() - Method in class org.orekit.time.LazyLoadedTimeScales
getQZSS() - Method in interface org.orekit.time.TimeScales: Get the Quasi-Zenith Satellite System time scale.
getQZSS() - Static method in class org.orekit.time.TimeScalesFactory: Get the Quasi-Zenith Satellite System time scale.
getQzssCodeOnL2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data: Get the QZSS code on L2 Channel.
getQzssEpoch() - Method in class org.orekit.time.AbstractTimeScales
getQzssEpoch() - Method in interface org.orekit.time.TimeScales: Reference epoch for QZSS weeks: 1980-01-06T00:00:00 QZSS time.
getQzssFitInterval() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data: Get the QZSS fit interval.
getQzssNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data: Get the QZSS navigation message corresponding to the current RTCM data.
getQzssNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data: Get the QZSS navigation message corresponding to the current RTCM data.
getQZSSNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation: Get all the QZSS navigation messages contained in the file.
getQZSSNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation: Get the QZSS navigation messages for the given satellite Id.
getQzssToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data: Get the QZSS time of clock.
getRaan() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Get the orbit right ascension of ascending node.
getRaan() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get Right Ascension of the Ascending node.
getRaan() - Method in class org.orekit.propagation.analytical.tle.TLE: Get Right Ascension of the Ascending node.
getRadiationParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention: Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention: Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient: Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in interface org.orekit.forces.radiation.RadiationSensitive: Get the drivers for supported parameters.
getRange(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame: Get the range of a point with regards to the topocentric frame center point.
getRange(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame: Get the range of a point with regards to the topocentric frame center point.
getRange1() - Method in class org.orekit.estimation.iod.IodGooding: Get the range for observation (1).
getRange2() - Method in class org.orekit.estimation.iod.IodGooding: Get the range for observation (2).
getRange3() - Method in class org.orekit.estimation.iod.IodGooding: Get the range for observation (3).
getRangeData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the range data for the data block.
getRangeMode() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the rangeMode.
getRangeModulus(RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the range modulus in meters.
getRangeRate(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame: Get the range rate of a point with regards to the topocentric frame center point.
getRangeRate(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame: Get the range rate of a point with regards to the topocentric frame center point.
getRangeType() - Method in class org.orekit.files.ilrs.CRDHeader: Get the range type.
getRangeType(int) - Static method in enum org.orekit.files.ilrs.CRDHeader.RangeType: Get the range type for the given indicator.
getRangeUnits() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the rangeUnits.
getRangeUnitsConverter() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder: Get the converter for Range Units.
getRate() - Method in class org.orekit.gnss.metric.ntrip.StreamedMessage: Get refresh rate.
getRate(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide: Get the angular rate of the tide.
getRatio() - Method in enum org.orekit.gnss.Frequency: Get the ratio f/f0, where f0 is the common frequency.
getRatio() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get the ratio of satellite period to central body rotation period.
getRatio() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get the ratio of satellite period to central body rotation period.
getRawCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics: Get a spherical harmonic cosine coefficient.
getRawContent() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the raw content of the entry.
getRawCorrectionRange() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the raw correction for range.
getRawDrivers() - Method in class org.orekit.utils.ParameterDriversList.DelegatingDriver: Get the raw drivers to which this one delegates.
getRawProvider() - Method in class org.orekit.frames.InterpolatingTransformProvider: Get the underlying provider for raw (non-interpolated) transforms.
getRawProvider() - Method in class org.orekit.frames.ShiftingTransformProvider: Get the underlying provider for raw (non-interpolated) transforms.
getRawPV(AbsoluteDate) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider: Get the position-velocity at date.
getRawPV(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider: Get the position-velocity at date.
getRawRangeModulus() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the raw range modulus.
getRawSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics: Get a spherical harmonic sine coefficient.
getRbar() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the critical distance.
getRcs() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the typical (50th percentile) radar cross-section.
getRcvrClkOffset() - Method in class org.orekit.gnss.CombinedObservationDataSet: Get receiver clock offset.
getRcvrClkOffset() - Method in class org.orekit.gnss.ObservationDataSet: Get receiver clock offset.
getRdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the Unique identifier of Reentry Data Message linked to this Orbit Data Message.
getReal(int, int) - Method in class org.orekit.utils.LoveNumbers: Get the real part of a nominal Love numbers.
getRealAPV(AbsolutePVCoordinates, AbsoluteDate, Frame) - Method in class org.orekit.bodies.CR3BPSystem: Get the AbsolutePVCoordinates from normalized units to standard units in an output frame.
getReceiveBand() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the receiveBand.
getReceiveDelays() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for receiveDelays.
getReceiverIdentifier() - Method in class org.orekit.gnss.clock.RinexClock.Receiver: Getter for the receiver identifier.
getReceiverNumber() - Method in class org.orekit.gnss.RinexObservationHeader: Get the number of the receiver.
getReceivers() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the receivers.
getReceiversAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader: Get parsed receivers antennas.
getReceiverType() - Method in class org.orekit.gnss.RinexObservationHeader: Get the type of the receiver.
getReceiverVersion() - Method in class org.orekit.gnss.RinexObservationHeader: Get the version of the receiver.
getRecommendedOdSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get sime span of observation recommended for the OD of the object.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Get the type of record.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the type of record.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord: Get the type of record.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.Record: Get the type of record.
getReductionTheory() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get reduction theory used for precession and nutation modeling.
getReferenceAttitude() - Method in class org.orekit.attitudes.FixedRate: Get the reference attitude.
getReferenceClocks() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the reference clocks.
getReferenceDate() - Method in class org.orekit.files.ccsds.utils.ContextBinding: Get initial date.
getReferenceDate() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the reference date for the harmonics.
getReferenceDate() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Get the reference date for the harmonics.
getReferenceDate() - Method in class org.orekit.propagation.integration.FieldStateMapper: Get reference date.
getReferenceDate() - Method in class org.orekit.propagation.integration.StateMapper: Get reference date.
getReferenceDate() - Method in class org.orekit.utils.ParameterDriver: Get current reference date.
getReferenceDate() - Method in class org.orekit.utils.SecularAndHarmonic: Get the reference date.
getReferenceFrame() - Method in class org.orekit.attitudes.Attitude: Get the reference frame.
getReferenceFrame() - Method in class org.orekit.attitudes.FieldAttitude: Get the reference frame.
getReferenceFrame() - Method in class org.orekit.estimation.measurements.AngularRaDec: Get the reference frame in which the right ascension - declination angles are given.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment: Get the reference frame from which attitude is defined.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance: Get the reference frame.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata: Get the value of REF_FRAME as an Orekit Frame.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver: Get Coordinate system for velocity increment vector.
getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Get the the value of REFERENCE_FRAME as an Orekit Frame.
getReferenceFrame() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment: Get the reference frame from which attitude is defined.
getReferenceFrame() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment: Get the reference frame from which attitude is defined.
getReferenceName() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock: Getter for the name of the receiver/satellite embedding the reference clock.
getReferenceRadius() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Get the reference radius of the central body attraction model.
getReferenceRadius() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Get the reference radius of the central body attraction model.
getReferenceTrajectories() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Getter for the reference trajectories.
getReferenceValue() - Method in class org.orekit.utils.ParameterDriver: Get reference parameter value.
getRefFrame() - Method in class org.orekit.files.ccsds.definitions.ModifiedFrame: Get the CCSDS reference frame.
getRefFrame() - Method in class org.orekit.files.ilrs.CPFHeader: Get the reference frame.
getRefFrameId() - Method in class org.orekit.files.ilrs.CPFHeader: Get the reference frame identifier.
getRefFrameString() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver: Get Coordinate system for the torque vector, for absolute frames.
getReflectivity() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the typical (50th percentile) coefficient of reflectivity.
getRefraction(double) - Method in interface org.orekit.models.AtmosphericRefractionModel: Compute the refraction angle from the true (geometrical) elevation.
getRefraction(double) - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
getRefraction(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
getRefractionModel() - Method in class org.orekit.propagation.events.ElevationDetector: Returns the currently configured refraction model.
getRefractionModel() - Method in class org.orekit.propagation.events.FieldElevationDetector: Returns the currently configured refraction model.
getRegistrationAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord: Get the web or mail address for registration.
getRemainingDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the total ΔV remaining for spacecraft.
getResults() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector: Get on all the results computed by the detector (e.g.: dates of cycle-slip).
getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the retrograde factor.
getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the retrograde factor.
getRevAtEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Get the revolution rumber.
getReversedProvider(TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils: Reverse a transform provider.
getRevolutionNumberAtEpoch() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the revolution number.
getRevolutionNumberAtEpoch() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the revolution number.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.CircularOrbit: Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.KeplerianOrbit: Get the right ascension of the ascending node.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.CircularOrbit: Get the right ascension of the ascending node derivative.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the right ascension of the ascending node derivative.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the right ascension of the ascending node derivative.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the right ascension of the ascending node derivative.
getRinexVersion() - Method in class org.orekit.gnss.RinexObservationHeader: Get Rinex Version.
getRMS() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the Root Mean Square Deviation of the fitting.
getRnml(double, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds: Get the upper bound value R^ε_n,m,l(γ).
getRnml(T, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds: Get the upper bound value R^ε_n,m,l(γ).
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get roa = R / a.
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get roa = R / a.
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get roa = R / a.
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get roa = R / a.
getRolloverReference() - Static method in class org.orekit.time.GNSSDate: Get the reference date ensuring continuity across GNSS week rollover.
getRoot() - Static method in class org.orekit.frames.Frame: Get the unique root frame.
getRotatingFrame() - Method in class org.orekit.bodies.CR3BPSystem: Get the CR3BP Rotating Frame.
getRotation() - Method in class org.orekit.attitudes.Attitude: Get the attitude rotation.
getRotation() - Method in class org.orekit.attitudes.FieldAttitude: Get the attitude rotation.
getRotation() - Method in class org.orekit.frames.FieldTransform: Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.frames.Transform: Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.utils.AngularCoordinates: Get the rotation.
getRotation() - Method in class org.orekit.utils.FieldAngularCoordinates: Get the rotation.
getRotationAcceleration() - Method in class org.orekit.attitudes.Attitude: Get the satellite rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.attitudes.FieldAttitude: Get the satellite rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.frames.FieldTransform: Get the second time derivative of the rotation.
getRotationAcceleration() - Method in class org.orekit.frames.Transform: Get the second time derivative of the rotation.
getRotationAcceleration() - Method in class org.orekit.utils.AngularCoordinates: Get the rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.utils.FieldAngularCoordinates: Get the rotation acceleration.
getRotationalAngleType() - Method in class org.orekit.files.ilrs.CPFHeader: Get the rotation angle type.
getRotationAngles() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler: Get the coordinates of the Euler angles (rad).
getRotationRate() - Method in class org.orekit.frames.FieldTransform: Get the first time derivative of the rotation.
getRotationRate() - Method in class org.orekit.frames.Transform: Get the first time derivative of the rotation.
getRotationRate() - Method in class org.orekit.utils.AngularCoordinates: Get the rotation rate.
getRotationRate() - Method in class org.orekit.utils.FieldAngularCoordinates: Get the rotation rate.
getRotationRates() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler: Get the rates of the Euler angles (rad/s).
getS() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey: Get s.
getS10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Get the EUV index (26-34 nm) scaled to F10.
getS10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Get the EUV 81-day averaged centered index.
getSample() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the states sample.
getSatConfiguration() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Gets the satellite configuration.
getSatelliteCode() - Method in class org.orekit.gnss.antenna.SatelliteAntenna: Get satellite code.
getSatelliteCount() - Method in class org.orekit.files.sp3.SP3: Get the number of satellites contained in this orbit file.
getSatelliteID() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData: Get the satellite ID.
getSatelliteID() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData: Get the satellite ID.
getSatelliteId(SatelliteSystem, int) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType: Transform the satellite ID parsed from the IGS SSR message to the real ID.
getSatelliteName() - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults: Get the satellite name.
getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the satellite id.
getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the satellite id.
getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Get the number of satellite revolutions to use for converting osculating to mean elements.
getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Get the number of satellite revolutions to use for converting osculating to mean elements.
getSatellites() - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Get the satellites related to this measurement.
getSatellites() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder: Get the satellites related to this measurement.
getSatellites() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Get the satellites related to this measurement.
getSatellites() - Method in class org.orekit.files.ccsds.ndm.adm.aem.Aem: Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm: Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.ccsds.ndm.odm.oem.Oem: Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in interface org.orekit.files.general.AttitudeEphemerisFile: Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in interface org.orekit.files.general.EphemerisFile: Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile: Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.general.OrekitEphemerisFile: Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.ilrs.CPF: Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.sp3.SP3
getSatellites() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the satellites.
getSatellitesAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader: Get parsed satellites antennas.
getSatelliteSystem() - Method in class org.orekit.gnss.antenna.SatelliteAntenna: Get satellite system.
getSatelliteSystem() - Method in class org.orekit.gnss.AppliedDCBS: Get the satellite system.
getSatelliteSystem() - Method in class org.orekit.gnss.AppliedPCVS: Get the satellite system.
getSatelliteSystem() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the satellite system.
getSatelliteSystem() - Method in class org.orekit.gnss.CombinedObservationDataSet: Get Satellite System.
getSatelliteSystem() - Method in enum org.orekit.gnss.Frequency: Get the satellite system for which this frequency is defined.
getSatelliteSystem() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmMessage: Get the satellite system associated to the message.
getSatelliteSystem() - Method in class org.orekit.gnss.navigation.RinexNavigation: Getter for the satellite system.
getSatelliteSystem() - Method in class org.orekit.gnss.ObservationDataSet: Get Satellite System.
getSatelliteSystem() - Method in class org.orekit.gnss.RinexObservationHeader: Get Satellite System.
getSatelliteSystem() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.PhaseShiftCorrection: Get the Satellite System.
getSatelliteSystem() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.ScaleFactorCorrection: Get the Satellite System.
getSatelliteType() - Method in class org.orekit.gnss.antenna.SatelliteAntenna: Get satellite type.
getSatsCorrected() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.PhaseShiftCorrection: Get the list of satellites involved.
getSaturn() - Method in interface org.orekit.bodies.CelestialBodies: Get the Saturn singleton body.
getSaturn() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Saturn singleton body.
getSaturn() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
getSBASNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation: Get all the SBAS navigation messages contained in the file.
getSBASNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation: Get the SBAS navigation messages for the given satellite Id.
getSBASOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator: Get the underlying SBAS orbital elements.
getScale() - Method in class org.orekit.utils.ParameterDriver: Get scale.
getScale() - Method in class org.orekit.utils.units.PowerTerm: Get the scaling factor.
getScale() - Method in class org.orekit.utils.units.Unit: Get the scaling factor to SI units.
getScaleFactor() - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockModifier: Get the scale factor used to compute relativistic effect.
getSclkOffsetAtEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the spacecraft clock count at OcmMetadata.getEpochT0().
getSclkSecPerSISec() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the number of spacecraft clock seconds occurring during one SI second.
getSecInDay() - Method in class org.orekit.time.GLONASSDate: Get the number of seconds since N_a start.
getSecond() - Method in class org.orekit.time.TimeComponents: Get the seconds number.
getSecondary() - Method in class org.orekit.bodies.CR3BPSystem: Get the secondary CelestialBody.
getSecondary() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector: Get the provider for the secondary satellite.
getSecondaryObject() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector: Get the secondaryObject.
getSecondaryStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange: Get the secondary ground station reflecting the signal.
getSecondsInLocalDay() - Method in class org.orekit.time.TimeComponents: Get the second number within the local day, without applying the offset from UTC.
getSecondsInUTCDay() - Method in class org.orekit.time.TimeComponents: Get the second number within the UTC day, applying the offset from UTC.
getSecondsOfWeek() - Method in class org.orekit.files.sp3.SP3: Returns the seconds of the GPS week as contained in the SP3 file.
getSegments() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris: Get the segments of the attitude ephemeris.
getSegments() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent: Get the segments.
getSegments() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris: Get the segments of the ephemeris.
getSegments() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris: Get the segments of the ephemeris.
getSegments() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris: Get the segments of the attitude ephemeris.
getSegments() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris: Get the segments of the ephemeris.
getSegments() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris: Get the segments of the attitude ephemeris.
getSegments() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris: Get the segments of the ephemeris.
getSegments() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris: Returns a list containing only this.
getSegments() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris: Returns a list containing only this.
getSelectedCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Get the selected short periodic coefficients that must be stored as additional states.
getSelectedCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Get the selected short periodic coefficients that must be stored as additional states.
getSelectedMu() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser: Select the gravitational coefficient to use.
getSelectedNormalizedParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the current value of selected normalized parameters.
getSelectedNormalizedParameters() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Get the current value of selected normalized parameters.
getSelectedOrbitalParametersDriversForBuilder(int) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel: Get the selected orbital drivers for a propagatorBuilder.
getSelectedParameters() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations: Get the selected parameters, in Jacobian matrix column order.
getSelectedParameters() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Deprecated.

Get the selected parameters, in Jacobian matrix column order.
getSelectedPropagationDriversForBuilder(int) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel: Get the selected propagation drivers for a propagatorBuilder.
getSelector() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler: Get the dates selector.
getSensors() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get description of sensors used.
getSensorsN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get number of sensors used.
getSequenceNumber() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the ephemeris sequence number.
getSerialNumber() - Method in class org.orekit.gnss.antenna.ReceiverAntenna: Get the serial number.
getShadowBodies() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get celestial bodies casting shadows.
getShadowModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get shadow model used for solar radiation pressure.
getShortPeriodTerms() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Get the short periodic terms.
getShortPeriodTermsValue(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Get the short period terms value.
getSic() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the SIC ID.
getSigma() - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter: Get the current value of sigma.
getSignalCode() - Method in enum org.orekit.gnss.ObservationType: Get the signal code.
getSignalID() - Method in class org.orekit.gnss.metric.messages.ssr.igm.CodeBias: Get the GNSS signal and tracking mode identifier.
getSignalID() - Method in class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias: Get the GNSS signal and tracking mode identifier.
getSignalStrength() - Method in class org.orekit.gnss.ObservationData: Get the signal strength.
getSignalStrengthUnit() - Method in class org.orekit.gnss.RinexObservationHeader: Get the unit of the carrier to noise ratio observables.
getSignalWideLaneIntegerIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias: Get the signal Wide-Lane integer indicator.
getSij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldFourierCjSjCoefficients: Get the coefficient S_i^j.
getSij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FourierCjSjCoefficients: Get the coefficient S_i^j.
getSinexCode() - Method in class org.orekit.gnss.antenna.Antenna: Get the sinex code of the antenna.
getSingularPoints() - Method in class org.orekit.models.earth.tessellation.AlongTrackAiming: Get points at which aiming direction cannot be computed.
getSingularPoints() - Method in class org.orekit.models.earth.tessellation.ConstantAzimuthAiming: Get points at which aiming direction cannot be computed.
getSingularPoints() - Method in class org.orekit.models.earth.tessellation.DivertedSingularityAiming: Get points at which aiming direction cannot be computed.
getSingularPoints() - Method in interface org.orekit.models.earth.tessellation.TileAiming: Get points at which aiming direction cannot be computed.
getSisa() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Getter for the signal in space accuracy (m).
getSiteCode() - Method in class org.orekit.files.sinex.Station: Get the site code (station identifier).
getSiteLocation() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients: Get the site location.
getSiteName() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients: Get the site name.
getSites() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory: Get the list of sites for which we have found coefficients, in lexicographic order ignoring case.
getSize() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Get the size of the problem.
getSize() - Method in class org.orekit.utils.LoveNumbers: Get the size of the arrays.
getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient: Get the S_j coefficient.
getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient: Get the S_j coefficient.
getSlope() - Method in class org.orekit.time.OffsetModel: Offset slope in seconds per UTC day (TAI minus UTC / dUTC).
getSlots() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the number of slots in use.
getSlotsEvictions() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the number of slots evictions.
getSma() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the semi-major axis.
getSma() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Semi-Major Axis.
getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the semi-major axis.
getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the semi-major axis.
getSnm() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data: Get the sine parameters of spherical harmonics expansion of degree N and order M.
getSnr() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement: Get the signal to noise ratio.
getSoftwareId() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Get the software configuration ID.
getSoftwareRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration: Get the software configuration record.
getSolarRadArea() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters: Get the solar radiation pressure area.
getSolarRadCoeff() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters: Get the solar radiation pressure coefficient.
getSolarSystemBarycenter() - Method in interface org.orekit.bodies.CelestialBodies: Get the solar system barycenter aggregated body.
getSolarSystemBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the solar system barycenter aggregated body.
getSolarSystemBarycenter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
getSolidPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions: Get the function computing solid pole tide (ΔC₂₁, ΔS₂₁).
getSolidTidesModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get solid tides model.
getSolution() - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution: Get the solution array.
getSolutionsSize() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Get the number of solutions found.
getSolveN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get number of solved-for states.
getSolveStates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get description of state elements solved-for.
getSource() - Method in class org.orekit.files.ilrs.CPFHeader: Get the ephemeris source.
getSource() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Gets the source of this GPS almanac.
getSource() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac: Gets the source of this QZSS almanac.
getSourceDCBS() - Method in class org.orekit.gnss.AppliedDCBS: Get the source of corrections.
getSourceIdentifier() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Get the source identifier.
getSourceIdentifier() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the source identifier.
getSourcePCVS() - Method in class org.orekit.gnss.AppliedPCVS: Get the source of corrections.
getSourceString() - Method in enum org.orekit.errors.OrekitMessages
getSourceTable() - Method in class org.orekit.gnss.metric.ntrip.NtripClient: Get a sourcetable.
getSouth() - Method in class org.orekit.bodies.FieldGeodeticPoint: Get the direction to the south of point, expressed in parent shape frame.
getSouth() - Method in class org.orekit.bodies.GeodeticPoint: Get the direction to the south of point, expressed in parent shape frame.
getSouth() - Method in class org.orekit.frames.TopocentricFrame: Get the south direction of topocentric frame, expressed in parent shape frame.
getSouthAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients: Get the amplitude along South axis.
getSouthPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients: Get the phase along South axis.
getSpacecraft() - Method in class org.orekit.forces.drag.DragForce: Get spacecraft that are sensitive to atmospheric drag forces.
getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get spacecraft shape.
getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Get spacecraft shape.
getSpacecraftBodyFrame() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints: Get the spacecraft body frame.
getSpacecraftClockAndDriftApplied() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Get the spacecraft clock offset and drift applied indicator.
getSpacecraftEpochTimeScale() - Method in class org.orekit.files.ilrs.CRDHeader: Get the spacecraft epoch time scale.
getSpacecraftParametersBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData: Get the spacecraft parameters logical block.
getSpacecraftParametersBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData: Get the spacecraft parameters logical block.
getSpacecraftParametersBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData: Get the spacecraft parameters logical block.
getSpaceWeatherEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get epoch of the Space Weather data.
getSpaceWeatherSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get Space Weather data source.
getSpan(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap: Get the time span containing a specified date.
getSpanAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition: Get the TimeSpanMap.Span valid after transition.
getSpanBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition: Get the TimeSpanMap.Span valid before transition.
getSpansNumber() - Method in class org.orekit.utils.TimeSpanMap: Get the number of spans.
getSpatialFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the spatial filter.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.adm.AdmParser: Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.NdmParser: Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser: Get the non-default token builders for special XML elements.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser: Get the non-default token builders for special XML elements.
getSpecifier() - Method in interface org.orekit.errors.LocalizedException: Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitException: Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitIllegalArgumentException: Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitIllegalStateException: Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitInternalError: Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitIOException: Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitParseException: Get the localizable specifier of the error message.
getSpectralFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the spectral filter.
getSphericalHarmonicsDegree() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data: Get the degree of spherical harmonic expansion.
getSphericalHarmonicsOrder() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data: Get the order of spherical harmonic expansion.
getSpin() - Method in class org.orekit.attitudes.Attitude: Get the satellite spin.
getSpin() - Method in class org.orekit.attitudes.FieldAttitude: Get the satellite spin.
getSpin() - Method in class org.orekit.models.earth.ReferenceEllipsoid: Gets the rotation of the ellipsoid about its axis.
getSpinAlpha() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Get the right ascension of spin axis vector (rad).
getSpinAngle() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Get the phase of the satellite about the spin axis (rad).
getSpinAngleVel() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Get the angular velocity of satellite around spin axis (rad/s).
getSpinDelta() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Get the declination of the spin axis vector (rad).
getSpinStabilizedBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData: Get the spin-stabilized logical block.
getSquaredDistance() - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution: Get the squared distance to the corresponding float solution.
getSrpCoefficient() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the nominal SRP coefficient.
getSrpConstantArea() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the attitude-independent SRP area, not already into attitude-dependent area along OEB.
getSrpModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get Solar Radiation Pressure model.
getSrpUncertainty() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the SRP coefficient 1σ uncertainty.
getSsrEpoch1s() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader: Get the SSR Epoch Time 1s.
getSsrIgm01Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01: Get the SSR IGM01 data parsed in the SSR message.
getSsrIgm02Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02: Get the SSR IGM02 data parsed in the SSR message.
getSsrIgm03Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03: Get the SSR IGM03 data parsed in the SSR message.
getSsrIgm04Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04: Get the SSR IGM04 data parsed in the SSR message.
getSsrIgm05Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05: Get the SSR IGM05 data parsed in the SSR message.
getSsrIgm06Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06: Get the SSR IGM06 data parsed in the SSR message.
getSsrIgm07Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07: Get the SSR IGM07 data parsed in the SSR message.
getSsrMultipleMessageIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader: Get the SSR Multiple Message Indicator.
getSsrProviderId() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader: Get the SSR Provider ID.
getSsrSolutionId() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader: Get the SSR Solution ID.
getSsrUpdateInterval() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader: Get the SSR Update Interval.
getSsrUra() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data: Get the SSR User Range Accuracy (URA).
getStandardModel(double) - Static method in class org.orekit.models.earth.troposphere.MariniMurrayModel: Create a new Marini-Murray model using a standard atmosphere model.
getStandardModel(double) - Static method in class org.orekit.models.earth.troposphere.MendesPavlisModel: Create a new Mendes-Pavlis model using a standard atmosphere model.
getStandardModel() - Static method in class org.orekit.models.earth.troposphere.SaastamoinenModel: Create a new Saastamoinen model using a standard atmosphere model.
getStart() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder: Get the start of the measurements time span.
getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris: Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment: Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris: Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory: Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris: Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment: Get the start date of this ephemeris segment.
getStart() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment: Get the start date of this ephemeris segment.
getStart() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris: Get the start date of the ephemeris.
getStart() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment: Get the start date of this ephemeris segment.
getStart() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris: Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment: Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris: Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment: Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris: Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris: Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
getStart() - Method in class org.orekit.time.OffsetModel: Get the date of the offset start.
getStart() - Method in class org.orekit.utils.TimeSpanMap.Span: Get the start of this time span.
getStartDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the start date.
getStartDate() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers: Get the start date.
getStartDate() - Method in class org.orekit.frames.EOPHistory: Get the date of the first available Earth Orientation Parameters.
getStartDate() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock: Getter for the validity period start date.
getStartDate() - Method in class org.orekit.propagation.AbstractPropagator: Get the start date.
getStartDate() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get the start date.
getStartDetector() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger: Getter for the firing start detector.
getStartDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector: Get the driver for start date.
getStartDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector: Get the driver for start date.
getStartEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the starting epoch (UTC).
getStartFiringDetector() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers: Getter for the start firing detector.
getStartTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get start of total time span covered by attitude data.
getStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the time of the earliest data contained in the OCM.
getStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata: Get start of total time span covered by ephemerides data and covariance data.
getStartTime() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the startTime.
getStartTransition() - Method in class org.orekit.utils.TimeSpanMap.Span: Get the transition at start of this time span.
getState(IonosphericModel) - Method in class org.orekit.estimation.measurements.modifiers.IonosphericGradientConverter: Get the state with the number of parameters consistent with ionospheric model.
getState(DiscreteTroposphericModel) - Method in class org.orekit.estimation.measurements.modifiers.TroposphericGradientConverter: Get the state with the number of parameters consistent with tropospheric model.
getState() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter: Get the state with the number of parameters consistent with the propagation model.
getState() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent: Get the triggering state.
getState() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent: Get the triggering state.
getState() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event: Get the spacecraft's state at the event.
getState() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event: Get the spacecraft's state at the event.
getStateDerivatives(int) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the partial derivatives of the simulated measurement with respect to state Cartesian coordinates.
getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.analytical.tle.TLEJacobiansMapper: Get the Jacobian with respect to state from a one-dimensional additional state array.
getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper: Get the Jacobian with respect to state from a one-dimensional additional state array.
getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper: Get the Jacobian with respect to state from a one-dimensional additional state array.
getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper: Get the Jacobian with respect to state from a one-dimensional additional state array.
getStates() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the states of the spacecrafts.
getStateSize() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get state size.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester: Extract state transition matrix from state.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester: Extract state transition matrix from state.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper: Extract state transition matrix from state.
getStateTransitionMatrix(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester: Extract state transition matrix from state.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations: Method returning the State Transition Matrix.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester: Extract state transition matrix from state.
getStateType() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder: Get the type of the elements used to define the orbital state (mean or osculating).
getStateVectorBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData: Get the state vector logical block.
getStation() - Method in class org.orekit.estimation.measurements.AngularAzEl: Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.AngularRaDec: Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.gnss.Phase: Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.Range: Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.RangeRate: Get the ground station from which measurement is performed.
getStation(String) - Method in class org.orekit.files.sinex.SinexLoader: Get the station corresponding to the given site code.
getStationClockAndDriftApplied() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Get the station clock offset and drift applied indicator.
getStationIdentifier() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the station identifier.
getStationName() - Method in class org.orekit.files.ilrs.CRDHeader: Get the station name from official list.
getStationName() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the station name.
getStationNetword() - Method in class org.orekit.files.ilrs.CRDHeader: Get the station network.
getStationOscDrift() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Get the estimated station oscillator drift in parts in 10¹⁵.
getStations() - Method in class org.orekit.files.sinex.SinexLoader: Get the parsed station data.
getStationUTCOffset() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Get the estimated station UTC offset.
getStatus() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the status.
getStep() - Method in class org.orekit.files.ilrs.CPFHeader: Get the time between table entries.
getStep() - Method in class org.orekit.frames.InterpolatingTransformProvider: Get the grid points time step.
getStep() - Method in class org.orekit.frames.ShiftingTransformProvider: Get the grid points time step.
getStmName() - Method in class org.orekit.propagation.AbstractMatricesHarvester: Get the State Transition Matrix state name.
getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris: Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment: Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris: Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory: Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris: Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment: Get the end date of this ephemeris segment.
getStop() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment: Get the end date of this ephemeris segment.
getStop() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris: Get the end date of the ephemeris.
getStop() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment: Get the end date of this ephemeris segment.
getStop() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris: Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment: Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris: Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment: Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris: Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris: Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
getStopDate() - Method in class org.orekit.propagation.events.EventState.EventOccurrence: Get the new time for a stop action.
getStopDate() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence: Get the new time for a stop action.
getStopDetector() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger: Getter for the firing stop detector.
getStopDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector: Get the driver for stop date.
getStopDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector: Get the driver for stop date.
getStopFiringDetector() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers: Getter for the stop firing detector.
getStopTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get end of total time span covered by attitude data.
getStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the time of the latest data contained in the OCM.
getStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata: Get end of total time span covered by ephemerides data and covariance data.
getStopTime() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the stopTime.
getStream(T) - Method in class org.orekit.data.AbstractListCrawler: Get the stream to read from an input.
getStream(File) - Method in class org.orekit.data.FilesListCrawler: Get the stream to read from an input.
getStream(URL) - Method in class org.orekit.data.NetworkCrawler: Get the stream to read from an input.
getStreamInfoAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord: Get the web address for stream information.
getStrengthLevel() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: Get the strength level for activity.
getStuffReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector: Get the stuff (all the things needed for, the detector).
getSubDailySequenceNumber() - Method in class org.orekit.files.ilrs.CPFHeader: Get the sub-daily ephemeris sequence number.
getSun() - Method in interface org.orekit.bodies.CelestialBodies: Get the Sun singleton body.
getSun() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Sun singleton body.
getSun() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
getSun() - Method in class org.orekit.forces.gravity.DeSitterRelativity: Get the sun model used to compute De Sitter effect.
getSunEarthCR3BP(AbsoluteDate, TimeScale) - Static method in class org.orekit.bodies.CR3BPFactory: Get the Sun-Earth CR3BP singleton bodies pair.
getSunJupiterCR3BP(AbsoluteDate, TimeScale) - Static method in class org.orekit.bodies.CR3BPFactory: Get the Sun-Jupiter CR3BP singleton bodies pair.
getSupportedNames() - Method in class org.orekit.data.AbstractSelfFeedingLoader: Get the supported names regular expression.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader: Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.gnss.SEMParser
getSupportedNames() - Method in class org.orekit.gnss.YUMAParser
getSupportedNames() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
getSupportedNames() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
getSupportedNames() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
getSupportedNames() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage: Getter for the user SV accuray (meters).
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage: Getter for the user SV accuray (meters).
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage: Getter for the user SV accuray (meters).
getSvHealth() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data: Get the satellite health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Getter for the SV health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage: Getter for the satellite health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage: Getter for the satellite health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage: Getter for the satellite health status.
getSVN() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Gets the satellite "SVN" reference number.
getSystem(CelestialBody, CelestialBody, double) - Static method in class org.orekit.bodies.CR3BPFactory: Get the corresponding CR3BP System.
getSystemId() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration: Get the system configuration ID.
getSystemIdentifier() - Method in class org.orekit.files.ilrs.CRDHeader: Get the system identifier.
getSystemNumber() - Method in class org.orekit.files.ilrs.CRDHeader: Get the system number.
getSystemObservationTypes() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the different observation type for each satellite system.
getSystemOccupancy() - Method in class org.orekit.files.ilrs.CRDHeader: Get the system occupancy.
getSystemRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration: Get the system configuration record.
getTabDensity() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester: Get the current density table.
getTable() - Method in class org.orekit.attitudes.TabulatedLofOffset: Get an unmodifiable view of the tabulated attitudes.
getTAI() - Method in class org.orekit.time.LazyLoadedTimeScales
getTAI() - Method in interface org.orekit.time.TimeScales: Get the International Atomic Time scale.
getTAI() - Static method in class org.orekit.time.TimeScalesFactory: Get the International Atomic Time scale.
getTaimutcT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the difference (TAI – UTC) in seconds at epoch OcmMetadata.getEpochT0().
getTargetClass() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the target class.
getTargetLocation() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the target location.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing: Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing: Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing: Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing: Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing: Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing: Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.NadirPointing: Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.NadirPointing: Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TargetPointing: Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TargetPointing: Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the target point position/velocity in specified frame.
getTargetSize() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the size of the target.
getTauC() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS time scale correction to UTC time.
getTauGps() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the correction to GPS time relative to GLONASS time.
getTauMultiplier() - Method in class org.orekit.models.earth.displacement.Tide: Get the multiplier for the τ Doodson argument.
getTC() - Method in class org.orekit.data.DelaunayArguments: Get the offset in Julian centuries.
getTC() - Method in class org.orekit.data.FieldDelaunayArguments: Get the offset in Julian centuries.
getTCB() - Method in class org.orekit.time.LazyLoadedTimeScales
getTCB() - Method in interface org.orekit.time.TimeScales: Get the Barycentric Coordinate Time scale.
getTCB() - Static method in class org.orekit.time.TimeScalesFactory: Get the Barycentric Coordinate Time scale.
getTCG() - Method in class org.orekit.time.LazyLoadedTimeScales
getTCG() - Method in interface org.orekit.time.TimeScales: Get the Geocentric Coordinate Time scale.
getTCG() - Static method in class org.orekit.time.TimeScalesFactory: Get the Geocentric Coordinate Time scale.
getTDB() - Method in class org.orekit.time.LazyLoadedTimeScales
getTDB() - Method in interface org.orekit.time.TimeScales: Get the Barycentric Dynamic Time scale.
getTDB() - Static method in class org.orekit.time.TimeScalesFactory: Get the Barycentric Dynamic Time scale.
getTdim() - Method in class org.orekit.bodies.CR3BPSystem: Get the CR3BP orbital period of m2 around m1.
getTdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the Unique identifier of Tracking Data Message linked to this Orbit Data Message.
getTdop() - Method in class org.orekit.gnss.DOP: Gets the time dilution of precision.
getTEC(AbsoluteDate, GeodeticPoint) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel: Computes the Total Electron Content (TEC) at a given date by performing a temporal interpolation with the two closest date in the IONEX file.
getTEC(FieldAbsoluteDate<T>, GeodeticPoint) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel: Computes the Total Electron Content (TEC) at a given date by performing a temporal interpolation with the two closest date in the IONEX file.
getTechAddress() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the address of Technical Point Of Contact at originator.
getTechOrg() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the creating agency or operator.
getTechPhone() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the phone number of Technical Point Of Contact at originator.
getTechPOC() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the Technical Point Of Contact at originator.
getTechPosition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the position of Technical Point Of Contact at originator.
getTEME() - Method in class org.orekit.frames.AbstractFrames
getTEME() - Method in interface org.orekit.frames.Frames: Get the TEME reference frame.
getTEME() - Static method in class org.orekit.frames.FramesFactory: Get the TEME reference frame.
getTemperature() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement: Get the surface temperature.
getTemperature() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Get the local temperature at the evaluation location.
getTemperature() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model: Returns the temperature at the station [K].
getTemperature() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel: Get the atmospheric temperature of the station depending its position.
getTemplateTLE() - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder: Getter for the template TLE.
getTempSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Get the temperature sensor manufacturer.
getTempSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Get the temperature sensor model.
getTempSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Get the temperature sensor serial number.
getTFirstObs() - Method in class org.orekit.gnss.RinexObservationHeader: Get the time of First observation record.
getTGD() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements: Gets the estimated group delay differential TGD for L1-L2 correction.
getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Gets for the Group Delay Differential (s).
getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage: Getter for the Group Delay Differential (s).
getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage: Getter for the estimated group delay differential TGD for L5-S correction.
getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage: Getter for the Group Delay Differential (s).
getTGD1() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage: Getter for the estimated group delay differential TGD1 for B1I signal.
getTGD2() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage: Getter for the estimated group delay differential TGD for B2I signal.
getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Get the theoretical standard deviation.
getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder: Get the theoretical standard deviation.
getTheoreticalStandardDeviation() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Get the theoretical standard deviation.
getTheta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext: Get Central body rotation angle θ.
getTheta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext: Get Central body rotation angle θ.
getTheta0() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction: Get the station elevation angle under free-space propagation .
getThetaMin() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction: Get the station minimal elevation angle.
getThreeHourlyAp() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the array of the eight three-hourly Ap indices for the current entry.
getThreeHourlyAp(int) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the three-hourly Ap index at index i from the threeHourlyAp array.
getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Get the value of the 3 hours geomagnetic index.
getThreeHourlyKp() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the array of the eight three-hourly Kp indices for the current entry.
getThreeHourlyKp(int) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the three-hourly Kp index at index i from the threeHourlyKp array.
getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: Get the value of the 3 hours geomagnetic index.
getThreeHourlyKP(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters: Get the value of the 3 hours geomagnetic index.
getThreshold() - Method in class org.orekit.propagation.events.AbstractDetector: Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.AdapterDetector: Get the convergence threshold in the event time search.
getThreshold() - Method in interface org.orekit.propagation.events.EventDetector: Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.FieldAbstractDetector: Get the convergence threshold in the event time search.
getThreshold() - Method in interface org.orekit.propagation.events.FieldEventDetector: Get the convergence threshold in the event time search.
getThrust() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get thrust.
getThrust() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver: Get the thrust.
getThrust() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the thrust.
getThrust() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the thrust value (N).
getThrust(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the thrust norm (N).
getThrustDirectionProvider() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver: Getter on Thrust direction and spaceraft attitude provided by an external object.
getThrustDirectionSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get one σ angular off-nominal thrust direction.
getThrustEfficiency() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get thrust efficiency η.
getThrusterAxisInSatelliteFrame() - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider: Thruster axis in satellite frame.
getThrustInterpolation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get interpolation mode between current and next thrust line.
getThrustIsp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get thrust specific impulse.
getThrustMagnitudeSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Get one σ percent error on thrust magnitude.
getThrustVector() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the thrust vector (N) in S/C frame.
getThrustVector(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getTidalDisplacementFrequencyCorrectionDiurnal() - Method in enum org.orekit.utils.IERSConventions: Get the correction function for tidal displacement for diurnal tides.
getTidalDisplacementFrequencyCorrectionDiurnal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions: Get the correction function for tidal displacement for diurnal tides.
getTidalDisplacementFrequencyCorrectionZonal() - Method in enum org.orekit.utils.IERSConventions: Get the correction function for tidal displacement for zonal tides.
getTidalDisplacementFrequencyCorrectionZonal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions: Get the correction function for tidal displacement for zonal tides.
getTide(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients: Get the tide.
getTideFrequencyDependenceFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions: Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).
getTideFrequencyDependenceFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions: Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).
getTideSystem() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the TideSystem used in the gravity field.
getTideSystem() - Method in interface org.orekit.forces.gravity.potential.TideSystemProvider: Get the TideSystem used in the gravity field.
getTime() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the reference time of the GNSS orbit as a duration from week start.
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Get the Reference Time.
getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the Reference Time.
getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Reference Time of the GNSS orbit as a duration from week start.
getTime() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Gets the Reference Time of the SBAS orbit in GPS seconds of the week.
getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Gets the Reference Time of the SBAS orbit in GPS seconds of the week.
getTime() - Method in class org.orekit.time.DateTimeComponents: Get the time component.
getTime() - Method in class org.orekit.utils.units.Unit: Get the time exponent.
getTimeConverter() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter: Get the current time converter.
getTimeOfFlight() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement: Get the time-of-flight.
getTimeOffset() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the time offset from first state date to measurement date.
getTimer() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration: Get the timer name.
getTimerSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration: Get the timer serial number.
getTimeScale() - Method in class org.orekit.files.ccsds.definitions.TimeConverter: Get the base time scale.
getTimeScale() - Method in class org.orekit.files.ilrs.CPF: Get the time scale used in CPF file.
getTimeScale() - Method in class org.orekit.files.ilrs.CRDParser: Get the time scale used to read the file.
getTimeScale() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the data time scale.
getTimeScale(TimeScales) - Method in enum org.orekit.gnss.TimeSystem: Get the time scale corresponding to time system.
getTimeScales() - Method in class org.orekit.data.CompositeDataContext
getTimeScales() - Method in interface org.orekit.data.DataContext: Get a factory for constructing TimeScales based on the auxiliary data in this context.
getTimeScales() - Method in class org.orekit.data.ExceptionalDataContext
getTimeScales() - Method in class org.orekit.data.LazyLoadedDataContext
getTimeScales() - Method in class org.orekit.frames.AbstractFrames: Get the time scales.
getTimeScales() - Method in class org.orekit.frames.EOPHistory: Get the time scales used in computing EOP corrections.
getTimeScales() - Static method in class org.orekit.time.TimeScalesFactory: Get the instance of TimeScales that is called by all of the static methods in this class.
getTimeSinceFirstObservation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get time elapsed between first accepted observation on epoch.
getTimeSinceLastObservation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get time elapsed between last accepted observation on epoch.
getTimeSource() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration: Get the time source.
getTimeSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the span of time in seconds that the OCM covers.
getTimeSystem() - Method in class org.orekit.files.ccsds.section.Metadata: Get the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.
getTimeSystem() - Method in class org.orekit.files.ccsds.utils.ContextBinding: Get the time system.
getTimeSystem() - Method in class org.orekit.files.sp3.SP3: Returns the TimeSystem used to time-stamp position entries.
getTimeSystem() - Method in class org.orekit.gnss.clock.RinexClock: Getter for the file time system.
getTimeSystemCorrectionA0() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection: Getter for the A0 coefficient of the time system correction.
getTimeSystemCorrectionA1() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection: Getter for the A1 coefficient of the time system correction.
getTimeSystemCorrections() - Method in class org.orekit.gnss.navigation.RinexNavigation: Getter for the time system corrections contained in the file header.
getTimeSystemCorrectionSecOfWeek() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection: Getter for the reference time of the time system correction polynomial.
getTimeSystemCorrectionType() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection: Getter for the time system correction type.
getTimeSystemCorrectionWeekNumber() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection: Getter for the reference week number of the time system correction polynomial.
getTimetagRef() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the timetagRef.
getTimingRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration: Get the timing system configuration record.
getTIRF(IERSConventions) - Method in class org.orekit.frames.AbstractFrames
getTIRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
getTIRF(IERSConventions) - Method in interface org.orekit.frames.Frames: Get the TIRF reference frame, ignoring tidal effects.
getTIRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames: Get the TIRF reference frame.
getTIRF(IERSConventions) - Static method in class org.orekit.frames.FramesFactory: Get the TIRF reference frame, ignoring tidal effects.
getTIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the TIRF reference frame.
getTk() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the time referenced to the beginning of the frame within the current day.
getTLastObs() - Method in class org.orekit.gnss.RinexObservationHeader: Get the time of last observation record.
getTLE() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Get the underlying TLE.
getTLE() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the underlying TLE.
getTLEBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData: Get the TLE logical block.
getTN() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Get the correction to the satellite time relative to GLONASS system time.
getTN() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the correction to the satellite time relative to GLONASS system time.
getTo() - Method in class org.orekit.utils.units.UnitsConverter: Get the destination unit.
getToc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements: Gets the clock correction reference time toc.
getToc() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Gets the clock correction reference time toc.
getTOD(boolean) - Method in class org.orekit.frames.AbstractFrames
getTOD(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
getTOD(boolean) - Method in interface org.orekit.frames.Frames: Get the TOD reference frame.
getTOD(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames: Get the TOD reference frame.
getTOD(boolean) - Static method in class org.orekit.frames.FramesFactory: Get the TOD reference frame.
getTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the TOD reference frame.
getTon2a() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext: Get ton2a = 2 / (n² * a).
getTon2a() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext: Get ton2a = 2 / (n² * a).
getTool() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade: Get the tool used for OD.
getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationDetector: Returns the currently configured topocentric frame definitions.
getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationExtremumDetector: Returns the topocentric frame centered on ground point.
getTopocentricFrame() - Method in class org.orekit.propagation.events.FieldElevationDetector: Returns the currently configured topocentric frame definitions.
getTorque() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver: Get the torque vector (N.m).
getTotalEclipse() - Method in class org.orekit.propagation.events.EclipseDetector: Get the total eclipse detection flag.
getTotalEclipse() - Method in class org.orekit.propagation.events.FieldEclipseDetector: Get the total eclipse detection flag.
getTotalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements: Returns the total intensity of the magnetic field (= norm of the field vector).
getTotalLightingRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get the total lighting ratio ([0-1]).
getTotalLightingRatio(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get the total lighting ratio ([0-1]).
getTotalNumberOfDataLines() - Method in class org.orekit.gnss.clock.RinexClock: Get the total number of complete data lines in the file.
getTrackId() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the tracking data identifier.
getTrackingSoftwares() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Get the tracking softwares.
getTrackingSoftwareVersions() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Get the tracking software versions.
getTracksAvailable() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get number of sensors tracks available for the OD within the actual OD span.
getTracksUsed() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get number of sensors tracks accepted for the OD within the actual OD span.
getTrajBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get basis of this trajectory state time history data.
getTrajBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get identification number of the orbit determination or simulation upon which this trajectory is based.
getTrajectoryStates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory: Get the trajectory states.
getTrajFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get epoch of the trajectory reference frame.
getTrajID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get trajectory identification number.
getTrajNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get identification number of next trajectory.
getTrajPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get identification number of previous trajectory.
getTrajReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get reference frame of the trajectory.
getTrajType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get trajectory element set type.
getTrajUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get trajectory element set units.
getTransform(AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<Gradient>, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get the transform with derivatives.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.EclipticProvider
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EclipticProvider
getTransform(AbsoluteDate) - Method in class org.orekit.frames.FixedTransformProvider: Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.FixedTransformProvider: Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider: Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider: Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation: Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.HelmertTransformation: Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.InterpolatingTransformProvider: Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.InterpolatingTransformProvider: Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter: Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter: Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.L1TransformProvider: Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.L1TransformProvider: Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.ShiftingTransformProvider: Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ShiftingTransformProvider: Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider: Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in interface org.orekit.frames.TransformProvider: Get the FieldTransform corresponding to specified date.
getTransformation() - Method in enum org.orekit.frames.HelmertTransformation.Predefined: Get the underlying HelmertTransformation.
getTransformation(TimeScale) - Method in enum org.orekit.frames.HelmertTransformation.Predefined: Get the underlying HelmertTransformation.
getTransformProvider() - Method in class org.orekit.frames.Frame: Get the provider for transform from parent frame to instance.
getTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame: Get the transform from the instance to another frame.
getTransformTo(Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.Frame: Get the transform from the instance to another frame.
getTransitions() - Method in class org.orekit.forces.drag.TimeSpanDragForce: Deprecated.
as of 11.1, replaced by TimeSpanDragForce.getFirstSpan()
getTransitions() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration: Deprecated.
as of 11.1, replace by TimeSpanParametricAcceleration.getFirstSpan()
getTransitions() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel: Deprecated.
as of 11.1, replaced by TimeSpanEstimatedTroposphericModel.getFirstSpan()
getTransitions() - Method in class org.orekit.utils.FieldTimeSpanMap: Get an unmodifiable view of the sorted transitions.
getTransitions() - Method in class org.orekit.utils.TimeSpanMap: Deprecated.
as of 11.1, replaced by TimeSpanMap.getFirstSpan(), TimeSpanMap.getLastSpan(), TimeSpanMap.getFirstTransition(), TimeSpanMap.getLastTransition(), and TimeSpanMap.getSpansNumber()
getTranslation() - Method in class org.orekit.frames.FieldTransform: Get the underlying elementary translation.
getTranslation() - Method in class org.orekit.frames.Transform: Get the underlying elementary translation.
getTransmissionOfSpectralFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the percentage of transmission of spectral filter.
getTransmitBand() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the transmitBand.
getTransmitDelays() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the transmitDelays.
getTranspClkRef() - Method in class org.orekit.files.ilrs.CPFHeader: Get the transponder Clock Reference Time.
getTranspClkRefTime() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Get the transponder clock reference time.
getTransponderId() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Get the transponder configuration ID.
getTransponderRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration: Get the transponder configuration record.
getTranspOscDrift() - Method in class org.orekit.files.ilrs.CPFHeader: Get the transponder Oscillator Drift in parts in 10^15.
getTranspOscDrift() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Get the estimated transponder oscillator drift in parts in 10¹⁵.
getTranspTransmitDelay() - Method in class org.orekit.files.ilrs.CPFHeader: Get the transponder transmit delay.
getTranspUtcOffset() - Method in class org.orekit.files.ilrs.CPFHeader: Get the transponder UTC offset.
getTranspUTCOffset() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Get the estimated transponder UTC offset.
getTrigger() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Get the triggering event.
getTriggeredEnd() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers: Getter for the triggered date of engine stop.
getTriggeredIncreasing() - Method in enum org.orekit.propagation.events.FilterType: Get the increasing status of triggered events.
getTriggeredStart() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers: Getter triggered date of engine start.
getTroposphericModel(AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel: Get the EstimatedTroposphericModel model valid at a date.
getTrueAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the true anomaly.
getTrueAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit: Get the true anomaly.
getTrueAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the true anomaly derivative.
getTrueAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the true anomaly derivative.
getTT() - Method in class org.orekit.time.LazyLoadedTimeScales
getTT() - Method in interface org.orekit.time.TimeScales: Get the Terrestrial Time scale.
getTT() - Static method in class org.orekit.time.TimeScalesFactory: Get the Terrestrial Time scale.
getTurnaroundDenominator() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the turnaroundDenominator.
getTurnaroundNumerator() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the turnaroundNumerator.
getTypAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.
getType() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade: Get the method type.
getType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Covariance: Get the type of the elements.
getType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState: Get the type of the elements.
getType() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation: Get the type of observation.
getType() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the type of the token.
getType() - Method in class org.orekit.files.sp3.SP3: Returns the SP3.SP3FileType associated with this SP3 file.
getType() - Method in class org.orekit.gnss.antenna.Antenna: Get the type of the antenna.
getType() - Method in class org.orekit.orbits.CartesianOrbit: Get the orbit type.
getType() - Method in class org.orekit.orbits.CircularOrbit: Get the orbit type.
getType() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldOrbit: Get the orbit type.
getType() - Method in class org.orekit.orbits.KeplerianOrbit: Get the orbit type.
getType() - Method in class org.orekit.orbits.Orbit: Get the orbit type.
getTypeCode() - Method in class org.orekit.gnss.metric.messages.ParsedMessage: Get the code for the message type.
getTypeObs() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.PhaseShiftCorrection: Get the Carrier Phase Observation Code.
getTypesObsScaled() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.ScaleFactorCorrection: Get the list of Observation Types scaled.
getU() - Method in class org.orekit.bodies.Ellipse: Get the unit vector along the major axis.
getU1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients: Get the coefficient U₁^j for Fourier index i.
getU1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients: Get the coefficient U₁^j for Fourier index i.
getU2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients: Get the coefficient U₂^j for Fourier index = 1 (i == 0).
getU2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients: Get the coefficient U₂^j for Fourier index = 1 (i == 0).
getUnderlyingAttitudeProvider() - Method in interface org.orekit.attitudes.AttitudeProviderModifier: Get the underlying attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.SpinStabilized: Get the underlying attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawCompensation: Get the underlying (ground pointing) attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawSteering: Get the underlying (ground pointing) attitude provider.
getUndulation(double, double, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid: Gets the Undulation of the Geoid, N at the given position.
getUnit() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Get the field unit.
getUnits() - Method in enum org.orekit.files.ccsds.definitions.ElementsType: Get the elements units.
getUnits() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the units.
getUnits(String) - Method in class org.orekit.utils.units.UnitsCache: Get units from a string specification.
getUnnormalizationFactors(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get a un-normalization factors array.
getUnnormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics: Get a spherical harmonic cosine coefficient.
getUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the gravity field coefficients provider from the first supported file.
getUnnormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Create a time-independent UnnormalizedSphericalHarmonicsProvider from canonical coefficients.
getUnnormalizedProvider(NormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Create an UnnormalizedSphericalHarmonicsProvider from a NormalizedSphericalHarmonicsProvider.
getUnnormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields: Get a gravity field unnormalized coefficients provider.
getUnnormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields: Get a gravity field unnormalized coefficients provider.
getUnnormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics: Get a spherical harmonic sine coefficient.
getUpperCaseAbbreviation() - Method in enum org.orekit.time.Month: Get the upper case three letters abbreviation.
getUpperCaseName() - Method in enum org.orekit.time.Month: Get the upper case full name.
getURA() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Gets the average URA number.
getURA() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage: Getter for the user range accuray (meters).
getURA() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Getter for the user range accuray (meters).
getUranus() - Method in interface org.orekit.bodies.CelestialBodies: Get the Uranus singleton body.
getUranus() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Uranus singleton body.
getUranus() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get start of useable time span covered by attitude data.
getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata: Get start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get end of useable time span covered by ephemerides data.
getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata: Get end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUsedObservationData() - Method in class org.orekit.gnss.CombinedObservationData: Get the list of observation data used to perform the combination of measurements.
getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData: Get user defined parameters logical block.
getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData: Get the user defined parameters logical block.
getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData: Get the user defined parameters logical block.
getUT1(EOPHistory) - Method in class org.orekit.time.AbstractTimeScales: Get the Universal Time 1 scale.
getUT1(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
getUT1(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
getUT1(EOPHistory) - Method in class org.orekit.time.LazyLoadedTimeScales: Get the Universal Time 1 scale.
getUT1(IERSConventions, boolean) - Method in interface org.orekit.time.TimeScales: Get the Universal Time 1 scale.
getUT1(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory: Get the Universal Time 1 scale.
getUT1(EOPHistory) - Static method in class org.orekit.time.TimeScalesFactory: Get the Universal Time 1 scale.
getUT1MinusUTC() - Method in class org.orekit.frames.EOPEntry: Get the UT1-UTC value.
getUT1MinusUTC(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the UT1-UTC value.
getUT1MinusUTC(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory: Get the UT1-UTC value.
getUt1mutcT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the difference (UT1 – UTC) in seconds at epoch OcmMetadata.getEpochT0().
getUtc() - Method in class org.orekit.frames.AbstractEopLoader: Get the UTC time scale.
getUtc() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the UTC time scale used to create this TLE.
getUTC() - Method in class org.orekit.time.LazyLoadedTimeScales
getUTC() - Method in interface org.orekit.time.TimeScales: Get the Universal Time Coordinate scale.
getUTC() - Static method in class org.orekit.time.TimeScalesFactory: Get the Universal Time Coordinate scale.
getUTCScale() - Method in class org.orekit.time.UT1Scale: Get the associated UTC scale.
getUTCTAIOffsets() - Method in class org.orekit.time.UTCScale: Returns the UTC-TAI offsets underlying this UTC scale.
getV() - Method in class org.orekit.bodies.Ellipse: Get the unit vector along the minor axis.
getV1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients: Get the coefficient V₁^j for Fourier index i.
getV1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients: Get the coefficient V₁^j for Fourier index i.
getV2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients: Get the coefficient V₂^j for Fourier index = 1 (i == 0).
getV2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients: Get the coefficient V₂^j for Fourier index = 1 (i == 0).
getValidFrom() - Method in class org.orekit.files.sinex.Station: Get start of validity.
getValidFrom() - Method in class org.orekit.gnss.antenna.SatelliteAntenna: Get start of validity.
getValidityStart() - Method in class org.orekit.time.UTCTAIOffset: Get the start time of validity for this offset.
getValidUntil() - Method in class org.orekit.files.sinex.Station: Get end of validity.
getValidUntil() - Method in class org.orekit.gnss.antenna.SatelliteAntenna: Get end of validity.
getValue() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
getValue() - Method in class org.orekit.gnss.CombinedObservationData: Get the combined observed value.
getValue() - Method in class org.orekit.gnss.ObservationData: Get the observed value.
getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction: Get Γ function value.
getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction: Get Γ function value.
getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear: Compute the value of the Hansen coefficient K_j^{-n-1, s}.
getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear: Compute the value of the Hansen coefficient K₀^{n, s}.
getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear: Get the K₀^-n-1,s coefficient value.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear: Compute the value of the Hansen coefficient K_j^{-n-1, s}.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear: Compute the value of the Hansen coefficient K₀^{n, s}.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear: Get the K₀^-n-1,s coefficient value.
getValue(int, int, int, Gradient) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials: Returns the value and derivatives of the Jacobi polynomial P_l^v,w evaluated at γ.
getValue(int, int, int, FieldGradient<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials: Returns the value and derivatives of the Jacobi polynomial P_l^v,w evaluated at γ.
getValue(int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.NewcombOperators: Get the Newcomb operator evaluated at n, s, ρ, σ.
getValue() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry: Get the value.
getValue() - Method in class org.orekit.utils.FieldArrayDictionary.Entry: Get the value.
getValue() - Method in class org.orekit.utils.ParameterDriver: Get current parameter value.
getValue(int, Map<String, Integer>) - Method in class org.orekit.utils.ParameterDriver: Get the value as a gradient.
getValuesSamples() - Method in class org.orekit.utils.InterpolationTableLoader: Returns a copy of the values samples for the interpolation function.
getVdim() - Method in class org.orekit.bodies.CR3BPSystem: Get the CR3BP orbital velocity of m2.
getVdop() - Method in class org.orekit.gnss.DOP: Gets the vertical dilution of precision.
getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get equinoctial frame vector f.
getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get equinoctial frame vector f.
getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get equinoctial frame vector g.
getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get equinoctial frame vector g.
getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get equinoctial frame vector w.
getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get equinoctial frame vector w.
getVeis1950() - Method in class org.orekit.frames.AbstractFrames
getVeis1950() - Method in interface org.orekit.frames.Frames: Get the VEIS 1950 reference frame.
getVeis1950() - Static method in class org.orekit.frames.FramesFactory: Get the VEIS 1950 reference frame.
getVelocity() - Method in class org.orekit.estimation.measurements.PV: Get the velocity.
getVelocity() - Method in class org.orekit.files.sinex.Station: Get the station velocity.
getVelocity() - Method in class org.orekit.frames.FieldTransform: Get the first time derivative of the translation.
getVelocity() - Method in class org.orekit.frames.Transform: Get the first time derivative of the translation.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere: Get the inertial velocity of atmosphere molecules.
getVelocity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere: Get the inertial velocity of atmosphere molecules.
getVelocity() - Method in class org.orekit.utils.FieldPVCoordinates: Gets the velocity.
getVelocity() - Method in class org.orekit.utils.PVCoordinates: Gets the velocity.
getVenus() - Method in interface org.orekit.bodies.CelestialBodies: Get the Venus singleton body.
getVenus() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Venus singleton body.
getVenus() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
getVersion() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the format version.
getVersion() - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration: Get ITRF version.
getVertices() - Method in class org.orekit.models.earth.tessellation.Tile: Get the four vertices.
getVmAbsolute() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the typical (50th percentile) visual magnitude.
getVmApparent() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the typical (50th percentile) apparent visual magnitude.
getVmApparentMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the maximum apparent visual magnitude.
getVmApparentMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the minimum apparent visual magnitude.
getVmns(int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory: Get the V_n,s^m coefficient from V_n,s.
getVtecQualityIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header: Get the VTEC quality indicator.
getWarmup() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter: Get the value of warmup iterations.
getWaterVaporPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model: Returns the water vapor pressure at the station [hPa].
getWavelength() - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase: Get the wavelength.
getWavelength() - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase: Get the wavelength.
getWavelength() - Method in class org.orekit.estimation.measurements.gnss.Phase: Get the wavelength.
getWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration: Get the transmit wavelength.
getWavelength() - Method in enum org.orekit.gnss.Frequency: Get the wavelength in meters.
getWaves() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Get the loaded waves.
getWeek() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Getter for the reference week of the GNSS orbit.
getWeek() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Gets the Reference Week of the GNSS orbit.
getWeek() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Gets the Reference Week of the SBAS orbit.
getWeek() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Gets the Reference Week of the SBAS orbit.
getWeekNumber() - Method in class org.orekit.time.GNSSDate: Get the week number since the GNSS reference epoch.
getWeightedRms() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get weighted RMS residual ratio.
getWest() - Method in class org.orekit.bodies.FieldGeodeticPoint: Get the direction to the west of point, expressed in parent shape frame.
getWest() - Method in class org.orekit.bodies.GeodeticPoint: Get the direction to the west of point, expressed in parent shape frame.
getWest() - Method in class org.orekit.frames.TopocentricFrame: Get the west direction of topocentric frame, expressed in parent shape frame.
getWestAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients: Get the amplitude along west axis.
getWestPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients: Get the phase along West axis.
getWetMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the total mass at T₀.
getWgs84(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid: Get the WGS84 ellipsoid, attached to the given body frame.
getWideLaneCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory: Get the Wide-Lane combination of measurements.
getWindUp(SatelliteSystem, int, String) - Method in class org.orekit.estimation.measurements.gnss.WindUpFactory: Get a modifier for a satellite/receiver pair.
getWMM(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory: Get the WMM model for the given year.
getWMM(double) - Method in interface org.orekit.models.earth.GeoMagneticFields: Get the WMM model for the given year.
getWMM(double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
getX() - Method in class org.orekit.frames.EOPEntry: Get the X component of the pole motion.
getX() - Method in class org.orekit.geometry.fov.SmoothFieldOfView: Get the X axis defining FoV boundary.
getX() - Method in class org.orekit.gnss.clock.RinexClock.Receiver: Getter for the X coordinate in meters in considered Earth centered frame.
getX() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Getter for the satellite X position.
getX() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
getX() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the ECEF-X component of satellite coordinates in PZ-90 datum.
getX() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Get the ECEF-X component of satellite coordinates.
getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext: Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext: Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getX2ON2A2XP1() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get (χ²) / (n² * a² * (χ + 1 ) ).
getX2ON2A2XP1() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get (χ²) / (n² * a² * (χ + 1 ) ).
getX3ON2A() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get χ³ / (n² * a).
getX3ON2A() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get χ³ / (n² * a).
getXDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Getter for the satellite X velocity.
getXDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
getXDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the ECEF-X component of satellite velocity vector in PZ-90 datum.
getXDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Get the ECEF-X component of satellite velocity vector.
getXDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Getter for the satellite X acceleration.
getXDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
getXDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the GLONASS ECEF-X component of satellite acceleration vector in PZ-90 datum.
getXDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Get the ECEF-X component of satellite acceleration vector.
getXM10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Get the MG2 index scaled to F10.
getXM10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Get the MG2 81-day average centered index.
getXON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get χ / (n² * a²).
getXON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get χ / (n² * a²).
getXp() - Method in class org.orekit.frames.FieldPoleCorrection: Get the x_p parameter.
getXp() - Method in class org.orekit.frames.PoleCorrection: Get the x_p parameter.
getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get Χ².
getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get Χ².
getXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get Χ³.
getXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get Χ³.
getXYSpXY2Function() - Method in enum org.orekit.utils.IERSConventions: Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.
getXYSpXY2Function(TimeScales) - Method in enum org.orekit.utils.IERSConventions: Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.
getY() - Method in class org.orekit.frames.EOPEntry: Get the Y component of the pole motion.
getY() - Method in class org.orekit.geometry.fov.SmoothFieldOfView: Get the Y axis defining FoV boundary.
getY() - Method in class org.orekit.gnss.clock.RinexClock.Receiver: Getter for the Y coordinate in meters in considered Earth centered frame.
getY() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Getter for the satellite Y position.
getY() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
getY() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the ECEF-Y component of satellite coordinates in PZ-90 datum.
getY() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Get the ECEF-Y component of satellite coordinates.
getY10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Get the Solar X-Ray & Lya index scaled to F10.
getY10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Get the Solar X-Ray & Lya 81-day ave.
getYawAngle(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the yaw compensation angle at date.
getYawAngle(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the yaw compensation angle at date.
getYawAngle() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data: Get the yaw angle used for computation of phase wind-up correction.
getYawRate() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data: Get the yaw rate.
getYDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Getter for the satellite Y velocity.
getYDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
getYDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the ECEF-Y component of satellite velocity vector in PZ-90 datum.
getYDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Get the ECEF-Y component of satellite velocity vector.
getYDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Getter for the satellite Y acceleration.
getYDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
getYDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the GLONASS ECEF-Y component of satellite acceleration vector in PZ-90 datum.
getYDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Get the ECEF-Y component of satellite acceleration vector.
getYear() - Method in enum org.orekit.frames.ITRFVersion: Get the reference year of the frame version.
getYear() - Method in class org.orekit.time.DateComponents: Get the year number.
getYearOfCentury() - Method in class org.orekit.files.ilrs.CRDHeader: Get the year of century from CPF or TLE.
getYp() - Method in class org.orekit.frames.FieldPoleCorrection: Get the y_p parameter.
getYp() - Method in class org.orekit.frames.PoleCorrection: Get the y_p parameter.
getZ() - Method in class org.orekit.geometry.fov.SmoothFieldOfView: Get the Z axis defining FoV boundary.
getZ() - Method in class org.orekit.gnss.clock.RinexClock.Receiver: Getter for the Z coordinate in meters in considered Earth centered frame.
getZ() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Getter for the satellite Z position.
getZ() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
getZ() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the ECEF-Z component of satellite coordinates in PZ-90 datum.
getZ() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Get the ECEF-Z component of satellite coordinates.
getZDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Getter for the satellite Z velocity.
getZDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
getZDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the ECEF-Z component of satellite velocity vector in PZ-90 datum.
getZDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Get the ECEF-Z component of satellite velocity vector.
getZDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Getter for the satellite Z acceleration.
getZDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
getZDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements: Get the GLONASS ECEF-Z component of satellite acceleration vector in PZ-90 datum.
getZDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Get the ECEF-Z component of satellite acceleration vector.
getZenith() - Method in class org.orekit.bodies.FieldGeodeticPoint: Get the direction above the point, expressed in parent shape frame.
getZenith() - Method in class org.orekit.bodies.GeodeticPoint: Get the direction above the point, expressed in parent shape frame.
getZenith() - Method in class org.orekit.frames.TopocentricFrame: Get the zenith direction of topocentric frame, expressed in parent shape frame.
getZenithAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients: Get the amplitude along zenith axis.
getZenithDelay() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader: Returns the zenith delay array.
getZenithOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to change station position along Zenith axis.
getZenithPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients: Get the phase along zenith axis.
getZero(Field<T>) - Static method in class org.orekit.utils.FieldPVCoordinates: Get fixed position/velocity at origin (both p, v and a are zero vectors).
getZInverseTransformationReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Get a reference to the Z inverse transformation matrix.
getZipJarCrawler(T) - Method in class org.orekit.data.AbstractListCrawler: Get a zip/jar crawler for an input.
getZipJarCrawler(File) - Method in class org.orekit.data.FilesListCrawler: Get a zip/jar crawler for an input.
getZipJarCrawler(URL) - Method in class org.orekit.data.NetworkCrawler: Get a zip/jar crawler for an input.
getZone() - Method in class org.orekit.geometry.fov.PolygonalFieldOfView: Get the interior zone.
getZone() - Method in class org.orekit.propagation.events.FootprintOverlapDetector: Get the geographic zone triggering the events.
getZone() - Method in class org.orekit.propagation.events.GeographicZoneDetector: Get the geographic zone.
GHIJjsPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities: Compute the G_js, H_js, I_js and J_js polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
GHIJjsPolynomials(double, double, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Create a set of G_js, H_js, I_js and J_js polynomials.
GHmsjPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities: Compute the G_ms^j and the H_ms^j polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
GHmsjPolynomials(double, double, double, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Create a set of G_ms^j and H_ms^j polynomials.
GillIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for GillIntegrator.
GillIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.GillIntegratorBuilder: Build a new instance.
GlobalIonosphereMapModel - Class in org.orekit.models.earth.ionosphere: Global Ionosphere Map (GIM) model.
GlobalIonosphereMapModel(String) - Constructor for class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel: Constructor with supported names given by user.
GlobalIonosphereMapModel(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel: Constructor that uses user defined supported names and data context.
GlobalMappingFunctionModel - Class in org.orekit.models.earth.troposphere: The Global Mapping Function model for radio techniques.
GlobalMappingFunctionModel() - Constructor for class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel: Build a new instance.
GlobalMappingFunctionModel(TimeScale) - Constructor for class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel: Build a new instance.
GlobalPressureTemperature2Model - Class in org.orekit.models.earth.weather: The Global Pressure and Temperature 2 (GPT2) model.
GlobalPressureTemperature2Model(String, double, double, Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model: Constructor with supported names given by user.
GlobalPressureTemperature2Model(String, double, double, Geoid, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model: Constructor with supported names and source of GPT2 auxiliary data given by user.
GlobalPressureTemperature2Model(double, double, Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model: Constructor with default supported names.
GlobalPressureTemperatureModel - Class in org.orekit.models.earth.weather: The Global Pressure and Temperature model.
GlobalPressureTemperatureModel(double, double, Frame) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperatureModel: Build a new instance.
GlobalPressureTemperatureModel(double, double, Frame, DataContext) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperatureModel: Build a new instance.
Glonass - Class in org.orekit.gnss.attitude: Attitude providers for Glonass navigation satellites.
Glonass(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Glonass: Simple constructor.
GLONASS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Reference epoch for GLONASS four-year interval number: 1996-01-01T00:00:00 GLONASS time.
GLONASS_EPOCH - Static variable in class org.orekit.time.DateComponents: Reference epoch for GLONASS four-year interval number: 1996-01-01.
GLONASS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants: Value of the Earth's universal gravitational parameter for GLONASS user in m³/s².
GLONASS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants: Value of Pi for conversion from semicircles to radian.
GLONASSAlmanac - Class in org.orekit.propagation.analytical.gnss.data: This class holds a GLONASS almanac as read from .agl files.
GLONASSAlmanac(int, int, int, int, int, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac: Constructor.
GLONASSAlmanac(int, int, int, int, int, double, double, double, double, double, double, double, double, double, double, TimeScale) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac: Constructor.
GLONASSAnalyticalPropagator - Class in org.orekit.propagation.analytical.gnss: This class aims at propagating a GLONASS orbit from GLONASSOrbitalElements.
GLONASSAnalyticalPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss: This nested class aims at building a GLONASSAnalyticalPropagator.
GLONASSAnalyticalPropagatorBuilder(GLONASSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder: Initializes the builder.
GLONASSAnalyticalPropagatorBuilder(GLONASSOrbitalElements, DataContext) - Constructor for class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder: Initializes the builder.
GLONASSDate - Class in org.orekit.time: Container for date in GLONASS form.
GLONASSDate(int, int, double) - Constructor for class org.orekit.time.GLONASSDate: Build an instance corresponding to a GLONASS date.
GLONASSDate(int, int, double, TimeScale) - Constructor for class org.orekit.time.GLONASSDate: Build an instance corresponding to a GLONASS date.
GLONASSDate(AbsoluteDate) - Constructor for class org.orekit.time.GLONASSDate: Build an instance from an absolute date.
GLONASSDate(AbsoluteDate, TimeScale) - Constructor for class org.orekit.time.GLONASSDate: Build an instance from an absolute date.
GLONASSEphemeris - Class in org.orekit.propagation.analytical.gnss.data: Class for GLONASS ephemeris used by the GLONASSNumericalPropagator.
GLONASSEphemeris(int, int, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris: Build a new instance.
GLONASSEphemeris(int, int, double, double, double, double, double, double, double, double, double, double, AbsoluteDate) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris: Build a new instance.
GLONASSNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a Glonass navigation message.
GLONASSNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Constructor.
GLONASSNumericalPropagator - Class in org.orekit.propagation.numerical: This class propagates GLONASS orbits using numerical integration.
GLONASSNumericalPropagator(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, Frame, AttitudeProvider, double, DataContext, boolean) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagator: Private constructor.
GLONASSNumericalPropagatorBuilder - Class in org.orekit.propagation.numerical: This nested class aims at building a GLONASSNumericalPropagator.
GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, boolean) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder: Initializes the builder.
GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, boolean, DataContext) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder: Initializes the builder.
GLONASSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data: This interface provides the minimal set of orbital elements needed by the GLONASSAnalyticalPropagator and the GLONASSNumericalPropagator.
GLONASSScale - Class in org.orekit.time: GLONASS time scale.
GlonassUserRangeAccuracy - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris.utils: Enumerate for GLONASS User Range Accuracy.
GlonassUserRangeAccuracy(int) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.GlonassUserRangeAccuracy: Simple constructor.
GMSTScale - Class in org.orekit.time: Greenwich Mean Sidereal Time.
GNSS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants: Value of Pi for conversion from semicircles to radians in GNSS.
GNSS_WEEK_IN_SECONDS - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants: Duration of the GNSS week in seconds.
GNSSAttitudeProvider - Interface in org.orekit.gnss.attitude: Attitude providers for navigation satellites.
GNSSClockElements - Interface in org.orekit.propagation.analytical.gnss.data: This interface provides the minimal set of orbital elements needed by the ClockCorrectionsProvider.
GNSSConstants - Interface in org.orekit.propagation.analytical.gnss.data: Set of useful physical constants used in Global Navigation Satellite Systems (GNSS).
GnssData - Class in org.orekit.gnss.metric.ntrip: GNSS data retrieved from Ntrip caster.
GnssData(byte[], int) - Constructor for class org.orekit.gnss.metric.ntrip.GnssData: Build a GNSS data bloc.
GNSSDate - Class in org.orekit.time: Container for date in GNSS form.
GNSSDate(int, double, SatelliteSystem) - Constructor for class org.orekit.time.GNSSDate: Build an instance corresponding to a GNSS date.
GNSSDate(int, double, SatelliteSystem, TimeScales) - Constructor for class org.orekit.time.GNSSDate: Build an instance corresponding to a GNSS date.
GNSSDate(AbsoluteDate, SatelliteSystem) - Constructor for class org.orekit.time.GNSSDate: Build an instance from an absolute date.
GNSSDate(AbsoluteDate, SatelliteSystem, TimeScales) - Constructor for class org.orekit.time.GNSSDate: Build an instance from an absolute date.
GNSSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data: This interface provides the minimal set of orbital elements needed by the GNSSPropagator.
GNSSPropagator - Class in org.orekit.propagation.analytical.gnss: Common handling of AbstractAnalyticalPropagator methods for GNSS propagators.
GNSSPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss: This nested class aims at building a GNSSPropagator.
GNSSPropagatorBuilder(GNSSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder: Initializes the builder.
GNSSPropagatorBuilder(GNSSOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder: Initializes the builder.
GPS_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants: Value of the earth's rotation rate in rad/s for GPS user.
GPS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
GPS_EPOCH - Static variable in class org.orekit.time.DateComponents: Reference epoch for GPS weeks: 1980-01-06.
GPS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants: WGS 84 value of the Earth's universal gravitational parameter for GPS user in m³/s².
GPS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants: Number of weeks in the GPS cycle.
GPSAlmanac - Class in org.orekit.propagation.analytical.gnss.data: This class holds a GPS almanac as read from SEM or YUMA files.
GPSAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Constructor.
GPSBlockIIA - Class in org.orekit.gnss.attitude: Attitude providers for GPS block IIA navigation satellites.
GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIA: Simple constructor.
GPSBlockIIF - Class in org.orekit.gnss.attitude: Attitude providers for GPS block IIF navigation satellites.
GPSBlockIIF(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIF: Simple constructor.
GPSBlockIIR - Class in org.orekit.gnss.attitude: Attitude providers for GPS block IIR navigation satellites.
GPSBlockIIR(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIR: Simple constructor.
GPSNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a GPS navigation message.
GPSNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage: Constructor.
GPSScale - Class in org.orekit.time: GPS time scale.
gradient(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Compute the gradient of the non-central part of the gravity field.
gradient(FieldAbsoluteDate<T>, FieldVector3D<T>, T) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Compute the gradient of the non-central part of the gravity field.
GraggBulirschStoerIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for GraggBulirschStoerIntegrator.
GraggBulirschStoerIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder: Build a new instance.
GRAM - Static variable in class org.orekit.utils.units.Unit: Gram unit.
GRAPHICCombination - Class in org.orekit.estimation.measurements.gnss: GRoup And Phase Ionospheric Calibration (GRAPHIC) combination.
GravityFieldFactory - Class in org.orekit.forces.gravity.potential: Factory used to read gravity field files in several supported formats.
GravityFields - Interface in org.orekit.forces.gravity.potential: Defines methods for obtaining gravity fields.
GRGS_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for GRGS files.
GRGSFormatReader - Class in org.orekit.forces.gravity.potential: Reader for the GRGS gravity field format.
GRGSFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader: Simple constructor.
GRGSFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader: Simple constructor.
GRIM5C1_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants: Earth angular velocity from GRIM5C1 model: 7.292115e-5 rad/s.
GRIM5C1_EARTH_C20 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized second zonal coefficient from GRIM5C1 model: -1.082626110612609e-3.
GRIM5C1_EARTH_C30 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized third zonal coefficient from GRIM5C1 model: 2.536150841690056e-6.
GRIM5C1_EARTH_C40 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized fourth zonal coefficient from GRIM5C1 model: 1.61936352497151e-6.
GRIM5C1_EARTH_C50 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized fifth zonal coefficient from GRIM5C1 model: 2.231013736607540e-7.
GRIM5C1_EARTH_C60 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized sixth zonal coefficient from GRIM5C1 model: -5.402895357302363e-7.
GRIM5C1_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Earth equatorial radius from GRIM5C1 model: 6378136.46 m.
GRIM5C1_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants: Earth flattening from GRIM5C1 model: 1.0 / 298.25765.
GRIM5C1_EARTH_MU - Static variable in interface org.orekit.utils.Constants: Earth gravitational constant from GRIM5C1 model: 3.986004415e14 m³/s².
GroundAtNightDetector - Class in org.orekit.propagation.events: Detector for ground location being at night.
GroundAtNightDetector(TopocentricFrame, PVCoordinatesProvider, double, AtmosphericRefractionModel) - Constructor for class org.orekit.propagation.events.GroundAtNightDetector: Simple constructor.
GroundFieldOfViewDetector - Class in org.orekit.propagation.events: Finder for satellite entry/exit events with respect to a sensor Field Of View attached to an arbitrary frame.
GroundFieldOfViewDetector(Frame, FieldOfView) - Constructor for class org.orekit.propagation.events.GroundFieldOfViewDetector: Build a new instance.
GroundPointing - Class in org.orekit.attitudes: Base class for ground pointing attitude providers.
GroundPointing(Frame, Frame) - Constructor for class org.orekit.attitudes.GroundPointing: Default constructor.
GroundStation - Class in org.orekit.estimation.measurements: Class modeling a ground station that can perform some measurements.
GroundStation(TopocentricFrame) - Constructor for class org.orekit.estimation.measurements.GroundStation: Build a ground station ignoring station displacements.
GroundStation(TopocentricFrame, EOPHistory, StationDisplacement...) - Constructor for class org.orekit.estimation.measurements.GroundStation: Simple constructor.
GRS80_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants: Earth angular velocity from GRS80 model: 7.292115e-5 rad/s.
GRS80_EARTH_C20 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized second zonal coefficient from GRS80 model: -1.08263e-3.
GRS80_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Earth equatorial radius from GRS80 model: 6378137.0 m.
GRS80_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants: Earth flattening from GRS80 model: 1.0 / 298.257222101.
GRS80_EARTH_MU - Static variable in interface org.orekit.utils.Constants: Earth gravitational constant from GRS80 model: 3.986005e14 m³/s².
GTODProvider - Class in org.orekit.frames: Greenwich True Of Date Frame, also known as True of Date Rotating frame (TDR) or Greenwich Rotating Coordinate frame (GCR).
GTODProvider(IERSConventions, EOPHistory, TimeScales) - Constructor for class org.orekit.frames.GTODProvider: Simple constructor.
guessCenter(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CenterName: Guess the name of the center of the reference frame.
guessFrame(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame: Guesses names from ODM Table 5-3 and Annex A.
GzipFilter - Class in org.orekit.data: Filter for gzip compressed data.
GzipFilter() - Constructor for class org.orekit.data.GzipFilter

H

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

I

i - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: final inclination.
i - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: final inclination.
IAU_2012_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants: Astronomical unit as a conventional unit of length since IAU 2012 resolution B2: 149597870700.0 m.
IAU_2015_NOMINAL_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Earth equatorial radius as defined by IAU 2015 resolution B3: 6.3781e6 (m).
IAU_2015_NOMINAL_EARTH_GM - Static variable in interface org.orekit.utils.Constants: Earth attraction coefficient as defined by IAU 2015 resolution B3: 3.986004e14 (m³/s²).
IAU_2015_NOMINAL_EARTH_POLAR_RADIUS - Static variable in interface org.orekit.utils.Constants: Earth polar radius as defined by IAU 2015 resolution B3: 6.3568e6 (m).
IAU_2015_NOMINAL_JUPITER_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Jupiter equatorial radius as defined by IAU 2015 resolution B3: 7.1492e7 (m).
IAU_2015_NOMINAL_JUPITER_GM - Static variable in interface org.orekit.utils.Constants: Jupiter attraction coefficient as defined by IAU 2015 resolution B3: 1.2668653e17 (m³/s²).
IAU_2015_NOMINAL_JUPITER_POLAR_RADIUS - Static variable in interface org.orekit.utils.Constants: Jupiter polar radius as defined by IAU 2015 resolution B3: 6.6854e7 (m).
IAU_2015_NOMINAL_SOLAR_RADIUS - Static variable in interface org.orekit.utils.Constants: Solar radius as defined by IAU 2015 resolution B3: 695700000.0 m.
IAU_2015_NOMINAL_SUN_GM - Static variable in interface org.orekit.utils.Constants: Sun attraction coefficient as defined by IAU 2015 resolution B3: 1.3271244e20 (m³/s²).
IAUPole - Interface in org.orekit.bodies: Interface for IAU pole and prime meridian orientations.
ICGEM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for ICGEM files.
ICGEMFormatReader - Class in org.orekit.forces.gravity.potential: Reader for the ICGEM gravity field format.
ICGEMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader: Simple constructor.
ICGEMFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader: Simple constructor.
IDENTITY - Static variable in class org.orekit.frames.Transform: Identity transform.
IDENTITY - Static variable in class org.orekit.utils.AngularCoordinates: Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).
IDENTITY - Static variable in class org.orekit.utils.units.UnitsConverter: Identity converter.
IDENTITY_PROVIDER - Static variable in class org.orekit.frames.TransformProviderUtils: Identity provider.
IdentityConverter - Class in org.orekit.files.ccsds.ndm.tdm: Identity converter for Range Units.
IdentityConverter() - Constructor for class org.orekit.files.ccsds.ndm.tdm.IdentityConverter
IERS2003_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants: Earth angular velocity from IERS2003 model: 7.292115e-5 rad/s.
IERS2003_EARTH_C20 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized second zonal coefficient from IERS2003 model: -1.0826359e-3.
IERS2003_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Earth equatorial radius from IERS2003 model: 6378136.6 m.
IERS2003_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants: Earth flattening from IERS2003 model: 1.0 / 298.25642.
IERS2003_EARTH_MU - Static variable in interface org.orekit.utils.Constants: Earth gravitational constant from IERS2003 model: 3.986004418e14 m³/s².
IERS2010_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants: Earth angular velocity from IERS2010 model: 7.292115e-5 rad/s.
IERS2010_EARTH_C20 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized second zonal coefficient from IERS2010 model: -1.0826359e-3.
IERS2010_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Earth equatorial radius from IERS2010 model: 6378136.6 m.
IERS2010_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants: Earth flattening from IERS2010 model: 1.0 / 298.25642.
IERS2010_EARTH_MU - Static variable in interface org.orekit.utils.Constants: Earth gravitational constant from IERS2010 model: 3.986004418e14 m³/s².
IERS96_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants: Earth angular velocity from IERS96 model: 7.292115e-5 rad/s.
IERS96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized second zonal coefficient from IERS96 model: -1.0826359e-3.
IERS96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Earth equatorial radius from IERS96 model: 6378136.49 m.
IERS96_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants: Earth flattening from IERS96 model: 1.0 / 298.25642.
IERS96_EARTH_MU - Static variable in interface org.orekit.utils.Constants: Earth gravitational constant from IERS96 model: 3.986004418e14 m³/s².
IERSConventions - Enum in org.orekit.utils: Supported IERS conventions.
IERSConventions.NutationCorrectionConverter - Interface in org.orekit.utils: Interface for functions converting nutation corrections between δΔψ/δΔε to δX/δY.
IgsSsrDataField - Enum in org.orekit.gnss.metric.parser: Enum containing all intermediate level data fields that can be parsed to build an IGS SSR message.
IgsSsrMessagesParser - Class in org.orekit.gnss.metric.parser: Parser for SSR encoded messages.
IgsSsrMessagesParser(List<Integer>) - Constructor for class org.orekit.gnss.metric.parser.IgsSsrMessagesParser: Constructor.
IgsSsrMessageType - Enum in org.orekit.gnss.metric.parser: Enum containing the supported IGS SSR messages types.
ILRSHeader - Class in org.orekit.files.ilrs: Container for common data contains in International Laser Ranging Service (ILRS) files header.
ILRSHeader() - Constructor for class org.orekit.files.ilrs.ILRSHeader
ImmutableTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils: A cache of TimeStamped data that provides concurrency through immutability.
ImmutableTimeStampedCache(int, Collection<? extends T>) - Constructor for class org.orekit.utils.ImmutableTimeStampedCache: Create a new cache with the given neighbors size and data.
ImpulseManeuver<T extends EventDetector> - Class in org.orekit.forces.maneuvers: Impulse maneuver model.
ImpulseManeuver(T, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver: Build a new instance.
ImpulseManeuver(T, AttitudeProvider, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver: Build a new instance.
INC - Static variable in enum org.orekit.orbits.OrbitType: Name for inclination.
increment(double[]) - Method in class org.orekit.utils.DoubleArrayDictionary.Entry: Increment the value.
increment(T[]) - Method in class org.orekit.utils.FieldArrayDictionary.Entry: Increment the value.
increment(double[]) - Method in class org.orekit.utils.FieldArrayDictionary.Entry: Increment the value.
inData() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Acknowledge data parsing has started.
inData() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Acknowledge data parsing has started.
InertialForces - Class in org.orekit.forces.inertia: Inertial force model.
InertialForces(Frame) - Constructor for class org.orekit.forces.inertia.InertialForces: Simple constructor.
InertialProvider - Class in org.orekit.attitudes: This class handles an attitude provider aligned with a frame or a fixed offset to it.
InertialProvider(Rotation) - Constructor for class org.orekit.attitudes.InertialProvider: Creates new instance.
InertialProvider(Frame) - Constructor for class org.orekit.attitudes.InertialProvider: Creates new instance aligned with the given frame.
InertialProvider(Rotation, Frame) - Constructor for class org.orekit.attitudes.InertialProvider: Creates new instance with a fixed attitude in the given frame.
inHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Acknowledge header parsing has started.
inHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Acknowledge header parsing has started.
init(JavacTask, String...) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder: Initialize builder at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler: Initialize scheduler at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder: Initialize builder at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.estimation.measurements.generation.Scheduler: Initialize scheduler at the start of a measurements generation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.estimation.sequential.EskfMeasurementHandler: Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter: Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter: Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.empirical.AccelerationModel: Initialize the acceleration model at the start of the propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel: Initialize the acceleration model at the start of the propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.ParametricAcceleration: Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel: Initialize the acceleration model at the start of the propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration: Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.ForceModel: Initialize the force model at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.ForceModel: Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay: Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate: Initialization method called at propagation start.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.Maneuver: Initialize the force model at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.Maneuver: Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel: Initialization method.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel: Initialization method.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers: Initialization method called at propagation start.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers: Initialization method called at propagation start.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers: Initialization method called at propagation start.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.maneuvers.trigger.FieldManeuverTriggersResetter: Initialization method called at propagation start.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers: Initialization method called at propagation start.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers: Initialization method called at propagation start.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter: Initialization method called at propagation start.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AbstractDetector: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AdapterDetector: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.BooleanDetector
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.events.EventDetector: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventShifter: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventSlopeFilter: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventState: Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector: Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector: Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldEventState: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, T) - Method in interface org.orekit.propagation.events.handlers.EventHandler: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, D) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler: Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler: Deprecated.
as of 11.1, replaced by FieldEventHandler.init(FieldSpacecraftState, FieldAbsoluteDate, FieldEventDetector)
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>, KK) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.MagneticFieldDetector: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.NegateDetector
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.PositionAngleDetector: Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations: Initialize the equations at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider: Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.integration.AdditionalEquations: Deprecated.

Initialize the equations at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.integration.AdditionalEquationsAdapter: Deprecated.

Initialize the generator at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations: Initialize the equations at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider: Initialize the generator at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations: Deprecated.

Initialize the equations at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAdditionalEquationsAdapter: Deprecated.

Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations: Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations: Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Deprecated.

Initialize the generator at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>, T) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler: Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler: Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer: Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer: Initialize step handler at the start of a propagation.
init(List<SpacecraftState>, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler: Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, double) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler: Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler: Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer: Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer: Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations: Deprecated.

Initialize the generator at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Initialize the force model at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Initialize the force model at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Initialize the force model at the start of propagation.
initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Check if the initial state is provided in osculating elements.
initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Check if the initial state is provided in osculating elements.
initializeFieldShortPeriodTerms(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester: Initialize the short periodic terms for the "field" elements.
initializePropagation() - Method in class org.orekit.propagation.AbstractPropagator: Initialize propagation.
initializePropagation() - Method in class org.orekit.propagation.FieldAbstractPropagator: Initialize propagation.
initializeResetters(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers: Initialize resetters.
initializeResetters(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers: Initialize resetters.
initializeShortPeriodicTerms(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Initialize the short periodic terms for the Kalman Filter.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Computes the highest power of the eccentricity and the highest power of a/R3 to appear in the truncated analytical power series expansion.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Performs initialization prior to propagation for the current force model.
initializeShortPeriodTerms(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Performs initialization prior to propagation for the current force model.
initMapper() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Initialize the mapper.
initMapper(Field<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Initialize the mapper.
initPVCoordinates() - Method in class org.orekit.orbits.CartesianOrbit: Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.CircularOrbit: Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.EquinoctialOrbit: Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldCartesianOrbit: Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldCircularOrbit: Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit: Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.KeplerianOrbit: Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.Orbit: Compute the position/velocity coordinates from the canonical parameters.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Acknowledge metada parsing has started.
inMetadata() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Acknowledge metada parsing has started.
InputStreamEncodedMessages - Class in org.orekit.gnss.metric.parser: Encoded message from an input stream.
InputStreamEncodedMessages(InputStream) - Constructor for class org.orekit.gnss.metric.parser.InputStreamEncodedMessages: Simple constructor.
insideLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale: Check if date is within a leap second introduction in this time scale.
insideLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale: Check if date is within a leap second introduction in this time scale.
insideLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale: Check if date is within a leap second introduction in this time scale.
insideLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale: Check if date is within a leap second introduction in this time scale.
insideLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale: Check if date is within a leap second introduction in this time scale.
insideLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale: Check if date is within a leap second introduction in this time scale.
intArrayToString(int[]) - Method in class org.orekit.files.ccsds.section.AbstractWriter: Convert an array of integer to a comma-separated list.
IntegerBootstrapping - Class in org.orekit.estimation.measurements.gnss: Bootstrapping engine for ILS problem solving.
IntegerBootstrapping(double) - Constructor for class org.orekit.estimation.measurements.gnss.IntegerBootstrapping: Constructor for the bootstrapping ambiguity estimator.
integerGaussTransformation(int, int) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Perform one integer Gauss transformation.
IntegerLeastSquareComparator - Class in org.orekit.estimation.measurements.gnss: Comparator for IntegerLeastSquareSolution instance.
IntegerLeastSquareComparator() - Constructor for class org.orekit.estimation.measurements.gnss.IntegerLeastSquareComparator: Simple constructor.
IntegerLeastSquareSolution - Class in org.orekit.estimation.measurements.gnss: Class holding a solution to an Integer Least Square problem.
IntegerLeastSquareSolution(long[], double) - Constructor for class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution: Simple constructor.
IntegerLeastSquareSolver - Interface in org.orekit.estimation.measurements.gnss: Interface for algorithms solving integer least square problems.
integrate(UnivariateVectorFunction, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussQuadrature: Integrates a given function on the given interval.
integrate(CalculusFieldUnivariateVectorFunction<T>, T, T, Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussQuadrature: Integrates a given function on the given interval.
IntegratedEphemeris - Class in org.orekit.propagation.integration: This class stores sequentially generated orbital parameters for later retrieval.
IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, PropagationType, DenseOutputModel, Map<String, double[]>, List<AdditionalStateProvider>, String[]) - Constructor for class org.orekit.propagation.integration.IntegratedEphemeris: Deprecated.
as of 11.1, replaced by IntegratedEphemeris.IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, PropagationType, DenseOutputModel, DoubleArrayDictionary, List, String[])
IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, PropagationType, DenseOutputModel, DoubleArrayDictionary, List<AdditionalStateProvider>, String[]) - Constructor for class org.orekit.propagation.integration.IntegratedEphemeris: Creates a new instance of IntegratedEphemeris.
IntegrationReference - Enum in org.orekit.files.ccsds.ndm.tdm: Relationship between time tag and integration interval.
INTERMEDIATE_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation: Suffix for ground station intermediate frame name.
interpolate(AbsoluteDate, Stream<Attitude>) - Method in class org.orekit.attitudes.Attitude: Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldAttitude<T>>) - Method in class org.orekit.attitudes.FieldAttitude: Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Collection<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform: Interpolate a transform from a sample set of existing transforms.
interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform: Interpolate a transform from a sample set of existing transforms.
interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, AngularDerivativesFilter, Stream<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform: Interpolate a transform from a sample set of existing transforms.
interpolate(AbsoluteDate, Stream<Transform>) - Method in class org.orekit.frames.Transform: Get an interpolated instance.
interpolate(AbsoluteDate, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<Transform>) - Static method in class org.orekit.frames.Transform: Interpolate a transform from a sample set of existing transforms.
interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.CartesianOrbit: Get an interpolated instance.
interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.CircularOrbit: Get an interpolated instance.
interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.EquinoctialOrbit: Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldCartesianOrbit: Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldCircularOrbit: Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get an interpolated instance.
interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.KeplerianOrbit: Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldSpacecraftState<T>>) - Method in class org.orekit.propagation.FieldSpacecraftState: Get an interpolated instance.
interpolate(AbsoluteDate, Stream<SpacecraftState>) - Method in class org.orekit.propagation.SpacecraftState: Get an interpolated instance.
interpolate(FieldAbsoluteDate<KK>, Collection<T>) - Method in interface org.orekit.time.FieldTimeInterpolable: Get an interpolated instance.
interpolate(FieldAbsoluteDate<KK>, Stream<T>) - Method in interface org.orekit.time.FieldTimeInterpolable: Get an interpolated instance.
interpolate(AbsoluteDate, Collection<T>) - Method in interface org.orekit.time.TimeInterpolable: Get an interpolated instance.
interpolate(AbsoluteDate, Stream<T>) - Method in interface org.orekit.time.TimeInterpolable: Get an interpolated instance.
interpolate(AbsoluteDate, Stream<AbsolutePVCoordinates>) - Method in class org.orekit.utils.AbsolutePVCoordinates
interpolate(Frame, AbsoluteDate, CartesianDerivativesFilter, Stream<AbsolutePVCoordinates>) - Static method in class org.orekit.utils.AbsolutePVCoordinates: Interpolate position-velocity.
interpolate(FieldAbsoluteDate<T>, Stream<FieldAbsolutePVCoordinates<T>>) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
interpolate(Frame, FieldAbsoluteDate<T>, CartesianDerivativesFilter, Stream<FieldAbsolutePVCoordinates<T>>) - Static method in class org.orekit.utils.FieldAbsolutePVCoordinates: Interpolate position-velocity.
interpolate(AbsoluteDate, AngularDerivativesFilter, Collection<TimeStampedAngularCoordinates>) - Static method in class org.orekit.utils.TimeStampedAngularCoordinates: Interpolate angular coordinates.
interpolate(AbsoluteDate, AngularDerivativesFilter, Collection<TimeStampedFieldAngularCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldAngularCoordinates: Interpolate angular coordinates.
interpolate(FieldAbsoluteDate<T>, AngularDerivativesFilter, Collection<TimeStampedFieldAngularCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldAngularCoordinates: Interpolate angular coordinates.
interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, Collection<TimeStampedFieldPVCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldPVCoordinates: Interpolate position-velocity.
interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, Stream<TimeStampedFieldPVCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldPVCoordinates: Interpolate position-velocity.
interpolate(AbsoluteDate, CartesianDerivativesFilter, Collection<? extends TimeStampedPVCoordinates>) - Static method in class org.orekit.utils.TimeStampedPVCoordinates: Interpolate position-velocity.
interpolate(AbsoluteDate, CartesianDerivativesFilter, Stream<? extends TimeStampedPVCoordinates>) - Static method in class org.orekit.utils.TimeStampedPVCoordinates: Interpolate position-velocity.
InterpolatingTransformProvider - Class in org.orekit.frames: Transform provider using thread-safe interpolation on transforms sample.
InterpolatingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double) - Constructor for class org.orekit.frames.InterpolatingTransformProvider: Simple constructor.
InterpolationGrid - Interface in org.orekit.propagation.semianalytical.dsst.utilities: Interface for interpolation grids.
InterpolationMethod - Enum in org.orekit.files.ccsds.ndm.odm.oem: OEM interpolation method.
InterpolationTableLoader - Class in org.orekit.utils: Used to read an interpolation table from a data file.
InterpolationTableLoader() - Constructor for class org.orekit.utils.InterpolationTableLoader
InterSatDirectViewDetector - Class in org.orekit.propagation.events: Detector for inter-satellites direct view (i.e.
InterSatDirectViewDetector(OneAxisEllipsoid, PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.InterSatDirectViewDetector: simple constructor.
InterSatellitesPhase - Class in org.orekit.estimation.measurements.gnss: Phase measurement between two satellites.
InterSatellitesPhase(ObservableSatellite, ObservableSatellite, AbsoluteDate, double, double, double, double) - Constructor for class org.orekit.estimation.measurements.gnss.InterSatellitesPhase: Constructor.
InterSatellitesPhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical inter-satellites phase measurement with ambiguity.
InterSatellitesPhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier: Constructor.
InterSatellitesPhaseBuilder - Class in org.orekit.estimation.measurements.generation: Builder for InterSatellitesPhase measurements.
InterSatellitesPhaseBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, double, double, double) - Constructor for class org.orekit.estimation.measurements.generation.InterSatellitesPhaseBuilder: Simple constructor.
InterSatellitesRange - Class in org.orekit.estimation.measurements: One-way or two-way range measurements between two satellites.
InterSatellitesRange(ObservableSatellite, ObservableSatellite, boolean, AbsoluteDate, double, double, double) - Constructor for class org.orekit.estimation.measurements.InterSatellitesRange: Simple constructor.
InterSatellitesRangeBuilder - Class in org.orekit.estimation.measurements.generation: Builder for InterSatellitesRange measurements.
InterSatellitesRangeBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, boolean, double, double) - Constructor for class org.orekit.estimation.measurements.generation.InterSatellitesRangeBuilder: Simple constructor.
IntervalEventTrigger<T extends AbstractDetector<T>> - Class in org.orekit.forces.maneuvers.trigger: Maneuver triggers based on a single event detector that defines firing intervals.
IntervalEventTrigger(T) - Constructor for class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger: Simple constructor.
intValue(EncodedMessage) - Method in interface org.orekit.gnss.metric.parser.DataField: Get the value of the field as an integer.
inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Inverse the decomposition.
inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod: Inverse the decomposition.
inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod: Inverse the decomposition.
IodGibbs - Class in org.orekit.estimation.iod: Gibbs initial orbit determination.
IodGibbs(double) - Constructor for class org.orekit.estimation.iod.IodGibbs: Creator.
IodGooding - Class in org.orekit.estimation.iod: Gooding angles only initial orbit determination, assuming Keplerian motion.
IodGooding(double) - Constructor for class org.orekit.estimation.iod.IodGooding: Creator.
IodLambert - Class in org.orekit.estimation.iod: Lambert initial orbit determination, assuming Keplerian motion.
IodLambert(double) - Constructor for class org.orekit.estimation.iod.IodLambert: Creator.
IodLaplace - Class in org.orekit.estimation.iod: Laplace angles-only initial orbit determination, assuming Keplerian motion.
IodLaplace(double) - Constructor for class org.orekit.estimation.iod.IodLaplace: Constructor.
IonosphereFreeCombination - Class in org.orekit.estimation.measurements.gnss: Ionosphere-free combination.
IonosphericGradientConverter - Class in org.orekit.estimation.measurements.modifiers: Converter for states and parameters arrays.
IonosphericGradientConverter(SpacecraftState, int, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.IonosphericGradientConverter: Simple constructor.
IonosphericMappingFunction - Interface in org.orekit.models.earth.ionosphere: Interface for mapping functions used in the ionospheric delay computation.
IonosphericModel - Interface in org.orekit.models.earth.ionosphere: Defines a ionospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.
IRNSS_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants: Value of the earth's rotation rate in rad/s for IRNSS user.
IRNSS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Reference epoch for IRNSS weeks: 1999-08-22T00:00:00 IRNSS time.
IRNSS_EPOCH - Static variable in class org.orekit.time.DateComponents: Reference epoch for IRNSS weeks: 1999-08-22.
IRNSS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants: WGS 84 value of the Earth's universal gravitational parameter for IRNSS user in m³/s².
IRNSS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants: Number of weeks in the IRNSS cycle.
IRNSSAlmanac - Class in org.orekit.propagation.analytical.gnss.data: Class for IRNSS almanac.
IRNSSAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.IRNSSAlmanac: Constructor.
IRNSSNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in an IRNSS navigation message.
IRNSSNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage: Constructor.
IRNSSScale - Class in org.orekit.time: IRNSS time scale (also called IRNWT for IRNSS NetWork Time).
isA2b() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints: Check if rotation direction is from frame A to frame B.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.AbstractPropagator: Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.analytical.Ephemeris: Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.FieldAbstractPropagator: Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.FieldPropagator: Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.Propagator: Check if an additional state is managed.
isAfter(TimeStamped) - Method in class org.orekit.time.AbsoluteDate: Check if the instance represents a time that is strictly after another.
isAfter(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate: Check if the instance represents a time that is strictly after another.
isAfterOrEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate: Check if the instance represents a time that is after or equal to another.
isAfterOrEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate: Check if the instance represents a time that is after or equal to another.
isBefore(TimeStamped) - Method in class org.orekit.time.AbsoluteDate: Check if the instance represents a time that is strictly before another.
isBefore(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate: Check if the instance represents a time that is strictly before another.
isBeforeOrEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate: Check if the instance represents a time that is before or equal to another.
isBeforeOrEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate: Check if the instance represents a time that is before or equal to another.
isBetween(TimeStamped, TimeStamped) - Method in class org.orekit.time.AbsoluteDate: Check if the instance represents a time that is strictly between two others representing the boundaries of a time span.
isBetween(FieldTimeStamped<T>, FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate: Check if the instance represents a time that is strictly between two others representing the boundaries of a time span.
isBetweenOrEqualTo(TimeStamped, TimeStamped) - Method in class org.orekit.time.AbsoluteDate: Check if the instance represents a time that is between two others representing the boundaries of a time span, or equal to one of them.
isBetweenOrEqualTo(FieldTimeStamped<T>, FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate: Check if the instance represents a time that is between two others representing the boundaries of a time span, or equal to one of them.
isCenterOfMassCorrectionApplied() - Method in class org.orekit.files.ilrs.CPFHeader: Get the flag telling if the center of mass correction is applied.
isCenterOfMassCorrectionApplied() - Method in class org.orekit.files.ilrs.CRDHeader: Get the center of mass correction applied indicator.
isChildOf(Frame) - Method in class org.orekit.frames.Frame: Determine if a Frame is a child of another one.
isClosedOrbit() - Method in class org.orekit.utils.AbstractMultipleShooting: Get he flag representing if the orbit is closed.
isCloseTo(TimeStamped, double) - Method in class org.orekit.time.AbsoluteDate: Check if the instance time is close to another.
isCloseTo(FieldTimeStamped<T>, double) - Method in class org.orekit.time.FieldAbsoluteDate: Check if the instance time is close to another.
isCompatibleWith(AttitudeEndoints) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints: Check if a endpoint is compatible with another one.
isCompatibleWithTIVs() - Method in class org.orekit.files.ilrs.CPFHeader: Get the flag for compatibility with TIVs.
isConsistencyMaintained() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header: Get the flag indicating if phase biases maintain consistency between non-dispersive and all original dispersive phase signals.
isCurrentStateInterpolated() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Determines if the current state is computed directly by the integrator, or if it is calculated using interpolation.
isDSStateDerivative(FieldSpacecraftState<T>) - Method in class org.orekit.forces.drag.AbstractDragForceModel: Check if a field state corresponds to derivatives with respect to state.
isEnabled() - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Check if a measurement is enabled.
isEnabled() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Check if a measurement is enabled.
isEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate: Check if the instance represents the same time as another.
isEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate: Check if the instance represents the same time as another.
isExternal2SpacecraftBody() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints: Check if attitude is from external frame to spacecraft body frame.
isFiring(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Check if maneuvering is on.
isFiring(FieldSpacecraftState<T>) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Check if maneuvering is on.
isFiring(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Check if maneuvering is on.
isFiring(AbsoluteDate, double[]) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers: Find out if the maneuver is firing or not.
isFiring(FieldAbsoluteDate<S>, S[]) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers: Find out if the maneuver is firing or not.
isFiring(AbsoluteDate, double[]) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers: Find out if the maneuver is firing or not.
isFiring(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers: Find out if the maneuver is firing or not.
isFiring(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers: Check if maneuvering is on.
isFiring(AbsoluteDate, double[]) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers: Find out if the maneuver is firing or not.
isFiring(FieldAbsoluteDate<T>, T[]) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers: Find out if the maneuver is firing or not.
isFiringOnInitialState(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers: Method to check if the thruster is firing on initialization.
isFiringOnInitialState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers: Method to check if the thruster is firing on initialization.
isFiringOnInitialState(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger: Method to check if the thruster is firing on initialization.
isFiringOnInitialState(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger: Method to check if the thruster is firing on initialization.
isFirst() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get the flag for the placement of the quaternion QC in the attitude data.
isFormatOK(String, String) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE: Check the lines format validity.
isFormatOK(String, String) - Static method in class org.orekit.propagation.analytical.tle.TLE: Check the lines format validity.
isForward() - Method in class org.orekit.propagation.events.AbstractDetector: Check if the current propagation is forward or backward.
isForward() - Method in class org.orekit.propagation.events.FieldAbstractDetector: Check if the current propagation is forward or backward.
isForward() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator: Check is integration direction is forward in date.
isForward() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Check is integration direction is forward in date.
isForwardPropagation() - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel: Return the forward propagation flag.
isGradientStateDerivative(FieldSpacecraftState<T>) - Method in class org.orekit.forces.drag.AbstractDragForceModel: Check if a field state corresponds to derivatives with respect to state.
isHealthAvailable() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the flag indicating if GLONASS almanac health is available.
isIncreasing() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent: Get the Increasing/decreasing status of the event.
isIncreasing() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent: Get the Increasing/decreasing status of the event.
isIncreasing() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event: Is the g() function increasing?
isIncreasing() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event: Is the g() function increasing?
isInitialize() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Deprecated.

Get the flag for the initialization of the state jacobian.
isInside(Vector3D) - Method in class org.orekit.bodies.Ellipsoid: Check if a point is inside the ellipsoid.
isMeanOrbit() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Deprecated.
as of 11.1, replaced by AbstractIntegratedPropagator.getPropagationType()
isMeanOrbit() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Check if only the mean elements should be used in a semianalitical propagation.
isMelbourneWubbenaConsistencyMaintained() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header: Get the flag indicating if consistency between code and phase biases is maintained for the MW combinations.
isNetworked() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Check if the stream is generated from a network of stations.
isNMEARequired() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Check if NMEA message must be sent to caster.
isOn() - Method in enum org.orekit.files.ccsds.definitions.OnOff: Check if status is "on".
isOnlyPosition() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Check if fitting uses only sample positions.
isOrbitDefined() - Method in class org.orekit.propagation.FieldSpacecraftState: Check if the state contains an orbit part.
isOrbitDefined() - Method in class org.orekit.propagation.SpacecraftState: Check if the state contains an orbit part.
IsotropicDrag - Class in org.orekit.forces.drag: This class models isotropic drag effects.
IsotropicDrag(double, double) - Constructor for class org.orekit.forces.drag.IsotropicDrag: Constructor with drag coefficient min/max set to ±∞.
IsotropicDrag(double, double, double, double) - Constructor for class org.orekit.forces.drag.IsotropicDrag: Constructor with drag coefficient min/max set by user.
IsotropicRadiationClassicalConvention - Class in org.orekit.forces.radiation: This class represents the features of a simplified spacecraft.
IsotropicRadiationClassicalConvention(double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention: Simple constructor.
IsotropicRadiationCNES95Convention - Class in org.orekit.forces.radiation: This class represents the features of a simplified spacecraft.
IsotropicRadiationCNES95Convention(double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention: Simple constructor.
IsotropicRadiationSingleCoefficient - Class in org.orekit.forces.radiation: This class represents the features of a simplified spacecraft.
IsotropicRadiationSingleCoefficient(double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient: Constructor with reflection coefficient min/max set to ±∞.
IsotropicRadiationSingleCoefficient(double, double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient: Constructor with reflection coefficient min/max set by user.
isPreviousStateInterpolated() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Determines if the previous state is computed directly by the integrator, or if it is calculated using interpolation.
isPseudoInertial() - Method in class org.orekit.frames.Frame: Check if the frame is pseudo-inertial.
isQuasiInertial() - Method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame: Check if frame should be treated as inertial.
isReceiveAmplitudeCorrectionApplied() - Method in class org.orekit.files.ilrs.CRDHeader: Get the receive amplitude correction applied indicator.
isRefractionCorrected() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement: Get the flag indicating if the refraction is corrected.
isSelected() - Method in class org.orekit.utils.ParameterDriver: Check if parameter is selected.
isSignalInteger() - Method in class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias: Get the flag indicating is signal has integer property.
isSimpleEOP() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder: Check if tidal effects are ignored when interpolating EOP.
isSimpleEOP() - Method in class org.orekit.files.ccsds.utils.ContextBinding: Get EOP interpolation method.
isSimpleEOP() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Get EOP interpolation method.
isSimpleEop() - Method in class org.orekit.frames.EOPHistory: Determine if this history uses simplified EOP corrections.
isSpacecraftBodyRate() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Check if rates are specified in spacecraft body frame.
isSpacecraftBodyRate() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler: Check if rates are specified in spacecraft body frame.
isSpacecraftTimeSimplified() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Get the spacecraft time simplified flag.
isStart() - Method in class org.orekit.utils.DateDriver: Check if driver corresponds to a start date.
isStationSystemDelayApplied() - Method in class org.orekit.files.ilrs.CRDHeader: Get the station system delay applied indicator.
isSupported(DataProvider) - Method in class org.orekit.data.DataProvidersManager: Check if some provider is supported.
isSupported(String) - Method in class org.orekit.forces.AbstractForceModel: Check if a parameter is supported.
isSupported(String) - Method in interface org.orekit.forces.ForceModel: Check if a parameter is supported.
isTime() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Check if a field is a time field.
isTransponderDelayApplied() - Method in class org.orekit.files.ilrs.CRDHeader: Get the spacecraft system delay applied (transponders) indicator.
isTroposphericRefractionApplied() - Method in class org.orekit.files.ilrs.CRDHeader: Get the tropospheric refraction correction applied indicator.
isTwoWay() - Method in class org.orekit.estimation.measurements.InterSatellitesRange: Check if the instance represents a two-way measurement.
isTwoWay() - Method in class org.orekit.estimation.measurements.Range: Check if the instance represents a two-way measurement.
isTwoWay() - Method in class org.orekit.estimation.measurements.RangeRate: Check if the instance represents a two-way measurement.
isValid(int) - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration: Check if configuration entry is valid for a date.
isVariable(DerivativeStructure, int) - Method in class org.orekit.forces.drag.AbstractDragForceModel: Check if a derivative represents a specified variable.
isVariable(Gradient, int) - Method in class org.orekit.forces.drag.AbstractDragForceModel: Check if a derivative represents a specified variable.
ITRFVersion - Enum in org.orekit.frames: Enumerate for ITRF versions.
ITRFVersion.Converter - Class in org.orekit.frames: Specialized transform provider between ITRF frames.
ITRFVersionConfiguration(String, ITRFVersion, int, int) - Constructor for class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration: Simple constructor.
ITRFVersionLoader - Class in org.orekit.frames: Loader for ITRF version configuration file.
ITRFVersionLoader(String) - Constructor for class org.orekit.frames.ITRFVersionLoader: Build a loader for ITRF version configuration file.
ITRFVersionLoader(String, DataProvidersManager) - Constructor for class org.orekit.frames.ITRFVersionLoader: Build a loader for ITRF version configuration file.
ITRFVersionLoader() - Constructor for class org.orekit.frames.ITRFVersionLoader: Build a loader for ITRF version configuration file using the default name.
ITRFVersionLoader.ITRFVersionConfiguration - Class in org.orekit.frames: ITRF version configuration entry.
ItrfVersionProvider - Interface in org.orekit.frames: Interface for retrieving the ITRF version for a given set of EOP data.

J

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

K

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

L

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

M

M2 - Static variable in class org.orekit.files.ccsds.definitions.Units: m² unit.
M2 - Static variable in class org.orekit.models.earth.displacement.Tide: M₂ tide.
M2 - Static variable in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Default value for M2 coefficient.
M2_NAME - Static variable in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Parameter name for M2 coefficient.
MagneticFieldDetector - Class in org.orekit.propagation.events: Detector for South-Atlantic anomaly frontier crossing.
MagneticFieldDetector(double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector: Build a new detector.
MagneticFieldDetector(double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector: Build a new detector.
MagneticFieldDetector(double, double, double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector: Build a detector.
MagneticFieldDetector(double, double, double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean, DataContext) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector: Build a detector.
MAN_LINE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm: Maneuver line element for XML messages.
manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector: The method is in charge of collecting the measurements, manage them, and call the detection method.
manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCycleSlipDetector: The method is in charge of collecting the measurements, manage them, and call the detection method.
manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCycleSlipDetector: The method is in charge of collecting the measurements, manage them, and call the detection method.
ManBasis - Enum in org.orekit.files.ccsds.ndm.odm.ocm: Basis of maneuver used in CCSDS Orbit Comprehensive Messages.
Maneuver - Class in org.orekit.files.ccsds.ndm.adm.apm: Maneuver in an APM file.
Maneuver() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.Maneuver: Simple constructor.
Maneuver - Class in org.orekit.files.ccsds.ndm.odm.ocm: Maneuver entry.
Maneuver() - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Build an uninitialized maneuver.
Maneuver - Class in org.orekit.files.ccsds.ndm.odm.opm: Maneuver in an OPM file.
Maneuver() - Constructor for class org.orekit.files.ccsds.ndm.odm.opm.Maneuver: Simple constructor.
Maneuver - Class in org.orekit.forces.maneuvers: A generic model for maneuvers.
Maneuver(AttitudeProvider, ManeuverTriggers, PropulsionModel) - Constructor for class org.orekit.forces.maneuvers.Maneuver: Generic maneuver constructor.
ManeuverFieldType - Enum in org.orekit.files.ccsds.ndm.odm.ocm: Maneuver field type used in CCSDS Orbit Comprehensive Messages.
ManeuverHistory - Class in org.orekit.files.ccsds.ndm.odm.ocm: Maneuver history.
ManeuverHistoryMetadata - Class in org.orekit.files.ccsds.ndm.odm.ocm: Metadata for maneuver history.
ManeuverHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm: Keys for maneuver history container entries.
ManeuverKey - Enum in org.orekit.files.ccsds.ndm.adm.apm: Keys for APM maneuver entries.
ManeuverKey - Enum in org.orekit.files.ccsds.ndm.odm.opm: Keys for OPM maneuver entries.
maneuverTriggered(SpacecraftState, boolean) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate: Observe a maneuver trigger.
maneuverTriggered(FieldSpacecraftState<T>, boolean) - Method in interface org.orekit.forces.maneuvers.trigger.FieldManeuverTriggersResetter: Observe a maneuver trigger.
maneuverTriggered(SpacecraftState, boolean) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter: Observe a maneuver trigger.
ManeuverTriggers - Interface in org.orekit.forces.maneuvers.trigger: Generic interface for the maneuver triggers used in a Maneuver.
ManeuverTriggersResetter - Interface in org.orekit.forces.maneuvers.trigger: Resetter for maneuver triggers.
map(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame: Map an Orekit frame to a CCSDS frame.
map(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CenterName: Map an Orekit frame to a CCSDS center.
map(Frame) - Static method in class org.orekit.files.ccsds.definitions.FrameFacade: Map an Orekit frame to a CCSDS frame facade.
mapArrayToOrbit(double[], double[], PositionAngle, AbsoluteDate, double, Frame) - Method in enum org.orekit.orbits.OrbitType: Convert state array to orbital parameters.
mapArrayToOrbit(T[], T[], PositionAngle, FieldAbsoluteDate<T>, T, Frame) - Method in enum org.orekit.orbits.OrbitType: Convert state array to orbital parameters.
mapArrayToState(T, T[], T[], PropagationType) - Method in class org.orekit.propagation.integration.FieldStateMapper: Map the raw double components to a spacecraft state.
mapArrayToState(FieldAbsoluteDate<T>, T[], T[], PropagationType) - Method in class org.orekit.propagation.integration.FieldStateMapper: Map the raw double components to a spacecraft state.
mapArrayToState(double, double[], double[], PropagationType) - Method in class org.orekit.propagation.integration.StateMapper: Map the raw double components to a spacecraft state.
mapArrayToState(AbsoluteDate, double[], double[], PropagationType) - Method in class org.orekit.propagation.integration.StateMapper: Map the raw double components to a spacecraft state.
mapDateToDouble(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldStateMapper: Map a date to a raw double time offset.
mapDateToDouble(AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper: Map a date to a raw double time offset.
mapDoubleToDate(T) - Method in class org.orekit.propagation.integration.FieldStateMapper: Map the raw double time offset to a date.
mapDoubleToDate(T, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldStateMapper: Map the raw double time offset to a date.
mapDoubleToDate(double) - Method in class org.orekit.propagation.integration.StateMapper: Map the raw double time offset to a date.
mapDoubleToDate(double, AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper: Map the raw double time offset to a date.
mapOrbitToArray(Orbit, PositionAngle, double[], double[]) - Method in enum org.orekit.orbits.OrbitType: Convert orbit to state array.
mapOrbitToArray(FieldOrbit<T>, PositionAngle, T[], T[]) - Method in enum org.orekit.orbits.OrbitType: Convert orbit to state array.
mappingFactor(double) - Method in interface org.orekit.models.earth.ionosphere.IonosphericMappingFunction: This method allows the computation of the ionospheric mapping factor.
mappingFactor(T) - Method in interface org.orekit.models.earth.ionosphere.IonosphericMappingFunction: This method allows the computation of the ionospheric mapping factor.
mappingFactor(double) - Method in class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction: This method allows the computation of the ionospheric mapping factor.
mappingFactor(T) - Method in class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction: This method allows the computation of the ionospheric mapping factor.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel: This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel: This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.MappingFunction: This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.MappingFunction: This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel: With the Mendes Pavlis tropospheric model, the mapping function is not split into hydrostatic and wet component.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel: With the Mendes Pavlis tropospheric model, the mapping function is not split into hydrostatic and wet component.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.NiellMappingFunctionModel: This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.NiellMappingFunctionModel: This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel: This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel: This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel: This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel: This method allows the computation of the hydrostatic and wet mapping functions.
MappingFunction - Interface in org.orekit.models.earth.troposphere: Interface for mapping functions used in the tropospheric delay computation.
mappingFunction(double, double, double, double) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils: Compute the mapping function related to the coefficient values and the elevation.
mappingFunction(T, T, T, T) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils: Compute the mapping function related to the coefficient values and the elevation.
mapStateToArray(FieldSpacecraftState<T>, T[], T[]) - Method in class org.orekit.propagation.integration.FieldStateMapper: Map a spacecraft state to raw double components.
mapStateToArray(SpacecraftState, double[], double[]) - Method in class org.orekit.propagation.integration.StateMapper: Map a spacecraft state to raw double components.
MariniMurrayModel - Class in org.orekit.models.earth.troposphere: The Marini-Murray tropospheric delay model for laser ranging.
MariniMurrayModel(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.MariniMurrayModel: Create a new Marini-Murray model for the troposphere using the given environmental conditions.
MARS - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Mars.
MarshallSolarActivityFutureEstimation - Class in org.orekit.models.earth.atmosphere.data: This class reads and provides solar activity data needed by atmospheric models: F107 solar flux, Ap and Kp indexes.
MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: Simple constructor.
MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: Constructor that allows specifying the source of the MSAFE auxiliary data files.
MarshallSolarActivityFutureEstimation.StrengthLevel - Enum in org.orekit.models.earth.atmosphere.data: Strength level of activity.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder: Sets the mass.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder: Sets the mass.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder: Sets the mass.
mass(double) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder: Sets the mass.
MASS_RATIO_SUFFIX - Static variable in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel: Suffix for parameter name for Mass Ratio enabling Jacobian processing.
MassDepletionDelay - Class in org.orekit.forces.maneuvers.jacobians: Generator for effect of delaying mass depletion when delaying a maneuver.
MassDepletionDelay(String, boolean, Maneuver) - Constructor for class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay: Simple constructor.
MatricesHarvester - Interface in org.orekit.propagation: Interface for extracting State Transition Matrices and Jacobians matrices from spacecraft state.
MAX_EPOCH - Static variable in class org.orekit.time.DateComponents: Maximum supported date.
MaxGapInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities: Interpolation grid where points obey a maximum time gap.
MaxGapInterpolationGrid(double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid: Constructor.
maxValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver: Notify that a parameter maximum value has been changed.
MEAN_ANOM - Static variable in enum org.orekit.orbits.OrbitType: Name for mean anomaly.
MEAN_LAT_ARG - Static variable in enum org.orekit.orbits.OrbitType: Name for mean argument of latitude.
MEAN_LON_ARG - Static variable in enum org.orekit.orbits.OrbitType: Name for mean argument of longitude.
meanDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic: Get mean derivative, truncated to first components.
meanSecondDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic: Get mean second derivative, truncated to first components.
meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit: Computes the eccentric latitude argument from the mean latitude argument.
meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit: Computes the eccentric longitude argument from the mean longitude argument.
meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit: Computes the eccentric latitude argument from the mean latitude argument.
meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit: Computes the eccentric longitude argument from the mean longitude argument.
meanToEllipticEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit: Computes the elliptic eccentric anomaly from the mean anomaly.
meanToEllipticEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit: Computes the elliptic eccentric anomaly from the mean anomaly.
meanToHyperbolicEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit: Computes the hyperbolic eccentric anomaly from the mean anomaly.
meanToHyperbolicEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit: Computes the hyperbolic eccentric anomaly from the mean anomaly.
meanValue(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic: Get mean value, truncated to first components.
MeasurementBuilder<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.generation: Interface for generating individual measurements.
MeasurementCombination - Interface in org.orekit.estimation.measurements.gnss: Interface for combination of measurements.
MeasurementCombinationFactory - Class in org.orekit.estimation.measurements.gnss: Factory for predefined combination of measurements.
MeasurementDecorator - Class in org.orekit.estimation.sequential: Decorator adding Measurement API to an ObservedMeasurement.
MeasurementDecorator(ObservedMeasurement<?>, RealMatrix, AbsoluteDate) - Constructor for class org.orekit.estimation.sequential.MeasurementDecorator: Simple constructor.
MeasurementFilter<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.filtering: Interface for measurement pre-processing filter.
measurementIsFeasible(double) - Method in enum org.orekit.estimation.measurements.generation.SignSemantic: Check if measurement is feasible.
MeasurementType - Enum in org.orekit.gnss: Enumerate for measurement type.
MEDIAN_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector: Default suffix for median driver.
MEDIAN_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector: Default suffix for median driver.
MedianDate - Class in org.orekit.forces.maneuvers.jacobians: Generator for one column of a Jacobian matrix for special case of maneuver median date.
MedianDate(String, String, String) - Constructor for class org.orekit.forces.maneuvers.jacobians.MedianDate: Simple constructor.
MelbourneWubbenaCombination - Class in org.orekit.estimation.measurements.gnss: Melbourne-Wübbena combination.
MendesPavlisModel - Class in org.orekit.models.earth.troposphere: The Mendes - Pavlis tropospheric delay model for optical techniques.
MendesPavlisModel(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.MendesPavlisModel: Create a new Mendes-Pavlis model for the troposphere.
MERCURY - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Mercury.
messageAvailable(String, ParsedMessage) - Method in interface org.orekit.gnss.metric.ntrip.MessageObserver: Notify that an encoded message is available.
messageNumberToSatelliteSystem(int) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType: Find the satellite system corresponding to the sub-type message number.
MessageObserver - Interface in org.orekit.gnss.metric.ntrip: Interface for objects that needs to be notified when new encoded messages are available.
MessageParser<T> - Interface in org.orekit.files.ccsds.utils.lexical: Parser for CCSDS messages.
MessagesParser - Class in org.orekit.gnss.metric.parser: Parser for IGS encoded messages.
MessagesParser(List<Integer>) - Constructor for class org.orekit.gnss.metric.parser.MessagesParser: Constructor.
MessageType - Interface in org.orekit.gnss.metric.parser: Interface for encoded message types.
MessageVersionXmlTokenBuilder - Class in org.orekit.files.ccsds.utils.lexical: Builder for the root element with CCSDS message version.
MessageVersionXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.utils.lexical.MessageVersionXmlTokenBuilder
MessageWriter<H extends Header,S extends Segment<?,?>,F extends NdmConstituent<H,S>> - Interface in org.orekit.files.ccsds.utils.generation: Interface for writing Navigation Data Message (NDM) files.
Metadata - Class in org.orekit.files.ccsds.section: This class gathers the meta-data present in the Navigation Data Message (ADM, ODM and TDM).
Metadata(TimeSystem) - Constructor for class org.orekit.files.ccsds.section.Metadata: Simple constructor.
MetadataKey - Enum in org.orekit.files.ccsds.section: Keys for NDM Metadata entries.
Meteo(SortedSet<CRD.MeteorologicalMeasurement>) - Constructor for class org.orekit.files.ilrs.CRD.Meteo: Constructor.
MeteorologicalConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
MeteorologicalMeasurement(AbsoluteDate, double, double, double) - Constructor for class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement: Constructor.
metersToRu(TdmMetadata, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.tdm.IdentityConverter: Convert a range expressed in meters.
metersToRu(TdmMetadata, AbsoluteDate, double) - Method in interface org.orekit.files.ccsds.ndm.tdm.RangeUnitsConverter: Convert a range expressed in meters.
METRE - Static variable in class org.orekit.utils.units.Unit: Metre unit.
MF - Static variable in class org.orekit.models.earth.displacement.Tide: Mf tide.
MHZ_TO_HZ - Static variable in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination: Mega Hertz to Hertz converter.
MidpointIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for MidpointIntegrator.
MidpointIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.MidpointIntegratorBuilder: Build a new instance.
MILLI_ARC_SECONDS_TO_RADIANS - Static variable in class org.orekit.utils.units.UnitsConverter: Milli arcseconds to radians converter.
MILLI_SECONDS_TO_SECONDS - Static variable in class org.orekit.utils.units.UnitsConverter: Milli seconds to seconds converter.
MIN_EPOCH - Static variable in class org.orekit.time.DateComponents: Maximum supported date.
MINUTE - Static variable in class org.orekit.utils.units.Unit: Minute unit.
minuteDuration(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale: Check length of the current minute in this time scale.
minuteDuration(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale: Check length of the current minute in this time scale.
minuteDuration(AbsoluteDate) - Method in interface org.orekit.time.TimeScale: Check length of the current minute in this time scale.
minuteDuration(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale: Check length of the current minute in this time scale.
minuteDuration(AbsoluteDate) - Method in class org.orekit.time.UTCScale: Check length of the current minute in this time scale.
minuteDuration(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale: Check length of the current minute in this time scale.
MINUTES_PER_DAY - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: Time units per julian day.
minValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver: Notify that a parameter minimum value has been changed.
missingCoefficientsAllowed() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Check if missing coefficients are allowed in the input data.
MM - Static variable in class org.orekit.gnss.metric.parser.Units: Millimetres units.
MM - Static variable in class org.orekit.models.earth.displacement.Tide: Mm tide.
MM_PER_S - Static variable in class org.orekit.gnss.metric.parser.Units: Millimetres per second units.
MM_PER_S2 - Static variable in class org.orekit.gnss.metric.parser.Units: Millimetres per square second units.
modelCalled(Orbit[], Map<ObservedMeasurement<?>, EstimatedMeasurement<?>>) - Method in interface org.orekit.estimation.leastsquares.ModelObserver: Notification callback for orbit changes.
ModelObserver - Interface in org.orekit.estimation.leastsquares: Observer for model calls.
MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents: Reference epoch for modified julian dates: 1858-11-17.
ModifiedFrame - Class in org.orekit.files.ccsds.definitions: A reference frame created from the REF_FRAME and CENTER_NAME is a CCSDS OPM, OMM, or OEM file.
ModifiedFrame(Frame, CelestialBodyFrame, CelestialBody, String) - Constructor for class org.orekit.files.ccsds.definitions.ModifiedFrame: Create a CCSDS reference frame by changing the origin of an existing frame.
ModifiedLambdaMethod - Class in org.orekit.estimation.measurements.gnss: Decorrelation/reduction engine for Modified LAMBDA method.
ModifiedLambdaMethod() - Constructor for class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
modify(EstimatedMeasurement<T>) - Method in interface org.orekit.estimation.measurements.EstimationModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.gnss.WindUp: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier
modify(EstimatedMeasurement<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier
modify(EstimatedMeasurement<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.Bias: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesPhaseModifier
modify(EstimatedMeasurement<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSPhaseModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSRangeModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaPhaseModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaRangeModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier
modify(EstimatedMeasurement<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesPhaseModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesRangeModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSPhaseModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockPhaseModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeRateModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSPhase>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<OneWayGNSSRange>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier: Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier
modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier: Apply a modifier to an estimated measurement.
MOLECULAR_NITROGEN - Static variable in class org.orekit.models.earth.atmosphere.DTM2000: Identifier for molecular nitrogen.
MOLECULAR_OXYGEN - Static variable in class org.orekit.models.earth.atmosphere.DTM2000: Identifier for molecular oxygen.
monitorDetector(T) - Method in class org.orekit.propagation.events.EventsLogger: Monitor an event detector.
monitorDetector(D) - Method in class org.orekit.propagation.events.FieldEventsLogger: Monitor an event detector.
Month - Enum in org.orekit.time: Enumerate representing a calendar month.
MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Moon.
MOON_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Moon equatorial radius: 1737400 m.
mu(double) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder: Sets the Earth gravity coefficient.
MU - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: Earth gravity coefficient in m³/s².
MultipleShooter - Class in org.orekit.utils: Multiple shooting method applicable for trajectories, in an ephemeris model.
MultipleShooter(List<SpacecraftState>, List<NumericalPropagator>, List<AdditionalEquations>, double, double) - Constructor for class org.orekit.utils.MultipleShooter: Deprecated.
as of 11.1, replaced by MultipleShooter.MultipleShooter(List, List, List, double, double, int)
MultipleShooter(List<SpacecraftState>, List<NumericalPropagator>, List<EpochDerivativesEquations>, double, double, int) - Constructor for class org.orekit.utils.MultipleShooter: Simple Constructor.
MultipleShooting - Interface in org.orekit.utils: Interface for Multiple shooting methods.
MultiplexedMeasurement - Class in org.orekit.estimation.measurements: Class multiplexing several measurements as one.
MultiplexedMeasurement(List<ObservedMeasurement<?>>) - Constructor for class org.orekit.estimation.measurements.MultiplexedMeasurement: Simple constructor.
multiply(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix: Multiply the argument matrix with the current matrix.
multiply(String, Unit) - Method in class org.orekit.utils.units.Unit: Create product of units.
MultiSatStepHandler - Interface in org.orekit.propagation.sampling: This interface is a space-dynamics aware step handler for multi-sat propagation.

N

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

O

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

P

P1 - Static variable in class org.orekit.models.earth.displacement.Tide: P₁ tide.
PA - Static variable in enum org.orekit.orbits.OrbitType: Name for perigee argument.
ParameterDrivenDateIntervalDetector - Class in org.orekit.propagation.events: Detector for date intervals that may be offset thanks to parameter drivers.
ParameterDrivenDateIntervalDetector(String, AbsoluteDate, double) - Constructor for class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector: Build a new instance.
ParameterDrivenDateIntervalDetector(String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector: Build a new instance.
ParameterDriver - Class in org.orekit.utils: Class allowing to drive the value of a parameter.
ParameterDriver(String, double, double, double, double) - Constructor for class org.orekit.utils.ParameterDriver: Simple constructor.
ParameterDriversList - Class in org.orekit.utils: Class managing several parameter drivers, taking care of duplicated names.
ParameterDriversList() - Constructor for class org.orekit.utils.ParameterDriversList: Creates an empty list.
ParameterDriversList.DelegatingDriver - Class in org.orekit.utils: Specialized driver delegating to several other managing the same parameter name.
ParameterFunction - Interface in org.orekit.utils: Interface representing a scalar function depending on a ParameterDriver.
ParameterObserver - Interface in org.orekit.utils: Interface for observing parameters changes.
ParametricAcceleration - Class in org.orekit.forces.empirical: This class implements a parametric acceleration.
ParametricAcceleration(Vector3D, boolean, AccelerationModel) - Constructor for class org.orekit.forces.empirical.ParametricAcceleration: Simple constructor.
ParametricAcceleration(Vector3D, AttitudeProvider, AccelerationModel) - Constructor for class org.orekit.forces.empirical.ParametricAcceleration: Simple constructor.
parse(InputStream, String) - Method in class org.orekit.data.PoissonSeriesParser: Parse a stream.
parse(String) - Method in class org.orekit.data.PolynomialParser: Parse a polynomial expression.
parse(InputStream, String) - Method in class org.orekit.data.SimpleTimeStampedTableParser: Parse a stream.
parse(String) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame: Parse a CCSDS frame.
parse(String, IERSConventions, boolean, DataContext, boolean, boolean, boolean) - Static method in class org.orekit.files.ccsds.definitions.FrameFacade: Simple constructor.
parse(String) - Static method in class org.orekit.files.ccsds.definitions.OdMethodFacade: Parse a string from OCM.
parse(String) - Static method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame: Build an instance from a normalized descriptor.
parse(String) - Method in class org.orekit.files.ccsds.definitions.TimeConverter: Parse a relative or absolute date.
parse(String) - Static method in enum org.orekit.files.ccsds.definitions.TimeSystem: Parse a value from a key=value entry.
parse(DataSource) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Parse an attitude ephemeris file from a data source.
parse(boolean, boolean, RotationOrder, boolean, ContextBinding, String[]) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType: Get the angular coordinates corresponding to the attitude data.
parse(DataSource) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Parse an ephemeris file from a data source.
parse(DataSource) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Parse an ephemeris file from a data source.
parse(DataSource) - Method in interface org.orekit.files.general.AttitudeEphemerisFileParser: Parse an attitude ephemeris file from a data source.
parse(DataSource) - Method in interface org.orekit.files.general.EphemerisFileParser: Parse an ephemeris file from a data source.
parse(DataSource) - Method in class org.orekit.files.ilrs.CPFParser: Parse an ephemeris file from a data source.
parse(DataSource) - Method in class org.orekit.files.ilrs.CRDParser: Parse a CRD file.
parse(DataSource) - Method in class org.orekit.files.sp3.SP3Parser
parse(InputStream, String) - Method in interface org.orekit.frames.EOPHistoryLoader.Parser: Parse EOP from the given input stream.
parse(InputStream) - Method in class org.orekit.gnss.clock.RinexClockParser: Parse an IGS clock file from an input stream using the UTF-8 charset.
parse(String) - Method in class org.orekit.gnss.clock.RinexClockParser: Parse an IGS clock file from a file on the local file system.
parse(BufferedReader, String) - Method in class org.orekit.gnss.clock.RinexClockParser: Parse an IGS clock file from a stream.
parse(EncodedMessage, boolean) - Method in class org.orekit.gnss.metric.parser.MessagesParser: Parse one message.
parse(EncodedMessage, int) - Method in interface org.orekit.gnss.metric.parser.MessageType: Parse an encoded message.
parse(DataSource) - Method in class org.orekit.gnss.navigation.RinexNavigationParser: Parse RINEX navigation messages.
parse(InputStream, String) - Method in class org.orekit.time.AGILeapSecondFilesLoader.Parser: Load UTC-TAI offsets entries read from some file.
parse(InputStream, String) - Method in class org.orekit.time.TAIUTCDatFilesLoader.Parser: Load UTC-TAI offsets entries read from some file.
parse(InputStream, String) - Method in class org.orekit.time.UTCTAIHistoryFilesLoader.Parser: Load UTC-TAI offsets entries read from some file.
parse(InputStream, String) - Method in interface org.orekit.time.UTCTAIOffsetsLoader.Parser: Parse leap seconds from the input stream.
parse(String) - Static method in class org.orekit.utils.units.Unit: Parse a unit.
parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Static method in class org.orekit.time.AbsoluteDate: Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSCalendarSegmentedTimeCode(byte, byte[], TimeScale) - Static method in class org.orekit.time.AbsoluteDate: Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Method in class org.orekit.time.FieldAbsoluteDate: Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSCalendarSegmentedTimeCode(byte, byte[], TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate: Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSDaySegmentedTimeCode(byte, byte[], DateComponents) - Static method in class org.orekit.time.AbsoluteDate: Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSDaySegmentedTimeCode(byte, byte[], DateComponents, TimeScale) - Static method in class org.orekit.time.AbsoluteDate: Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSDaySegmentedTimeCode(Field<T>, byte, byte[], DateComponents) - Static method in class org.orekit.time.FieldAbsoluteDate: Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSDaySegmentedTimeCode(Field<T>, byte, byte[], DateComponents, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate: Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSUnsegmentedTimeCode(byte, byte, byte[], AbsoluteDate) - Static method in class org.orekit.time.AbsoluteDate: Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseCCSDSUnsegmentedTimeCode(byte, byte, byte[], AbsoluteDate, AbsoluteDate) - Static method in class org.orekit.time.AbsoluteDate: Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseCCSDSUnsegmentedTimeCode(Field<T>, byte, byte, byte[], FieldAbsoluteDate<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseCCSDSUnsegmentedTimeCode(Field<T>, byte, byte, byte[], FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseClockDataType(String) - Static method in enum org.orekit.gnss.clock.RinexClock.ClockDataType: Parse a string to get the time system.
parseCoefficient(String, List<List<Double>>, int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Deprecated.
as of 11.1, replaced by PotentialCoefficientsReader.parseCoefficient(String, Flattener, double[], int, int, String, String)
parseCoefficient(String, double[][], int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Deprecated.
as of 11.1, replaced by PotentialCoefficientsReader.parseCoefficient(String, Flattener, double[], int, int, String, String)
parseCoefficient(String, Flattener, double[], int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Parse a coefficient.
parseDate(String) - Static method in class org.orekit.time.DateComponents: Parse a string in ISO-8601 format to build a date.
parseDateTime(String) - Static method in class org.orekit.time.DateTimeComponents: Parse a string in ISO-8601 format to build a date/time.
ParsedMessage - Class in org.orekit.gnss.metric.messages: Abstract base class for decoded IGS messages.
ParsedMessage(int) - Constructor for class org.orekit.gnss.metric.messages.ParsedMessage: Simple constructor.
parseDouble(String) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Parse a double from a string.
ParsedUnitsBehavior - Enum in org.orekit.files.ccsds.ndm: Behavior adopted for units that have been parsed from a CCSDS message.
parseMessage(DataSource) - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser: Parse a data source.
parseMessage(DataSource) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser: Parse a data source.
parseMessageNumber(EncodedMessage) - Method in class org.orekit.gnss.metric.parser.IgsSsrMessagesParser: Parse the message number.
parseMessageNumber(EncodedMessage) - Method in class org.orekit.gnss.metric.parser.MessagesParser: Parse the message number.
parseMessageNumber(EncodedMessage) - Method in class org.orekit.gnss.metric.parser.RtcmMessagesParser: Parse the message number.
parseMonth(String) - Static method in enum org.orekit.time.Month: Parse the string to get the month.
Parser() - Constructor for class org.orekit.gnss.RinexObservationLoader.Parser
Parser() - Constructor for class org.orekit.time.AGILeapSecondFilesLoader.Parser: Simple constructor.
Parser() - Constructor for class org.orekit.time.TAIUTCDatFilesLoader.Parser: Simple constructor.
Parser() - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader.Parser: Simple constructor.
Parser - Class in org.orekit.utils.units: Parser for units.
ParserBuilder - Class in org.orekit.files.ccsds.ndm: Builder for all CCSDS Message files parsers.
ParserBuilder() - Constructor for class org.orekit.files.ccsds.ndm.ParserBuilder: Simple constructor.
ParserBuilder(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.ParserBuilder: Simple constructor.
parseSatelliteSystem(String) - Static method in enum org.orekit.gnss.SatelliteSystem: Parse a string to get the satellite system.
parseSatelliteType(String) - Static method in enum org.orekit.gnss.antenna.SatelliteType: Parse a string to get the satellite type.
parseTime(String) - Static method in class org.orekit.time.TimeComponents: Parse a string in ISO-8601 format to build a time.
parseTimeSystem(String) - Static method in enum org.orekit.gnss.TimeSystem: Parse a string to get the time system.
ParseToken - Class in org.orekit.files.ccsds.utils.lexical: Token occurring during CCSDS file parsing.
ParseToken(TokenType, String, String, Unit, int, String) - Constructor for class org.orekit.files.ccsds.utils.lexical.ParseToken: Simple constructor.
ParseToken.BooleanConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume boolean values.
ParseToken.CenterConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume center values.
ParseToken.CenterListConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume center lists.
ParseToken.CharConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume character values.
ParseToken.DateConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume date values.
ParseToken.DoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume double values.
ParseToken.DoublyIndexedDoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume doubly-indexed double values.
ParseToken.EnumConsumer<T extends Enum<T>> - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume enum values.
ParseToken.EnumListConsumer<T extends Enum<T>> - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume lists of enum values.
ParseToken.FrameConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume frame values.
ParseToken.IndexedDoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume indexed double values.
ParseToken.IndexedStringConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume indexed string values.
ParseToken.IntConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume integer values.
ParseToken.IntegerArrayConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume integer array.
ParseToken.LabeledDoubleConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume labeled double values.
ParseToken.StringConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume string values.
ParseToken.StringListConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume lists of strings values.
ParseToken.TimeSystemConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume time systems values.
ParseToken.UnitListConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume units lists values.
ParseToken.VectorConsumer - Interface in org.orekit.files.ccsds.utils.lexical: Interface representing instance methods that consume vector values.
parseType(String) - Static method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType: Parse an attitude type.
parseType(String) - Static method in enum org.orekit.files.sp3.SP3.SP3OrbitType: Parse a string to get the type.
PartialDerivativesEquations - Class in org.orekit.propagation.numerical: Deprecated.
as of 11.1, replaced by Propagator.setupMatricesComputation(String, org.hipparchus.linear.RealMatrix, org.orekit.utils.DoubleArrayDictionary)
PartialDerivativesEquations(String, NumericalPropagator) - Constructor for class org.orekit.propagation.numerical.PartialDerivativesEquations: Deprecated.

Simple constructor.
PASCAL - Static variable in class org.orekit.utils.units.Unit: Pascal unit.
PAST_INFINITY - Static variable in class org.orekit.time.AbsoluteDate: Dummy date at infinity in the past direction.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel: Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, double, double[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel: Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel: Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, double, T[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel: Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(AbsoluteDate, GeodeticPoint, double, double) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel: Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
pathDelay(FieldAbsoluteDate<T>, GeodeticPoint, T, double) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel: Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel: Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel: Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(AbsoluteDate, GeodeticPoint, double, double, double, double[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel: Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel: Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldAbsoluteDate<T>, FieldGeodeticPoint<T>, T, T, double, T[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel: Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel: Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel: Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel: Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel: Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
PERCENT - Static variable in class org.orekit.utils.units.Unit: Percentage unit.
PERCENTS_TO_UNIT - Static variable in class org.orekit.utils.units.UnitsConverter: Percents to units converter.
perige - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: perigee, expressed in KM and ALTITUDE.
perige - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: perigee, expressed in KM and ALTITUDE.
permutation(int, double) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Perform one symmetric permutation involving rows/columns k0 and k0+1.
Perturbations - Class in org.orekit.files.ccsds.ndm.odm.ocm: Perturbation parameters.
Perturbations(CelestialBodies) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Simple constructor.
PerturbationsKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm: Keys for perturbations data entries.
Phase - Class in org.orekit.estimation.measurements.gnss: Class modeling a phase measurement from a ground station.
Phase(GroundStation, AbsoluteDate, double, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.Phase: Simple constructor.
PhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical phase measurement with ambiguity.
PhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier: Constructor.
PhaseBias - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for phase bias data.
PhaseBias(int, boolean, int, int, double) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias: Constructor.
PhaseBuilder - Class in org.orekit.estimation.measurements.gnss: Builder for Phase measurements.
PhaseBuilder(CorrelatedRandomVectorGenerator, GroundStation, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.PhaseBuilder: Simple constructor.
PhaseCenterVariationFunction - Interface in org.orekit.gnss.antenna: Model for antennas phase center variations.
PhaseIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical phase measurement with ionospheric delay.
PhaseIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier: Constructor.
PhaseMinusCodeCombination - Class in org.orekit.estimation.measurements.gnss: Phase minus Code combination.
PhaseMinusCodeCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss: Phase minus code cycle slip detectors.
PhaseMinusCodeCycleSlipDetector(double, double, int, int) - Constructor for class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCycleSlipDetector: Polynomial single frequency cycle-slip detector Constructor.
PhaseTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical phase measurement with tropospheric delay.
PhaseTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier: Constructor.
PhysicalProperties - Class in org.orekit.files.ccsds.ndm.odm.ocm: Spacecraft physical properties.
PhysicalPropertiesKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm: Keys for physical properties data entries.
PLUTO - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Pluto.
pointAt(double) - Method in class org.orekit.bodies.Ellipse: Get a point of the 2D ellipse.
pointAtDistance(double, double, double) - Method in class org.orekit.frames.TopocentricFrame: Compute the point observed from the station at some specified distance.
pointOnLimb(Vector3D, Vector3D) - Method in class org.orekit.bodies.Ellipsoid: Find a point on ellipsoid limb, as seen by an external observer.
PoissonSeries - Class in org.orekit.data: Class representing a Poisson series for nutation or ephemeris computations.
PoissonSeries(PolynomialNutation, Map<Long, SeriesTerm>) - Constructor for class org.orekit.data.PoissonSeries: Build a Poisson series from an IERS table file.
PoissonSeries.CompiledSeries - Interface in org.orekit.data: This interface represents a fast evaluator for Poisson series.
PoissonSeriesParser - Class in org.orekit.data: Parser for Poisson series files.
PoissonSeriesParser(int) - Constructor for class org.orekit.data.PoissonSeriesParser: Build a parser for a Poisson series from an IERS table file.
PoleCorrection - Class in org.orekit.frames: Simple container class for pole correction parameters.
PoleCorrection(double, double) - Constructor for class org.orekit.frames.PoleCorrection: Simple constructor.
PolygonalFieldOfView - Class in org.orekit.geometry.fov: Class representing a spacecraft sensor Field Of View with polygonal shape.
PolygonalFieldOfView(SphericalPolygonsSet, double) - Constructor for class org.orekit.geometry.fov.PolygonalFieldOfView: Build a new instance.
PolygonalFieldOfView(Vector3D, PolygonalFieldOfView.DefiningConeType, Vector3D, double, int, double) - Constructor for class org.orekit.geometry.fov.PolygonalFieldOfView: Build Field Of View with a regular polygon shape.
PolygonalFieldOfView.DefiningConeType - Enum in org.orekit.geometry.fov: Enumerate for cone/polygon relative position.
PolynomialAccelerationModel - Class in org.orekit.forces.empirical: Polynomial acceleration model.
PolynomialAccelerationModel(String, AbsoluteDate, int) - Constructor for class org.orekit.forces.empirical.PolynomialAccelerationModel: Simple constructor.
PolynomialFunctionMatrix - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen: A quadratic matrix of PolynomialFunction.
PolynomialNutation - Class in org.orekit.data: Polynomial nutation function.
PolynomialNutation(double...) - Constructor for class org.orekit.data.PolynomialNutation: Build a polynomial from its coefficients.
PolynomialParser - Class in org.orekit.data: Parser for polynomials in IERS tables.
PolynomialParser(char, PolynomialParser.Unit) - Constructor for class org.orekit.data.PolynomialParser: Simple constructor.
PolynomialParser.Unit - Enum in org.orekit.data: Unit for the coefficients.
POS_X - Static variable in enum org.orekit.orbits.OrbitType: Name for position along X.
POS_Y - Static variable in enum org.orekit.orbits.OrbitType: Name for position along Y.
POS_Z - Static variable in enum org.orekit.orbits.OrbitType: Name for position along Z.
Position - Class in org.orekit.estimation.measurements: Class modeling a position only measurement.
Position(AbsoluteDate, Vector3D, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position: Constructor with one double for the standard deviation.
Position(AbsoluteDate, Vector3D, double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position: Constructor with one vector for the standard deviation.
Position(AbsoluteDate, Vector3D, double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position: Constructor with full covariance matrix and all inputs.
PositionAngle - Enum in org.orekit.orbits: Enumerate for true, eccentric and mean position angles.
PositionAngleDetector - Class in org.orekit.propagation.events: Detector for in-orbit position angle.
PositionAngleDetector(OrbitType, PositionAngle, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector: Build a new detector.
PositionAngleDetector(double, double, OrbitType, PositionAngle, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector: Build a detector.
PositionBuilder - Class in org.orekit.estimation.measurements.generation: Builder for Position measurements.
PositionBuilder(CorrelatedRandomVectorGenerator, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.PositionBuilder: Simple constructor.
PotentialCoefficientsReader - Class in org.orekit.forces.gravity.potential: This abstract class represents a Gravitational Potential Coefficients file reader.
PotentialCoefficientsReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Simple constructor.
PotentialCoefficientsReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Simple constructor.
power(String, Fraction) - Method in class org.orekit.utils.units.Unit: Create power of unit.
PowerTerm - Class in org.orekit.utils.units: A container for a term with associated power.
Predefined - Enum in org.orekit.frames: Predefined frames provided by Frames.
PREFIX - Static variable in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay: Prefix for state name.
prepareData() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Prepare data for parsing.
prepareData() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Prepare data for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Prepare header for parsing.
prepareHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Prepare header for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Prepare metadata for parsing.
prepareMetadata() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Prepare metadata for parsing.
previous() - Method in class org.orekit.utils.TimeSpanMap.Span: Get the previous time span.
previous() - Method in class org.orekit.utils.TimeSpanMap.Transition: Get the previous transition.
process(ParseToken, ContextBinding, AdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.AdmMetadataKey: Process one token.
process(ParseToken, ContextBinding, AemMetadata) - Method in enum org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey: Process an token.
process(ParseToken, ContextBinding, AttitudeEntry) - Method in enum org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Process an token.
process(ParseToken, ContextBinding, ApmQuaternion) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey: Process one token.
process(ParseToken, ContextBinding, Euler) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.EulerKey: Process one token.
process(ParseToken, ContextBinding, Maneuver) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey: Process one token.
process(ParseToken, ContextBinding, SpacecraftParameters) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParametersKey: Process one token.
process(ParseToken, ContextBinding, SpinStabilized) - Method in enum org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey: Process one token.
process(ParseToken, ContextBinding, CartesianCovariance) - Method in enum org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Process one token.
process(ParseToken, ContextBinding, CommonMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.CommonMetadataKey: Process one token.
process(ParseToken, ContextBinding, KeplerianElements) - Method in enum org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey: Process one token.
process(ParseToken, ContextBinding, CovarianceHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadataKey: Process an token.
process(String, ContextBinding, Maneuver, int, String) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Process one field.
process(ParseToken, ContextBinding, ManeuverHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadataKey: Process an token.
process(ParseToken, OcmParser) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey: Process one token.
process(ParseToken, ContextBinding, OcmMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey: Process an token.
process(ParseToken, ContextBinding, OrbitDetermination) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey: Process an token.
process(ParseToken, ContextBinding, Perturbations) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Process an token.
process(ParseToken, ContextBinding, PhysicalProperties) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.PhysicalPropertiesKey: Process an token.
process(ParseToken, ContextBinding, TrajectoryStateHistoryMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey: Process an token.
process(ParseToken, ContextBinding, OdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.OdmMetadataKey: Process one token.
process(ParseToken, ContextBinding, OemMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.oem.OemMetadataKey: Process an token.
process(ParseToken, ContextBinding, OmmMetadata) - Method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmMetadataKey: Process one token.
process(ParseToken, ContextBinding, OmmTle) - Method in enum org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey: Process one token.
process(ParseToken, ContextBinding, Maneuver) - Method in enum org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey: Process one token.
process(ParseToken, ContextBinding, SpacecraftParameters) - Method in enum org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey: Process one token.
process(ParseToken, ContextBinding, StateVector) - Method in enum org.orekit.files.ccsds.ndm.odm.StateVectorKey: Process one token.
process(ParseToken, ContextBinding, RangeUnitsConverter, TdmMetadata, ObservationsBlock) - Method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType: Process an observation line.
process(ParseToken, ContextBinding, ObservationsBlock) - Method in enum org.orekit.files.ccsds.ndm.tdm.TdmDataKey: Process one token.
process(ParseToken, ContextBinding, TdmMetadata) - Method in enum org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Process an token.
process(ParseToken, ContextBinding, Header) - Method in enum org.orekit.files.ccsds.section.HeaderKey: Process an token.
process(ParseToken, AbstractConstituentParser<?, ?>) - Method in enum org.orekit.files.ccsds.section.KvnStructureKey: Process an token.
process(ParseToken, ContextBinding, Metadata) - Method in enum org.orekit.files.ccsds.section.MetadataKey: Process an token.
process(ParseToken, AbstractConstituentParser<?, ?>) - Method in enum org.orekit.files.ccsds.section.XmlStructureKey: Process an token.
process(ParseToken) - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser: Process a parse token.
process(ParseToken) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser: Process a parse token.
processAsBoolean(ParseToken.BooleanConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a boolean.
processAsCenter(ParseToken.CenterConsumer, CelestialBodies) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a body center.
processAsCenterList(ParseToken.CenterListConsumer, CelestialBodies) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a body center list.
processAsDate(ParseToken.DateConsumer, ContextBinding) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a date.
processAsDouble(Unit, ParsedUnitsBehavior, ParseToken.DoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a double.
processAsDoublyIndexedDouble(int, int, Unit, ParsedUnitsBehavior, ParseToken.DoublyIndexedDoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a doubly-indexed double.
processAsEnum(Class<T>, ParseToken.EnumConsumer<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as an enum.
processAsEnumsList(Class<T>, ParseToken.EnumListConsumer<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a list of enums.
processAsFrame(ParseToken.FrameConsumer, ContextBinding, boolean, boolean, boolean) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a frame.
processAsIndexedDouble(int, Unit, ParsedUnitsBehavior, ParseToken.IndexedDoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as an indexed double.
processAsIndexedNormalizedString(int, ParseToken.IndexedStringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as an indexed normalized string.
processAsIndexedUppercaseString(int, ParseToken.IndexedStringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as an indexed normalized uppercase string.
processAsInteger(ParseToken.IntConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as an integer.
processAsIntegerArray(ParseToken.IntegerArrayConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as an array of integers.
processAsLabeledDouble(char, Unit, ParsedUnitsBehavior, ParseToken.LabeledDoubleConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as an labeled double.
processAsNormalizedCharacter(ParseToken.CharConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a normalized character.
processAsNormalizedList(ParseToken.StringListConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a list of normalized strings.
processAsNormalizedString(ParseToken.StringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a normalized string.
processAsTimeSystem(ParseToken.TimeSystemConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a time system.
processAsUnitList(ParseToken.UnitListConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a list of units.
processAsUppercaseList(ParseToken.StringListConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a list of normalized uppercase strings.
processAsUppercaseString(ParseToken.StringConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a normalized uppercase string.
processAsVector(ParseToken.VectorConsumer) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Process the content as a vector.
ProcessingState - Interface in org.orekit.files.ccsds.utils.parsing: Interface for processing parsing tokens for CCSDS NDM files.
processMeasurements(Iterable<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.KalmanEstimator: Process several measurements.
processMeasurements(List<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator: Process a single measurement.
processMeasurements(List<ObservedMeasurement<?>>, ExtendedKalmanFilter<MeasurementDecorator>) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Process a single measurement.
processRotationOrder(ParseToken, AdmParser.RotationOrderConsumer) - Static method in class org.orekit.files.ccsds.ndm.adm.AdmParser: Process a CCSDS Euler angles sequence as a RotationOrder.
processToken(ParseToken) - Method in class org.orekit.files.ccsds.section.HeaderProcessingState: Process one token.
processToken(ParseToken) - Method in class org.orekit.files.ccsds.section.KvnStructureProcessingState: Process one token.
processToken(ParseToken) - Method in class org.orekit.files.ccsds.section.XmlStructureProcessingState: Process one token.
processToken(ParseToken) - Method in class org.orekit.files.ccsds.utils.parsing.ErrorState: Process one token.
processToken(ParseToken) - Method in interface org.orekit.files.ccsds.utils.parsing.ProcessingState: Process one token.
projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.CircularFieldOfView: Find the direction on Field Of View Boundary closest to a line of sight.
projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.EllipticalFieldOfView: Find the direction on Field Of View Boundary closest to a line of sight.
projectToBoundary(Vector3D) - Method in interface org.orekit.geometry.fov.FieldOfView: Find the direction on Field Of View Boundary closest to a line of sight.
projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView: Find the direction on Field Of View Boundary closest to a line of sight.
projectToEllipse(Vector2D) - Method in class org.orekit.bodies.Ellipse: Find the closest ellipse point.
projectToEllipse(TimeStampedPVCoordinates) - Method in class org.orekit.bodies.Ellipse: Project position-velocity-acceleration on an ellipse.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in interface org.orekit.bodies.BodyShape: Project a point to the ground.
projectToGround(TimeStampedPVCoordinates, Frame) - Method in interface org.orekit.bodies.BodyShape: Project a moving point to the ground.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid: Project a point to the ground.
projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid: Project a moving point to the ground.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.models.earth.Geoid
projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.models.earth.Geoid
propagate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator: Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Propagate from a start date towards a target date.
propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Propagate from a start date towards a target date.
propagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator: Propagate towards a target date.
propagate(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldPropagator: Propagate towards a target date.
propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldPropagator: Propagate from a start date towards a target date.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Propagate from a start date towards a target date.
propagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Propagate towards a target date.
propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Propagate from a start date towards a target date.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator: Propagate towards a target date.
propagate(AbsoluteDate) - Method in interface org.orekit.propagation.Propagator: Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.propagation.Propagator: Propagate from a start date towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.PropagatorsParallelizer: Propagate from a start date towards a target date.
propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator: Gets the PVCoordinates of the GLONASS SV in ECEF frame.
propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator: Gets the PVCoordinates of the GNSS SV in ECEF frame.
propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator: Gets the PVCoordinates of the GNSS SV in ECEF frame.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris: Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Extrapolate an orbit up to a specific target date.
PropagationType - Enum in org.orekit.propagation: Enumerate to define the propagation type used by the propagator.
Propagator - Interface in org.orekit.propagation: This interface provides a way to propagate an orbit at any time.
PropagatorBuilder - Interface in org.orekit.propagation.conversion: This interface is the top-level abstraction to build propagators for conversion.
PropagatorConverter - Interface in org.orekit.propagation.conversion: This interface is the top-level abstraction for propagators conversions.
PropagatorsParallelizer - Class in org.orekit.propagation: This class provides a way to propagate simultaneously several orbits.
PropagatorsParallelizer(List<Propagator>, MultiSatStepHandler) - Constructor for class org.orekit.propagation.PropagatorsParallelizer: Simple constructor.
PropulsionModel - Interface in org.orekit.forces.maneuvers.propulsion: Generic interface for a propulsion model used in a Maneuver.
put(String, double[]) - Method in class org.orekit.utils.DoubleArrayDictionary: Add an entry.
put(String, T[]) - Method in class org.orekit.utils.FieldArrayDictionary: Add an entry.
put(String, double[]) - Method in class org.orekit.utils.FieldArrayDictionary: Add an entry.
putAll(Map<String, double[]>) - Method in class org.orekit.utils.DoubleArrayDictionary: Put all the entries from the map in the dictionary.
putAll(DoubleArrayDictionary) - Method in class org.orekit.utils.DoubleArrayDictionary: Put all the entries from another dictionary.
putAll(Map<String, T[]>) - Method in class org.orekit.utils.FieldArrayDictionary: Put all the entries from the map in the dictionary.
putAll(FieldArrayDictionary<T>) - Method in class org.orekit.utils.FieldArrayDictionary: Put all the entries from another dictionary.
PV - Class in org.orekit.estimation.measurements: Class modeling a position-velocity measurement.
PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV: Constructor with two double for the standard deviations.
PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV: Constructor with two vectors for the standard deviations.
PV(AbsoluteDate, Vector3D, Vector3D, double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV: Constructor with one vector for the standard deviations.
PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV: Constructor with 2 smaller covariance matrices.
PV(AbsoluteDate, Vector3D, Vector3D, double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV: Constructor with full covariance matrix and all inputs.
PVBuilder - Class in org.orekit.estimation.measurements.generation: Builder for PV measurements.
PVBuilder(CorrelatedRandomVectorGenerator, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.PVBuilder: Simple constructor.
PVCoordinates - Class in org.orekit.utils: Simple container for Position/Velocity/Acceleration triplets.
PVCoordinates() - Constructor for class org.orekit.utils.PVCoordinates: Simple constructor.
PVCoordinates(Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates: Builds a PVCoordinates triplet with zero acceleration.
PVCoordinates(Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates: Builds a PVCoordinates triplet.
PVCoordinates(double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates: Multiplicative constructor.
PVCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates: Subtractive constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates: Linear constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates: Linear constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates: Linear constructor.
PVCoordinates(FieldVector3D) - Constructor for class org.orekit.utils.PVCoordinates: Builds a PVCoordinates triplet from a FieldVector3D<Derivative>.
PVCoordinatesProvider - Interface in org.orekit.utils: Interface for PV coordinates providers.

Q

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

R

RAAN - Static variable in enum org.orekit.orbits.OrbitType: Name for right ascension of ascending node.
RADIAN - Static variable in class org.orekit.utils.units.Unit: Radian unit.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention: Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention: Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention: Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention: Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient: Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient: Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in interface org.orekit.forces.radiation.RadiationSensitive: Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in interface org.orekit.forces.radiation.RadiationSensitive: Compute the acceleration due to radiation pressure.
RadiationSensitive - Interface in org.orekit.forces.radiation: Interface for spacecraft that are sensitive to radiation pressure forces.
radiusCorrection(double) - Method in enum org.orekit.propagation.events.VisibilityTrigger: Apply radius correction.
Range - Class in org.orekit.estimation.measurements: Class modeling a range measurement from a ground station.
Range(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Range: Simple constructor.
RangeBuilder - Class in org.orekit.estimation.measurements.generation: Builder for Range measurements.
RangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, boolean, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.RangeBuilder: Simple constructor.
RangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical range measurement with ionospheric delay.
RangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier: Constructor.
RangeMeasurement(AbsoluteDate, double, int) - Constructor for class org.orekit.files.ilrs.CRD.RangeMeasurement: Constructor.
RangeMeasurement(AbsoluteDate, double, int, double) - Constructor for class org.orekit.files.ilrs.CRD.RangeMeasurement: Constructor.
RangeMode - Enum in org.orekit.files.ccsds.ndm.tdm: Type of range tones.
RangeRate - Class in org.orekit.estimation.measurements: Class modeling one-way or two-way range rate measurement between two vehicles.
RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.RangeRate: Simple constructor.
RangeRateBuilder - Class in org.orekit.estimation.measurements.generation: Builder for RangeRate measurements.
RangeRateBuilder(CorrelatedRandomVectorGenerator, GroundStation, boolean, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.RangeRateBuilder: Simple constructor.
rangeRateErrorTroposphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier: Compute the measurement error due to Troposphere.
rangeRateErrorTroposphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier: Compute the measurement error due to Troposphere.
RangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical range-rate measurement with ionospheric delay.
RangeRateIonosphericDelayModifier(IonosphericModel, double, boolean) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier: Constructor.
RangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical range-rate measurements with tropospheric delay.
RangeRateTroposphericDelayModifier(DiscreteTroposphericModel, boolean) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier: Constructor.
RangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical range measurement with tropospheric delay.
RangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier: Constructor.
RangeUnits - Enum in org.orekit.files.ccsds.ndm.tdm: Units of the range observable.
RangeUnitsConverter - Interface in org.orekit.files.ccsds.ndm.tdm: Interface for converting Range Units to meters.
RAPID_DATA_PREDICITON_COLUMNS_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory: Default regular expression for the Rapid Data and Prediction EOP columns files (IAU2000 compatibles).
RAPID_DATA_PREDICITON_XML_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory: Default regular expression for the Rapid Data and Prediction EOP XML files (IAU2000 compatibles).
RAPID_DATA_PREDICTION_COLUMNS_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory: Default regular expression for the Rapid Data and Prediction EOP columns files (IAU1980 compatibles).
RAPID_DATA_PREDICTION_XML_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory: Default regular expression for the Rapid Data and Prediction EOP XML files (IAU1980 compatibles).
rateFrameIsA() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Check if rates are specified in frame A.
rateFrameIsA() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler: Check if rates are specified in frame A.
rawDataIsBinary() - Method in interface org.orekit.data.DataSource.Opener: Check if the raw data is binary.
RawSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential: Interface used to provide raw spherical harmonics coefficients.
RawSphericalHarmonicsProvider.RawSphericalHarmonics - Interface in org.orekit.forces.gravity.potential: The raw spherical harmonics at a particular instant.
rawToSI(RangeUnitsConverter, TdmMetadata, AbsoluteDate, double) - Method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType: Convert a measurement to SI units.
readGravityField(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Read a gravity field coefficients provider from the first supported file.
readGravityField(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields: Read a gravity field coefficients provider from the first supported file.
readLine() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader: Read a line from the input data stream.
readLineOrThrow(Localizable, Object...) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader: Read a line from the input data stream, or if the end of the stream has been reached throw an exception.
Receiver(String, String, double, double, double) - Constructor for class org.orekit.gnss.clock.RinexClock.Receiver: Constructor.
ReceiverAntenna - Class in org.orekit.gnss.antenna: GNSS receiver antenna model.
ReceiverAntenna(String, String, Map<Frequency, FrequencyPattern>, String) - Constructor for class org.orekit.gnss.antenna.ReceiverAntenna: Simple constructor.
Record - Class in org.orekit.gnss.metric.ntrip: Record in source table.
Record(String) - Constructor for class org.orekit.gnss.metric.ntrip.Record: Build a record by parsing a source table line.
RecordAndContinue<T extends EventDetector> - Class in org.orekit.propagation.events.handlers: Handler that will record every time an event occurs and always return Action.CONTINUE.
RecordAndContinue() - Constructor for class org.orekit.propagation.events.handlers.RecordAndContinue: Create a new handler using an ArrayList to store events.
RecordAndContinue(List<RecordAndContinue.Event<T>>) - Constructor for class org.orekit.propagation.events.handlers.RecordAndContinue: Create a handler using the given collection to store events.
RecordAndContinue.Event<T> - Class in org.orekit.propagation.events.handlers: A single event detected during propagation.
RecordType - Enum in org.orekit.gnss.metric.ntrip: Enumerate for record types in sourcetable.
recoverAmbiguities() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Recover ambiguities prior to the Z-transformation.
recoverAmbiguities() - Method in class org.orekit.estimation.measurements.gnss.IntegerBootstrapping: Recover ambiguities prior to the Z-transformation.
reduction() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Perform LAMBDA reduction.
reduction() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod: Perform LAMBDA reduction.
reduction() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod: Perform MLAMBDA reduction.
ReferenceClock(String, String, double, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.gnss.clock.RinexClock.ReferenceClock: Constructor.
referenceDateChanged(AbsoluteDate, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver: Notify that a parameter reference date has been changed.
ReferenceEllipsoid - Class in org.orekit.models.earth: A Reference Ellipsoid for use in geodesy.
ReferenceEllipsoid(double, double, Frame, double, double) - Constructor for class org.orekit.models.earth.ReferenceEllipsoid: Creates a new geodetic Reference Ellipsoid from four defining parameters.
referenceValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver: Notify that a parameter reference value has been changed.
REFLECTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive: Parameter name for reflection coefficient.
refuseFurtherComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer: Set flag to refuse further comments.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Register an attitude provider.
registerSwitchEvents(Propagator) - Method in class org.orekit.attitudes.AttitudesSequence: Register all wrapped switch events to the propagator.
registerSwitchEvents(Field<T>, FieldPropagator<T>) - Method in class org.orekit.attitudes.AttitudesSequence: Register all wrapped switch events to the propagator.
RegularXmlTokenBuilder - Class in org.orekit.files.ccsds.utils.lexical: Regular builder using XML elements names and content for tokens.
RegularXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.utils.lexical.RegularXmlTokenBuilder: Simple constructor.
reinitializeBegin(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState: Reinitialize the beginning of the step.
reinitializeBegin(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState: Reinitialize the beginning of the step.
RelativisticClockInterSatellitesPhaseModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical inter-satellites phase measurement with relativistic clock correction.
RelativisticClockInterSatellitesPhaseModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesPhaseModifier: Simple constructor.
RelativisticClockInterSatellitesRangeModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical inter-satellites range measurement with relativistic clock correction.
RelativisticClockInterSatellitesRangeModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesRangeModifier: Simple constructor.
RelativisticClockOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical one-way GNSS phase measurement with relativistic clock correction.
RelativisticClockOneWayGNSSPhaseModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSPhaseModifier: Simple constructor.
RelativisticClockOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical one-way GNSS range measurement with relativistic clock correction.
RelativisticClockOneWayGNSSRangeModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeModifier: Simple constructor.
RelativisticClockPhaseModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical phase measurement with relativistic clock correction.
RelativisticClockPhaseModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockPhaseModifier: Simple constructor.
RelativisticClockRangeModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical range measurement with relativistic clock correction.
RelativisticClockRangeModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeModifier: Simple constructor.
RelativisticClockRangeRateModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical range-rate measurement with relativistic frequency deviation.
RelativisticClockRangeRateModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeRateModifier: Simple constructor.
relativisticCorrection(EstimatedMeasurement<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockModifier: Computes the relativistic clock correction.
Relativity - Class in org.orekit.forces.gravity: Post-Newtonian correction force due to general relativity.
Relativity(double) - Constructor for class org.orekit.forces.gravity.Relativity: Create a force model to add post-Newtonian acceleration corrections to an Earth orbit.
remove(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer: Remove a handler.
remove(FieldOrekitFixedStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer: Remove a handler.
remove(OrekitStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer: Remove a handler.
remove(OrekitFixedStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer: Remove a handler.
remove(String) - Method in class org.orekit.utils.DoubleArrayDictionary: Remove an entry.
remove(String) - Method in class org.orekit.utils.FieldArrayDictionary: remove an entry.
removeForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Remove all perturbing force models from the global perturbation model.
removeForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator: Remove all force models (except central attraction).
removeForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Remove all perturbing force models from the global perturbation model (except central attraction).
removeForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Remove all perturbing force models from the global perturbation model (except central attraction).
removeObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver: Remove an observer.
removeProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager: Remove one provider.
removeSolution() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Remove spurious solution.
replaceObserver(ParameterObserver, ParameterObserver) - Method in class org.orekit.utils.ParameterDriver: Replace an observer.
requiresDenseOutput() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer: Determines whether this handler needs dense output.
requiresDenseOutput() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer: Determines whether this handler needs dense output.
rescale(double, boolean, double[][], double[][], boolean, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Deprecated.
as of 11.1, replaced by PotentialCoefficientsReader.rescale(double, boolean, Flattener, Flattener, double[])
rescale(double, boolean, Flattener, Flattener, double[]) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Rescale coefficients arrays.
rescale(boolean, Flattener, Flattener, TimeDependentHarmonic[]) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Rescale coefficients arrays.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.NdmParser: Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Reset parser to initial state before parsing.
reset(FileFormat) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Reset parser to initial state before parsing.
reset(FileFormat) - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser: Reset parser to initial state before parsing.
reset(FileFormat, ProcessingState) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser: Reset parser to initial state before parsing.
resetActiveProvider(AttitudeProvider) - Method in class org.orekit.attitudes.AttitudesSequence: Reset the active provider.
resetFiltersToDefault() - Method in class org.orekit.data.DataProvidersManager: Reset all filters to default.
resetFitting(AbsoluteDate, double...) - Method in class org.orekit.utils.SecularAndHarmonic: Reset fitting.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AdapterPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.Ephemeris: Try (and fail) to reset the initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.KeplerianPropagator: Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator: Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldPropagator: Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in interface org.orekit.propagation.Propagator: Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Reset the initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Reset the initial state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AdapterPropagator: Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.Ephemeris: Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator: Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator: Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator: Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator: Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.KeplerianPropagator: Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Reset an intermediate state.
resetOrbit(Orbit) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Reset the orbit in the propagator builder.
resetOrbit(Orbit, PropagationType) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder: Reset the orbit in the propagator builder.
resetOrbit(Orbit) - Method in interface org.orekit.propagation.conversion.OrbitDeterminationPropagatorBuilder: Reset the orbit in the propagator builder.
resetState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate: Reset state as a maneuver triggers.
resetState(FieldSpacecraftState<T>) - Method in interface org.orekit.forces.maneuvers.trigger.FieldManeuverTriggersResetter: Reset state as a maneuver triggers.
resetState(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggersResetter: Reset state as a maneuver triggers.
resetState(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector: Reset the state prior to continue propagation.
resetState(SpacecraftState) - Method in class org.orekit.propagation.events.AdapterDetector: Reset the state prior to continue propagation.
resetState(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector: Reset the state prior to continue propagation.
resetState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector: Reset the state prior to continue propagation.
resetState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector: Reset the state prior to continue propagation.
resetState(T, SpacecraftState) - Method in interface org.orekit.propagation.events.handlers.EventHandler: Reset the state prior to continue propagation.
resetState(D, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler: Reset the state prior to continue propagation.
resetState(KK, FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler: Reset the state prior to continue propagation.
ResidualFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.filtering: Residual pre-processing filter.
ResidualFilter(double) - Constructor for class org.orekit.estimation.measurements.filtering.ResidualFilter: Constructor.
restrictStep(FieldSpacecraftState<T>, FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator: Create a new restricted version of the instance.
restrictStep(SpacecraftState, SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Create a new restricted version of the instance.
REV_PER_DAY - Static variable in class org.orekit.files.ccsds.definitions.Units: Revolutions per day unit.
REV_PER_DAY2_SCALED - Static variable in class org.orekit.files.ccsds.definitions.Units: Scaled revolutions per square day unit.
REV_PER_DAY3_SCALED - Static variable in class org.orekit.files.ccsds.definitions.Units: Scaled revolutions per cubic day divieded by 6 unit.
revert() - Method in class org.orekit.utils.AngularCoordinates: Revert a rotation/rotation rate/ rotation acceleration triplet.
revert() - Method in class org.orekit.utils.FieldAngularCoordinates: Revert a rotation / rotation rate / rotation acceleration triplet.
revert() - Method in class org.orekit.utils.TimeStampedAngularCoordinates: Revert a rotation/rotation rate pair.
revert() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates: Revert a rotation/rotation rate pair.
REVOLUTION - Static variable in class org.orekit.utils.units.Unit: Revolution unit.
RichardsonExpansion - Class in org.orekit.orbits: Class implementing the Third-Order Richardson Expansion.
RichardsonExpansion(CR3BPSystem, LagrangianPoints) - Constructor for class org.orekit.orbits.RichardsonExpansion: Simple Constructor.
RinexClock - Class in org.orekit.gnss.clock: Represents a parsed clock file from the IGS.
RinexClock(Function<? super String, ? extends Frame>) - Constructor for class org.orekit.gnss.clock.RinexClock: Constructor.
RinexClock.ClockDataLine - Class in org.orekit.gnss.clock: Clock data for a single station.
RinexClock.ClockDataType - Enum in org.orekit.gnss.clock: Clock data type.
RinexClock.Receiver - Class in org.orekit.gnss.clock: Represents a receiver or a satellite with its position in the considered frame.
RinexClock.ReferenceClock - Class in org.orekit.gnss.clock: Represents a reference clock with its validity time span.
RinexClockParser - Class in org.orekit.gnss.clock: A parser for the clock file from the IGS.
RinexClockParser() - Constructor for class org.orekit.gnss.clock.RinexClockParser: Create an clock file parser using default values.
RinexClockParser(Function<? super String, ? extends Frame>) - Constructor for class org.orekit.gnss.clock.RinexClockParser: Create a clock file parser and specify the frame builder.
RinexClockParser(Function<? super String, ? extends Frame>, TimeScales) - Constructor for class org.orekit.gnss.clock.RinexClockParser: Constructor, build the IGS clock file parser.
RinexNavigation - Class in org.orekit.gnss.navigation: Represents a parsed RINEX navigation messages files.
RinexNavigation() - Constructor for class org.orekit.gnss.navigation.RinexNavigation: Constructor.
RinexNavigation.TimeSystemCorrection - Class in org.orekit.gnss.navigation: Container for time system corrections.
RinexNavigationParser - Class in org.orekit.gnss.navigation: Parser for RINEX navigation messages files.
RinexNavigationParser() - Constructor for class org.orekit.gnss.navigation.RinexNavigationParser: Constructor.
RinexNavigationParser(TimeScales) - Constructor for class org.orekit.gnss.navigation.RinexNavigationParser: Constructor.
RinexObservationHeader - Class in org.orekit.gnss: Container for Rinex observation file header.
RinexObservationHeader(double, SatelliteSystem, String, String, String, String, String, String, String, String, String, String, Vector3D, double, Vector2D, Vector3D, Vector3D, Vector3D, double, AbsoluteDate, AbsoluteDate, int, int) - Constructor for class org.orekit.gnss.RinexObservationHeader: Simple constructor, for Rinex 2 Header.
RinexObservationHeader(double, SatelliteSystem, String, String, String, String, String, String, String, String, String, String, Vector3D, double, Vector2D, Vector3D, String, Vector3D, Vector3D, double, Vector3D, Vector3D, String, double, AbsoluteDate, AbsoluteDate, int, List<AppliedDCBS>, List<AppliedPCVS>, List<RinexObservationLoader.Parser.PhaseShiftCorrection>, int, int, int, int) - Constructor for class org.orekit.gnss.RinexObservationHeader: Simple constructor, for Rinex 3 Header.
RinexObservationLoader - Class in org.orekit.gnss: Loader for Rinex measurements files.
RinexObservationLoader(String) - Constructor for class org.orekit.gnss.RinexObservationLoader: Simple constructor.
RinexObservationLoader(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.gnss.RinexObservationLoader: Create a RINEX loader/parser with the given source of RINEX auxiliary data files.
RinexObservationLoader(DataSource) - Constructor for class org.orekit.gnss.RinexObservationLoader: Simple constructor.
RinexObservationLoader(DataSource, TimeScales) - Constructor for class org.orekit.gnss.RinexObservationLoader: Loads RINEX from the given input stream using the specified auxiliary data.
RinexObservationLoader.Parser - Class in org.orekit.gnss: Parser for rinex files.
RinexObservationLoader.Parser.PhaseShiftCorrection - Class in org.orekit.gnss: Phase Shift corrections.
RinexObservationLoader.Parser.ScaleFactorCorrection - Class in org.orekit.gnss: Scale Factor to be applied.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.Aem: Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.Apm: Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm: Root element for XML messages.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.Oem: Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.Omm: Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Root element for XML files.
ROOT - Static variable in class org.orekit.files.ccsds.ndm.tdm.Tdm: Root element for XML files.
ROOT22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
ROOT32 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
ROOT44 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
ROOT52 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
ROOT54 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
rotationFromInertial(PVCoordinates) - Method in enum org.orekit.frames.LOFType: Get the rotation from inertial frame to local orbital frame.
rotationFromInertial(Field<T>, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType: Get the rotation from inertial frame to local orbital frame.
RotationXmlTokenBuilder - Class in org.orekit.files.ccsds.ndm.adm: Builder for rotation angles and rates.
RotationXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.ndm.adm.RotationXmlTokenBuilder: Simple constructor.
Rtcm1019 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris: RTCM 1019 message: GPS Satellite Ephemeris Data.
Rtcm1019(int, Rtcm1019Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019: Constructor.
Rtcm1019Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris: Container for RTCM 1019 data.
Rtcm1019Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data: Constructor.
Rtcm1020 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris: RTCM 1020 message: Glonass Satellite Ephemeris Data.
Rtcm1020(int, Rtcm1020Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020: Constructor.
Rtcm1020Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris: Container for RTCM 1020 data.
Rtcm1020Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Constructor.
Rtcm1042 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris: RTCM 1042 message: Beidou Satellite Ephemeris Data.
Rtcm1042(int, Rtcm1042Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042: Constructor.
Rtcm1042Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris: Container for RTCM 1042 data.
Rtcm1042Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data: Constructor.
Rtcm1044 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris: RTCM 1044 message: QZSS Satellite Ephemeris Data.
Rtcm1044(int, Rtcm1044Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044: Constructor.
Rtcm1044Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris: Container for RTCM 1044 data.
Rtcm1044Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data: Constructor.
Rtcm1045 - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris: RTCM 1045 message: Galileo F/NAV Satellite Ephemeris Data.
Rtcm1045(int, Rtcm1045Data) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045: Constructor.
Rtcm1045Data - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris: Container for RTCM 1045 data.
Rtcm1045Data() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data: Constructor.
RtcmData - Class in org.orekit.gnss.metric.messages.rtcm: Container for common data in RTCM message.
RtcmData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.RtcmData
RtcmDataField - Enum in org.orekit.gnss.metric.parser: Enum containing all intermediate level data fields that can be parsed to build a RTCM message.
RtcmEphemerisData - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris: Container for common data in RTCM ephemeris message type.
RtcmEphemerisData() - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData: Constructor.
RtcmEphemerisMessage<D extends RtcmEphemerisData> - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris: Base class for RTCM ephemeris messages.
RtcmEphemerisMessage(int, D) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisMessage: Constructor.
RtcmMessage<D extends RtcmData> - Class in org.orekit.gnss.metric.messages.rtcm: Base class for RTCM messages.
RtcmMessage(int, List<D>) - Constructor for class org.orekit.gnss.metric.messages.rtcm.RtcmMessage: Constructor.
RtcmMessagesParser - Class in org.orekit.gnss.metric.parser: Parser for RTCM encoded messages.
RtcmMessagesParser(List<Integer>) - Constructor for class org.orekit.gnss.metric.parser.RtcmMessagesParser: Constructor.
RtcmMessageType - Enum in org.orekit.gnss.metric.parser: Enum containing the supported RTCM messages types.
run() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor
ruToMeters(TdmMetadata, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.tdm.IdentityConverter: Convert a range expressed in Range Units.
ruToMeters(TdmMetadata, AbsoluteDate, double) - Method in interface org.orekit.files.ccsds.ndm.tdm.RangeUnitsConverter: Convert a range expressed in Range Units.

S

S - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S2 - Static variable in class org.orekit.models.earth.displacement.Tide: S₂ tide.
s4 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: s* new value for the contant s.
s4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: s* new value for the contant s.
S_2FASX4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_3FASX6 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_FASX2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_G22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_G32 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_G44 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_G52 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
S_G54 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
SaastamoinenModel - Class in org.orekit.models.earth.troposphere: The modified Saastamoinen model.
SaastamoinenModel(double, double, double) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel: Create a new Saastamoinen model for the troposphere using the given environmental conditions and table from the reference book.
SaastamoinenModel(double, double, double, String) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel: Create a new Saastamoinen model for the troposphere using the given environmental conditions.
SaastamoinenModel(double, double, double, String, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel: Create a new Saastamoinen model for the troposphere using the given environmental conditions.
sameDimension(Unit) - Method in class org.orekit.utils.units.Unit: Check if a unit has the same dimension as another unit.
sameDimensionSI() - Method in class org.orekit.utils.units.Unit: Create the SI unit with same dimension.
sample(SphericalPolygonsSet, double, double) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator: Sample a zone of interest into a grid sample of geodetic points.
SatelliteAntenna - Class in org.orekit.gnss.antenna: GNSS satellite antenna model.
SatelliteAntenna(String, String, Map<Frequency, FrequencyPattern>, SatelliteSystem, int, SatelliteType, int, String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.gnss.antenna.SatelliteAntenna: Simple constructor.
SatelliteClockScale - Class in org.orekit.time: Scale for on-board clock.
SatelliteClockScale(String, AbsoluteDate, TimeScale, double, double) - Constructor for class org.orekit.time.SatelliteClockScale: Create a linear model for satellite clock.
SatelliteSystem - Enum in org.orekit.gnss: Enumerate for satellite system.
SatelliteType - Enum in org.orekit.gnss.antenna: Enumerate for satellite types.
SATURN - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Saturn.
SBAS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants: WGS 84 value of the Earth's universal gravitational parameter for SBAS user in m³/s².
SBASNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a SBAS navigation message.
SBASNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Constructor.
SBASOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data: This interface provides the minimal set of orbital elements needed by the SBASPropagator.
SBASPropagator - Class in org.orekit.propagation.analytical.gnss: This class aims at propagating a SBAS orbit from SBASOrbitalElements.
SBASPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss: This nested class aims at building a SBASPropagator.
SBASPropagatorBuilder(SBASOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder: Initializes the builder.
scale(double, Orbit) - Method in enum org.orekit.orbits.OrbitType: Compute scaling factor for parameters drivers.
scale(String, double) - Method in class org.orekit.utils.units.Unit: Scale a unit.
scaleChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver: Notify that a parameter scale has been changed.
ScaledConstantThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion: Thrust propulsion model with parameters (for estimation) represented by scale factors on the X, Y and Z axis of the spacecraft frame.
ScaledConstantThrustPropulsionModel(double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel: Constructor with min/max deviation for the scale factors.
Scheduler<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.generation: Interface for generating measurements sequences.
SDP4 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE: Identifier for SDP4 type of ephemeris.
SDP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE: Identifier for SDP4 type of ephemeris.
SDP8 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE: Identifier for SDP8 type of ephemeris.
SDP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE: Identifier for SDP8 type of ephemeris.
SEC_TO_MILLI - Static variable in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData: Seconds to milliseconds converter.
SECOND - Static variable in class org.orekit.utils.units.Unit: Second unit.
Section - Interface in org.orekit.files.ccsds.section: Top level interface for all CCSDS message sections.
SecularAndHarmonic - Class in org.orekit.utils: Class for fitting evolution of osculating orbital parameters.
SecularAndHarmonic(int, double...) - Constructor for class org.orekit.utils.SecularAndHarmonic: Simple constructor.
Segment<M extends Metadata,D extends Data> - Class in org.orekit.files.ccsds.section: NDM segments are (Metadata, Data) pairs.
Segment(M, D) - Constructor for class org.orekit.files.ccsds.section.Segment: Constructor.
SegmentWriter() - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter
SegmentWriter() - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter
select(Unit, Unit) - Method in enum org.orekit.files.ccsds.ndm.ParsedUnitsBehavior: Select the unit to use for interpreting parsed value.
select(DataSource) - Static method in class org.orekit.files.ccsds.utils.lexical.LexicalAnalyzerSelector: Select a LexicalAnalyzer for a DataSource based on content.
selectDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.BurstSelector: Select dates within an interval.
selectDates(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.time.DatesSelector: Select dates within an interval.
selectDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.FixedStepSelector: Select dates within an interval.
selectExtrapolator(FieldTLE<T>, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Selects the extrapolator to use with the selected TLE.
selectExtrapolator(FieldTLE<T>, Frames, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Selects the extrapolator to use with the selected TLE.
selectExtrapolator(FieldTLE<T>, AttitudeProvider, T, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Selects the extrapolator to use with the selected TLE.
selectExtrapolator(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator: Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE, Frames) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator: Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE, AttitudeProvider, double) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator: Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE, AttitudeProvider, double, Frame) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator: Selects the extrapolator to use with the selected TLE.
selectionChanged(boolean, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver: Notify that a parameter selection status has been changed.
selectTransformer(Transformer, double, boolean) - Method in enum org.orekit.propagation.events.FilterType: Get next function transformer in the specified direction.
SEMI_CIRCLE - Static variable in class org.orekit.gnss.metric.parser.Units: Semi-circles units.
SemiAnalyticalKalmanEstimator - Class in org.orekit.estimation.sequential: Implementation of an Extended Semi-analytical Kalman Filter (ESKF) to perform orbit determination.
SemiAnalyticalKalmanEstimator(MatrixDecomposer, DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator: Kalman filter estimator constructor (package private).
SemiAnalyticalKalmanEstimatorBuilder - Class in org.orekit.estimation.sequential: Builder for a Semi-analytical Kalman Filter.
SemiAnalyticalKalmanEstimatorBuilder() - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder: Default constructor.
SemiAnalyticalKalmanModel - Class in org.orekit.estimation.sequential: Process model to use with a SemiAnalyticalKalmanEstimator.
SemiAnalyticalKalmanModel(DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Kalman process model constructor (package private).
SEMParser - Class in org.orekit.gnss: This class reads SEM almanac files and provides GPS almanacs.
SEMParser(String) - Constructor for class org.orekit.gnss.SEMParser: Simple constructor.
SEMParser(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.gnss.SEMParser: Create a SEM loader/parser with the given source of SEM auxiliary data files.
SequentialBatchLSEstimator - Class in org.orekit.estimation.leastsquares: Sequential least squares estimator for orbit determination.
SequentialBatchLSEstimator(SequentialGaussNewtonOptimizer, OrbitDeterminationPropagatorBuilder...) - Constructor for class org.orekit.estimation.leastsquares.SequentialBatchLSEstimator: Simple constructor.
setA(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Set the orbit semi-major axis.
setA(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector: Set acceleration component.
setA2b(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints: Set rotation direction.
setAcceleration(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set acceleration component.
setAccelerationDirectionSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set one σ angular off-nominal acceleration direction.
setAccelerationInterpolation(OnOff) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set interpolation mode between current and next acceleration line.
setAccelerationMagnitudeSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set one σ percent error on acceleration magnitude.
setAccuracy(int, double) - Method in class org.orekit.files.sp3.SP3: Set the formal accuracy for a satellite.
setAccuracy(double) - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris: Set the accuracy for this satellite.
setAccuracyProvider(AccuracyProvider) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData: Set the accuracy provider of the ephemeris message.
setActualOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set actual time span used for the OD of the object.
setAdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the Unique identifier of Attitude Data Message linked to this Orbit Data Message.
setAe(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the central body reference radius.
setAf0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Setter for the SV Clock Bias Correction Coefficient (s).
setAf1(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Setter for the SV Clock Drift Correction Coefficient (s/s).
setAf2(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Setter for the Drift Rate Correction Coefficient (s/s²).
setAgency(String) - Method in class org.orekit.files.sp3.SP3: Set the agency string for this SP3 file.
setAgencyName(String) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the agency name.
setAgencyName(String) - Method in class org.orekit.gnss.navigation.RinexNavigation: Setter for the agency name.
setAGf0(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Setter for the SV clock bias.
setAGf1(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Setter for the SV relative frequency.
setAlbedoGridSize(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set albedo grid size.
setAlbedoModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set albedo model.
setAlternateNames(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the alternate names for this space object.
setAmplifierBandwidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the amplifier bandwidth.
setAmplifierGain(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the amplifier gain.
setAmplifierInUse(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the amplifier in use.
setAnalysisCenterID(String) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the analysis center ID.
setAnalysisCenterName(String) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the analysis center name.
setAngleType(AngleType) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the angleType.
setAngularThreshold(double) - Method in class org.orekit.bodies.OneAxisEllipsoid: Set the angular convergence threshold.
setAnomaly(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Set the orbit anomaly.
setAnomalyType(PositionAngle) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Set the type of anomaly.
setAODC(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage: Setter for the age of data clock.
setAODE(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage: Setter for the age of data ephemeric.
setApplicableWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the applicable wavelength.
setAppliedVoltage(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the applied voltage.
setAreAdditionalDataAvailable(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the flag indicating if additional parameters are in the message.
setAtmosphericModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set name of atmospheric model.
setAttitudeActuatorType(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the type of actuator for attitude control.
setAttitudeControlAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the accuracy of attitude control.
setAttitudeControlMode(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the attitude control mode.
setAttitudeKnowledgeAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the accuracy of attitude knowledge.
setAttitudePointingAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the overall accuracy of spacecraft to maintain attitude.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.AbstractPropagator: Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Set the attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.FieldAbstractPropagator: Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.FieldPropagator: Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.StateMapper: Set the attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.Propagator: Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Set attitude provider.
setAttitudeType(AttitudeType) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Set the format of the data lines in the message.
setBeamDivergence(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Set the beam divergence.
setBeidouNavigationMessage(BeidouNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data: Set the Beidou navigation message.
setBeidouToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data: Set the Beidou time of clock.
setBGDE1E5a(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Setter for the E1/E5a broadcast group delay (s).
setBGDE5bE1(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Setter for the E5b/E1 broadcast group delay (s).
setBN(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the GLONASS B_n Word.
setBolDv(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the total ΔV capability at beginning of life.
setBStar(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Set the SGP/SGP4 drag-like coefficient.
setBusModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the bus model name.
setCacheSlotsNumber(int) - Static method in class org.orekit.utils.OrekitConfiguration: Set the number of slots to use in caches.
setCatalogName(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the specification of satellite catalog source.
setCdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the Unique identifier of Conjunction Data Message linked to this Orbit Data Message.
setCelestialSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the source and version of celestial body (e.g.
setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata: Set the body at origin of reference frame.
setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata: Set the origin of reference frame.
setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set the origin of reference frame.
setCenterOfMassOffset(double) - Method in class org.orekit.files.ilrs.CPFHeader: Set the approximate center of mass to reflector offset.
setCentralBodyRotation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set central body angular rotation rate.
setCic(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Setter for te Cic parameter.
setCis(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Setter for the Cis parameter.
setClassification(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the message classification.
setClassificationType(char) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Set the classification type.
setClockCorrection(ClockCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data: Set the clock correction data.
setClockCorrection(ClockCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data: Set the clock correction data.
setClosedOrbitConstraint(boolean) - Method in class org.orekit.utils.AbstractMultipleShooting: Set the constraint of a closed orbit or not.
setCnm(double[][]) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data: Set the cosine parameters of spherical harmonics expansion of degree N and order M.
setComparator(Comparator<IntegerLeastSquareSolution>) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Set a custom comparator for integer least square solutions comparison.
setConfidence(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set confidence metric.
setConfigurationRecords(CRDConfiguration) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Set the configuration records for the current data block.
setConsiderN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set number of consider parameters.
setConsiderParameters(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set description of consider parameters.
setConstellation(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the name of the constellation this space object belongs to.
setContext(ContextBinding) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter: Reset context binding.
setConvergenceChecker(ConvergenceChecker<LeastSquaresProblem.Evaluation>) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Set a custom convergence checker.
setConvergenceRMS(double) - Method in class org.orekit.utils.SecularAndHarmonic: Set RMS for convergence.
setCoordinateSystem(String) - Method in class org.orekit.files.sp3.SP3: Set the coordinate system used for the orbit entries.
setCorrectionAberrationDiurnal(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the diurnal aberration correction.
setCorrectionAberrationYearly(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the yearly aberration correction.
setCorrectionAngle1(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the correctionAngle1.
setCorrectionAngle2(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the correctionAngle2.
setCorrectionDoppler(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the correctionDoppler.
setCorrectionMagnitude(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the magnitude correction.
setCorrectionRcs(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the radar cross section correction.
setCorrectionReceive(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the correctionReceive.
setCorrectionsApplied(CorrectionApplied) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the correctionApplied.
setCorrectionTransmit(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the correctionTransmit.
setCountry(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the name of the country where the space object owner is based.
setCovarianceMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance: Set an entry in the Position/Velocity covariance matrix.
setCovBasis(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Set basis of this covariance time history data.
setCovBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Set identification number of the orbit determination or simulation upon which this covariance is based.
setCovConfidence(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Set the measure of confidence in covariance error matching reality.
setCovFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Set epoch of the covariance reference frame.
setCovID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Set covariance identification number.
setCovNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Set identification number of next covariance.
setCovOrdering(Ordering) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Set covariance ordering.
setCovPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Set identification number of previous covariance.
setCovReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Set reference frame of the covariance.
setCovScaleMax(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Set the maximum scale factor to apply to achieve realism.
setCovScaleMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Set the minimum scale factor to apply to achieve realism.
setCovType(ElementsType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Set covariance element set type.
setCovUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata: Set covariance element set units.
setCrc(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Setter for the Crc parameter.
setCreationDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.section.Header: Set the file creation date and time in UTC.
setCreationDate(AbsoluteDate) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the creation date.
setCreationDate(AbsoluteDate) - Method in class org.orekit.gnss.navigation.RinexNavigation: Setter for the creation date.
setCreationDateString(String) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the creation date as a string.
setCreationDateString(String) - Method in class org.orekit.gnss.navigation.RinexNavigation: Setter for the creation date as a string.
setCreationTimeString(String) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the creation time as a string.
setCreationTimeString(String) - Method in class org.orekit.gnss.navigation.RinexNavigation: Setter for the creation time as a string.
setCreationTimeZoneString(String) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the creation time zone.
setCreationTimeZoneString(String) - Method in class org.orekit.gnss.navigation.RinexNavigation: Setter for the creation time zone.
setCrs(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Setter for the Crs parameter.
setCrsIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header: Set the Global/Regional CRS Indicator.
setCrsIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header: Set the Global/Regional CRS Indicator.
setCuc(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Setter for the Cuc parameter.
setCus(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Setter for the Cus parameter.
setDarkCount(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the dark count.
setDataQuality(DataQuality) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the dataQuality.
setDataReleaseFlag(int) - Method in class org.orekit.files.ilrs.CRDHeader: Set the flag indicating the data release.
setDataType(int) - Method in class org.orekit.files.ilrs.CRDHeader: Set the data type.
setDataTypes(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set observation data types used.
setDataTypes(List<ObservationType>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the data types in the data section.
setDataUsed(String) - Method in class org.orekit.files.sp3.SP3: Set the data used indicator for this SP3 file.
setDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set date.
setDate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Setter for the reference date of the ephemeris.
setDate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Setter for the reference epoch.
setDateAndTime(String) - Method in class org.orekit.files.ilrs.CRDHeader: Set the string value of date and time.
setDayFraction(double) - Method in class org.orekit.files.sp3.SP3: Set the day fraction for this SP3 file.
setDcBodyFrame(SpacecraftBodyFrame) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set spacecraft body frame in which ManeuverHistoryMetadata.getDcBodyTrigger() is specified.
setDcBodyTrigger(Vector3D) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set direction in body frame for triggering duty cycle.
setDcExecStart(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set the start time of initial duty cycle-based maneuver execution.
setDcExecStop(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set the end time of final duty cycle-based maneuver execution.
setDcMaxCycles(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set the maximum number of "ON" duty cycles.
setDcMinCycles(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set the minimum number of "ON" duty cycles.
setDcPhaseStartAngle(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set phase angle of pulse start.
setDcPhaseStopAngle(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set phase angle of pulse stop.
setDcRefDir(Vector3D) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set reference direction for triggering duty cycle.
setDcRefTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set duty cycle thrust reference time.
setDcTimePulseDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set duty cycle pulse "ON" duration.
setDcTimePulsePeriod(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set duty cycle elapsed time between start of a pulse and start of next pulse.
setDcType(DutyCycleType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set type of duty cycle.
setDcWindowClose(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set the end time of duty cycle-based maneuver window.
setDcWindowOpen(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set the start time of duty cycle-based maneuver window.
setDefault(LazyLoadedDataContext) - Static method in interface org.orekit.data.DataContext: Set the default data context that is used to implement Orekit's static factories.
setDeltaInc(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac: Sets the the correction of orbit reference inclination at reference time.
setDeltaMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set mass change.
setDeltaMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver: Set mass change during maneuver (value is < 0).
setDeltaN(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Setter for the delta of satellite mean motion.
setDeltaSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac: Sets the difference between the square root of the semi-major axis and the square root of the nominal semi-major axis.
setDeltaTN(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the deltaTauN value.
setDeployDirSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set one σ angular off-nominal deployment vector direction.
setDeployDv(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set velocity increment component of deployed "child" object.
setDeployDvCda(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.
setDeployDvRatio(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set ratio of child-to-host ΔV vectors.
setDeployDvSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set one σ percent error on deployment ΔV magnitude.
setDeployId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set identifier of resulting "child" object deployed from this host.
setDeployMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set decrement in host mass as a result of deployment.
setDetectorId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the detector configuration ID.
setDetectorRecord(CRDConfiguration.DetectorConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Set the detector configuration record.
setDetectorType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the detector type.
setDockedWith(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the other space objects this object is docked to.
setDomes(String) - Method in class org.orekit.files.sinex.Station: Set the DOMES number.
setDopplerCountBias(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Set the Doppler count bias.
setDopplerCountRollover(boolean) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Set the indicator for Doppler count rollover.
setDopplerCountScale(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Set the Doppler count Scale.
setDragArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters: Set the drag area.
setDragCoeff(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters: Set the drag coefficient.
setDragCoefficient(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the the nominal drag coefficient.
setDragConstantArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
setDragUncertainty(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the drag coefficient 1σ uncertainty.
setDryMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the mass without propellant.
setDuration(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver: Set duration (value is 0 for impulsive maneuver).
setDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set duration.
setDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver: Set duration (value is 0 for impulsive maneuver).
setDv(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set velocity increment component.
setDV(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver: Set velocity increment component.
setDvDirSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set one σ angular off-nominal ΔV direction.
setDvMagSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set one σ percent error on ΔV magnitude.
setE(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Set the orbit eccentricity.
setE(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Setter the eccentricity.
setEccentricities(Vector3D) - Method in class org.orekit.files.sinex.Station: Set the last known station antenna eccentricities.
setEccRefSystem(Station.ReferenceSystem) - Method in class org.orekit.files.sinex.Station: Set the reference system used to define the eccentricity vector (local or cartesian).
setElem(int, int, PolynomialFunction) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix: Set an element of the matrix.
setElementSetNo(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Set the element set number for this satellite.
setEn(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS E_n Word.
setEnabled(boolean) - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Enable or disable a measurement.
setEnabled(boolean) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Enable or disable a measurement.
setEndEpoch(AbsoluteDate) - Method in class org.orekit.files.ilrs.ILRSHeader: Set the ending epoch (UTC).
setEndTagSeen(boolean) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser: Set the flag for XML end tag.
setEOPContinuityThreshold(double) - Static method in class org.orekit.frames.FramesFactory: Set the threshold to check EOP continuity.
setEOPContinuityThreshold(double) - Method in class org.orekit.frames.LazyLoadedEop: Set the threshold to check EOP continuity.
setEOPContinuityThreshold(double) - Method in class org.orekit.frames.LazyLoadedFrames: Set the threshold to check EOP continuity.
setEopSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the source and version of Earth Orientation Parameters.
setEphemerisNames(Map<Integer, String>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the external ephemeris names for participants.
setEphemerisType(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Set the ephemeris type.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion: Set the epoch of the data.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance: Set matrix epoch.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Set epoch of state vector, Keplerian elements and covariance matrix data.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set time tag for orbit determination solved-for state.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector: Set epoch of state vector, Keplerian elements and covariance matrix data.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.sinex.Station: Set the coordinates reference epoch.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.sp3.SP3: Set the epoch of the SP3 file.
setEpochDelayCorrection(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration: Set the epoch delay correction.
setEpochEigenMaj(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set positional error ellipsoid 1σ major eigenvalue at the epoch of OD.
setEpochEigenMed(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set positional error ellipsoid 1σ intermediate eigenvalue at the epoch of OD.
setEpochEigenMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set positional error ellipsoid 1σ minor eigenvalue at the epoch of OD.
setEpochFreedom(int, boolean) - Method in class org.orekit.utils.AbstractMultipleShooting: Set the epoch a patch point to free or not.
setEpochIdentifier(int) - Method in class org.orekit.files.ilrs.CRDHeader: Set the epoch identifier.
setEpochIgnition(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver: Set epoch ignition.
setEpochInterval(double) - Method in class org.orekit.files.sp3.SP3: Set the epoch interval for this SP3 file.
setEpochStart(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver: Set epoch start.
setEpochT0(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the epoch to which all relative times are referenced in data blocks.
setEpochToc(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Setter for the time of clock epoch.
setEpochToc(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Setter for the time of clock epoch.
setEquatorialRadius(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set oblate spheroid equatorial radius of central body.
setEstimatedValue(double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Set the estimated value.
setEulerRotSeq(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Set the rotation order for Euler angles.
setEulerRotSeq(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler: Set the rotation order for Euler angles.
setEvaluationsCounter(Incrementor) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel: Set the counter for evaluations.
setExternalClockReference(String) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the external clock reference.
setExternalSignalProcessing(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the external signal processing.
setFallback(ProcessingState) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser: Set fallback processing state.
setFileType(String) - Method in class org.orekit.gnss.navigation.RinexNavigation: Setter for the file type.
setFilter(CartesianDerivativesFilter) - Method in class org.orekit.files.ilrs.CPF: Set the derivatives filter.
setFilter(CartesianDerivativesFilter) - Method in class org.orekit.files.sp3.SP3: Set the derivatives filter.
setFiring(boolean, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers: Set the firing start or end date depending on the firing flag.
setFix(int, int, double, double, double, double, double) - Method in class org.orekit.gnss.metric.ntrip.NtripClient: Set GPS fix data to send as NMEA sentence to Ntrip caster if required.
setFixedF10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set fixed (time invariant) value of the Solar Flux Unit daily proxy F10.7.
setFixedF10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set fixed (time invariant) value of the Solar Flux Unit 81-day running center-average proxy F10.7.
setFixedGeomagneticAp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set fixed (time invariant) value of the planetary 3-hour-range geomagnetic index aₚ.
setFixedGeomagneticDst(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set fixed (time invariant) value of the planetary 1-hour-range geomagnetic index Dst.
setFixedGeomagneticKp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set fixed (time invariant) value of the planetary 3-hour-range geomagnetic index Kₚ.
setFixedM10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set fixed (time invariant) value of the Solar Flux daily proxy M10.7.
setFixedM10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy M10.7.
setFixedS10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set fixed (time invariant) value of the Solar Flux daily proxy S10.7.
setFixedS10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy S10.7.
setFixedY10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set fixed (time invariant) value of the Solar Flux daily proxy Y10.7.
setFixedY10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy Y10.7.
setFormat(String) - Method in class org.orekit.files.ilrs.ILRSHeader: Set the file format.
setFormatVersion(double) - Method in class org.orekit.files.ccsds.section.Header: Set the CCSDS NDM (ADM, ODM or TDM) format version.
setFormatVersion(double) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the format version.
setFormatVersion(double) - Method in class org.orekit.gnss.navigation.RinexNavigation: Setter for the format version.
setFrameA(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints: Set frame A.
setFrameB(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints: Set frame B.
setFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata: Set epoch of reference frame, if not intrinsic to the definition of the reference frame.
setFrameEpochString(String) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata: Set epoch of reference frame, if not intrinsic to the definition of the reference frame.
setFrameName(String) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the frame name.
setFreqOffset(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the freqOffset.
setFrequencyNumber(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Setter for the frequency number.
setFrequencySource(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration: Set the frequency source.
setFT(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the GLONASS F_T Word.
setGalileoDataValidityStatus(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data: Set the Galileo data validity status.
setGalileoNavigationMessage(GalileoNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data: Set the Galileo navigation message.
setGalileoToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data: Set the Galileo time of clock.
setGammaN(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Setter for the SV relative frequency bias.
setGdop(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set generalize Dilution Of Precision.
setGlonassNavigationMessage(GLONASSNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the Glonass navigation message.
setGm(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set gravitational coefficient of attracting body.
setGnssIod(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data: Set the GNSS IOD.
setGnssIod(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data: Set the GNSS IOD.
setGpsCodeOnL2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data: Set the GPS code on L2.
setGpsFitInterval(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data: Set the GPS fit interval.
setGpsL2PDataFlag(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data: Set the GPS L2 P-code data flag.
setGpsNavigationMessage(GPSNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data: Set the GPS navigation message.
setGpsToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data: Set the GPS time of clock.
setGpsWeek(int) - Method in class org.orekit.files.sp3.SP3: Set the GPS week of the SP3 file.
setGravitationalAssist(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set the origin of gravitational assist.
setGravityModel(String, int, int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set gravity model.
setHandlers(List<EventHandler<D>>) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler: Change handlers list with user input.
setHarvesters(MatricesHarvester[]) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Setter for the jacobian harvesters.
setHeader(CRDHeader) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Set the header for the current data block.
setHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Setter for the health status.
setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac: Sets the health status.
setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Sets the health status.
setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac: Sets the health status.
setHealthAvailabilityIndicator(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the flag indicating if GLONASS almanac health is available.
setHealthE1(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac: Sets the E1-B/C signal health status.
setHealthE5a(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac: Sets the E5a signal health status.
setHealthE5b(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac: Sets the E5b signal health status.
setHeightIonosphericLayer(double) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data: Set the height of the ionospheric layer.
setHighRateClockCorrection(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data: Set the high rate clock correction to be added to the polynomial clock correction.
setHumiSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Set the humidity sensor manufacturer.
setHumiSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Set the humidity sensor model.
setHumiSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Set the humidity sensor serial number.
setI(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Set the orbit inclination.
setI0(double, double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac: Sets the Inclination Angle at Reference Time (rad).
setI0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Setter for the Inclination Angle at Reference Time (rad).
setI11(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Set the moment of Inertia about the 1-axis (N.m²).
setI12(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Set the moment of Inertia about the 1 and 2 axes (N.m²).
setI13(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Set the moment of Inertia about the 1 and 3 axes (N.m²).
setI22(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Set the moment of Inertia about the 2-axis (N.m²).
setI23(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Set the moment of Inertia about the 2 and 3 axes (N.m²).
setI33(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Set the moment of Inertia about the 3-axis (N.m²).
setId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set identification number.
setIDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Setter for the Rate of Inclination Angle (rad/s).
setIgnoreCentralAttraction(boolean) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Set the flag to ignore or not the creation of a NewtonianAttraction.
setIgnoreCentralAttraction(boolean) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Set the flag to ignore or not the creation of a NewtonianAttraction.
setIlrsSatelliteId(String) - Method in class org.orekit.files.ilrs.ILRSHeader: Set the IRLS satellite ID (based on COSPAR ID).
setInertiaMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set an entry in the inertia matrix.
setInertiaReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Set the coordinate system for the inertia tensor.
setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.analytical.tle.TLEJacobiansMapper: Set the Jacobian with respect to state into a one-dimensional additional state array.
setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations: Deprecated.

Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations: Deprecated.

Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper: Set the Jacobian with respect to state into a one-dimensional additional state array.
setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations: Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations: Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.numerical.JacobiansMapper: Set the Jacobian with respect to state into a one-dimensional additional state array.
setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Deprecated.

Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Deprecated.

Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper: Set the Jacobian with respect to state into a one-dimensional additional state array.
setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations: Deprecated.

Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations: Deprecated.

Set the initial value of the Jacobian with respect to state and parameter.
setInitialPhi(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations: Method adding the standard initial values of the additional state to the initial spacecraft state.
setInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Set the initial state.
setInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Set the initial state.
setInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Set the initial state with osculating orbital elements.
setInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Set the initial state.
setInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Set the initial state with osculating orbital elements.
setInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Set the initial state.
setInitialWetMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the total mass at beginning of life.
setInRotationAngles(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler: Set flag for rotation angle parsing.
setIntegrationInterval(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the integrationInterval.
setIntegrationRef(IntegrationReference) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the integrationRef.
setInternationalDesignator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the international designator for the object.
setInterpMethodEOP(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the interpolation method for Earth Orientation Parameters.
setInterpMethodSW(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set the interpolation method for Space Weather data.
setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Set the interpolation degree.
setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set the interpolation degree.
setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata: Set the interpolation degree.
setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Set the interpolation degree.
setInterpolationGridToFixedNumberOfPoints(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Set the interpolation grid generator.
setInterpolationGridToFixedNumberOfPoints(int) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Set the interpolation grid generator.
setInterpolationGridToMaxTimeGap(double) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Set the interpolation grid generator.
setInterpolationGridToMaxTimeGap(T) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Set the interpolation grid generator.
setInterpolationMethod(String) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Set the interpolation method to be used.
setInterpolationMethod(InterpolationMethod) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set the interpolation method to be used.
setInterpolationMethod(InterpolationMethod) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata: Set the interpolation method to be used.
setInterpolationMethod(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Set the interpolation method to be used.
setInterpolationSample(int) - Method in class org.orekit.files.ilrs.CPF: Set the interpolation sample.
setIOD(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac: Sets the Issue of Data (IOD).
setIODC(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage: Setter for the Issue of Data Clock.
setIODC(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage: Setter for the Issue of Data, Clock.
setIODE(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage: Setter for the Issue of Data Ephemeris.
setIODE(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage: Setter for the Issue of Data, Ephemeris.
setIODEC(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage: Setter for the Issue of Data, Ephemeris and Clock.
setIODN(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Setter for the issue of data navigation.
setIODNav(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Setter for the Issue of Data of the navigation batch.
setIodSsr(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader: Set the IOD SSR.
setIonosphericCorrectionType(String) - Method in class org.orekit.gnss.navigation.RinexNavigation: Setter for the ionospheric correction type.
setIsCenterOfMassCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CPFHeader: Set the flag telling if the center of mass correction is applied.
setIsCenterOfMassCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader: Set the center of mass correction applied indicator.
setIsCompatibleWithTIVs(boolean) - Method in class org.orekit.files.ilrs.CPFHeader: Set the flag for compatibility with TIVs.
setIsConsistencyMaintained(boolean) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header: Set the flag indicating if phase biases maintain consistency between non-dispersive and all original dispersive phase signals.
setIsFirst(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Set the flag for the placement of the quaternion QC in the attitude data.
setIsMelbourneWubbenaConsistencyMaintained(boolean) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header: Set the flag indicating if consistency between code and phase biases is maintained for the MW combinations.
setIsReceiveAmplitudeCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader: Set the receive amplitude correction applied indicator.
setIsSpacecraftTimeSimplified(boolean) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Set the spacecraft time simplified flag.
setIsStationSystemDelayApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader: Set the station system delay applied indicator.
setIsTransponderDelayApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader: Set the spacecraft system delay applied (transponders) indicator.
setIsTroposphericRefractionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader: Set the tropospheric refraction correction applied indicator.
setIterationsCounter(Incrementor) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel: Set the counter for iterations.
setJulianDay(int) - Method in class org.orekit.files.sp3.SP3: Set the julian day for this SP3 file.
setKlobucharAlpha(double[]) - Method in class org.orekit.gnss.navigation.RinexNavigation: Set the "alpha" ionspheric parameters.
setKlobucharBeta(double[]) - Method in class org.orekit.gnss.navigation.RinexNavigation: Set the "beta" ionospheric parameters.
setLaserId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Set the laser configuration ID.
setLaserRecord(CRDConfiguration.LaserConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Set the laser configuration record.
setLaserType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Set the laser type.
setLNFifthString(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the GLONASS l_n Word extracted from fifth string of the subframe.
setLNThirdString(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the GLONASS l_n Word extracted from third string of the subframe.
setLocalTimingId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration: Set the local timing system configuration ID.
setLowElevationThreshold(double) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel: Set the low elevation threshold value for path delay computation.
setM(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the GLONASS M Word.
setM0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Setter for the Mean Anomaly at Reference Time (rad).
setMainFieldCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField: Set the given main field coefficients.
setManBasis(ManBasis) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set basis of this maneuver history data.
setManBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set identification number of the orbit determination or simulation upon which this maneuver is based.
setManComposition(List<ManeuverFieldType>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set maneuver element of information.
setManDeviceID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set identifier of the device used for this maneuver.
setManeuversFrequency(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the average frequency of orbit or attitude maneuvers (in SI units, hence per second).
setManFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set epoch of the maneuver reference frame.
setManID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set maneuver identification number.
setManNextEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set start time of next maneuver.
setManNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set identification number of next maneuver.
setManPredSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set prediction source on which this maneuver is based.
setManPrevEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set completion time of previous maneuver.
setManPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set identification number of previous maneuver.
setManPurpose(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set the purposes of the maneuver.
setManReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set reference frame of the maneuver.
setManufacturer(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set manufacturer name.
setManUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata: Set maneuver element of information units.
setMappers(AbstractJacobiansMapper[]) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Deprecated.
as of 11.1, replaced by AbstractKalmanModel.setHarvesters(MatricesHarvester[])
setMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters: Set the spacecraft mass.
setMass(double) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder: Set the initial mass.
setMass(double) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Set the initial mass.
setMatrix(PolynomialFunction[][]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix: Set values for all elements.
setMatrixLine(int, PolynomialFunction[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix: Set the value of a line of the matrix.
setMaxAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the maximum cross-sectional area for collision probability estimation purposes.
setMaxEvaluations(int) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Set the maximum number of model evaluations.
setMaximumObsGap(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set maximum time between observations in the OD of the object.
setMaxIter(int) - Method in class org.orekit.utils.SecularAndHarmonic: Set maximum number of iterations.
setMaxIterations(int) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Set the maximum number of iterations.
setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Set the degree limit for the next file parsing.
setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the degree limit for the next file parsing.
setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Set the order limit for the next file parsing.
setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the order limit for the next file parsing.
setMaxPredictedEigenMaj(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set maximum predicted major eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
setMaxRcs(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the maximum radar cross-section.
setMaxThrust(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the maximum composite thrust the spacecraft can accomplish.
setMaxValue(double) - Method in class org.orekit.utils.ParameterDriver: Set maximum parameter value.
setMeanElementTheory(String) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata: Set the description of the Mean Element Theory.
setMeanMotion(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Set the orbit mean motion.
setMeanMotionDot(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Set the first time derivative of the mean motion.
setMeanMotionDotDot(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Set the second time derivative of the mean motion.
setMessageId(String) - Method in class org.orekit.files.ccsds.section.Header: Set the ID that uniquely identifies a message from a given originator.
setMeteorologicalId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Set the meteorological configuration ID.
setMeteorologicalRecord(CRDConfiguration.MeteorologicalConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Set the meteorological record.
setMethod(OdMethodFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set orbit determination method.
setMinAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the minimum cross-sectional area for collision probability estimation purposes.
setMinPredictedEigenMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set minimum predicted minor eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
setMinRcs(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the minimum radar cross-section.
setMinValue(double) - Method in class org.orekit.utils.ParameterDriver: Set minimum parameter value.
setMode(TrackingMode) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the mode.
setMu(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Set the gravitational coefficient.
setMu(double) - Method in class org.orekit.files.ilrs.CPF: Set the gravitational coefficient.
setMu(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the central body attraction coefficient.
setMu(double) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set the central attraction coefficient μ.
setMu(T) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Set the central attraction coefficient μ.
setMu(T) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Set the central attraction coefficient μ.
setMu(double) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Set the central attraction coefficient μ.
setMu(double) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Set the central attraction coefficient μ.
setMu(T) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Set the central attraction coefficient μ.
setMuCreated(double) - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser: Set the gravitational coefficient created from the knowledge of the central body.
setMuParsed(double) - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser: Set the gravitational coefficient parsed in the ODM File.
setN4(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the four-year interval number starting from 1996.
setNA(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the GLONASS N^A Word.
setName(int, SatelliteSystem) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector: Create the name of a satellite from its PRN number and satellite System it belongs to.
setName(String) - Method in class org.orekit.files.ilrs.ILRSHeader: Set the satellite target name.
setName(String) - Method in class org.orekit.utils.ParameterDriver: Change the name of this parameter driver.
setNBodyPerturbations(List<BodyFacade>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set n-body perturbation bodies.
setNeQuickAlpha(double[]) - Method in class org.orekit.gnss.navigation.RinexNavigation: Set the "alpha" ionospheric parameters.
setNextMessageEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the creation date of next message from a given originator.
setNextMessageID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the unique ID identifying next message from a given originator.
setNominalFireRate(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Set the nominal fire rate.
setNoradID(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Set the NORAD Catalog Number ("Satellite Number").
setNoradId(String) - Method in class org.orekit.files.ilrs.ILRSHeader: Set the satellite NORAD ID.
setNormalizedValue(double) - Method in class org.orekit.utils.ParameterDriver: Set normalized value.
setNt(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the current date.
setNumberOfBiasesProcessed(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data: Set the number of biases processed for the current satellite.
setNumberOfBiasesProcessed(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data: Set the number of biases processed for the current satellite.
setNumberOfEpochs(int) - Method in class org.orekit.files.sp3.SP3: Set the number of epochs as contained in the SP3 file.
setNumberOfIonosphericLayers(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header: Set the number of ionospheric layers.
setNumberOfLeapSeconds(int) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the number of leap seconds.
setNumberOfLeapSeconds(int) - Method in class org.orekit.gnss.navigation.RinexNavigation: Setter for the current number of leap seconds.
setNumberOfLeapSecondsGNSS(int) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the number of leap seconds for GNSS time scales.
setNumberOfSatellites(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader: Set the number of satellites for the current IGM message.
setNutation(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Set the nutation angle of spin axis (rad).
setNutationPeriod(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Set the body nutation period of the spin axis (s).
setNutationPhase(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Set the inertial nutation phase (rad).
setObjectDesignator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the unique satellite identification designator for the object.
setObjectID(String) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata: Set the spacecraft ID for which the attitude data are provided.
setObjectID(String) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata: Set the spacecraft ID for which the orbit state is provided.
setObjectName(String) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata: Set the spacecraft name for which the attitude data are provided.
setObjectName(String) - Method in class org.orekit.files.ccsds.ndm.odm.OdmMetadata: Set the spacecraft name for which the orbit state is provided.
setObjectType(ObjectType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the type of object.
setOblateFlattening(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set central body oblate spheroid oblateness.
setObsAvailable(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set number of observations available within the actual OD span.
setObservations(List<Observation>) - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock: Set the list of Observations Data Lines.
setObserver(BatchLSObserver) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Set an observer for iterations.
setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.KalmanEstimator: Set the observer.
setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator: Set the observer.
setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Set the observer.
setObsUsed(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set number of observations accepted within the actual OD span.
setOceanTidesModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set ocean tides model.
setOcmDataElements(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the list of elements of information data blocks included in this message.
setOebAreaAlongIntermediate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the cross-sectional area of Optimally Enclosing Box along Y-OEB.
setOebAreaAlongMax(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the cross-sectional area of Optimally Enclosing Box along X-OEB.
setOebAreaAlongMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the cross-sectional area of Optimally Enclosing Box along Z-OEB.
setOebIntermediate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
setOebMax(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the dimensions of Optimally Enclosing Box along X-OEB (i.e max).
setOebMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the dimensions of Optimally Enclosing Box along Z-OEB (i.e min).
setOebParentFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the Optimally Enclosing Box parent reference frame.
setOebParentFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the Optimally Enclosing Box parent reference frame epoch.
setOebQ(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: set the component of quaternion defining Optimally Enclosing Box.
setOmega0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Setter for the Longitude of Ascending Node of Orbit Plane at Weekly Epoch (rad).
setOmegaDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Setter for the rate of Rate of Right Ascension (rad/s).
setOperator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the operator of the space object.
setOpsStatus(OpsStatus) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the operational status.
setOrbAveraging(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set type of averaging (Osculating, mean Brouwer, other.
setOrbitCategory(OrbitCategory) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the orbit category.
setOrbitCorrection(OrbitCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data: Set the orbit correction data.
setOrbitCorrection(OrbitCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data: Set the orbit correction data.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set propagation orbit type.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Set propagation orbit type.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Set propagation orbit type.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Set propagation orbit type.
setOrbitTypeKey(String) - Method in class org.orekit.files.sp3.SP3: Set the orbit type key for this SP3 file.
setOrbRevNum(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set the integer orbit revolution number.
setOrbRevNumBasis(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set the basis for orbit revolution number.
setOriginator(String) - Method in class org.orekit.files.ccsds.section.Header: Set the file originator.
setOriginatorAddress(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the address of Programmatic Point Of Contact at originator.
setOriginatorPhone(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: GSet the phone number of Programmatic Point Of Contact at originator.
setOriginatorPOC(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the programmatic Point Of Contact at originator.
setOriginatorPosition(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the position of Programmatic Point Of Contact at originator.
setOutputPulseType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the output pulse type.
setOutputPulseWidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the output pulse width.
setOwner(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the owner of the space object.
setP(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector: Set position component.
setP(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the GLONASS P Word.
setP1(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the GLONASS P1 Word.
setP2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the GLONASS P2 Word.
setP3(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the the GLONASS P3 Word.
setP4(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the GLONASS P4 Word.
setPa(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Set the orbit argument of pericenter.
setPa(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Setter fir the Argument of Perigee (rad).
setParameterDerivatives(ParameterDriver, double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Set the partial derivatives of the simulated measurement with respect to parameter.
setParameters(double[]) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Set the selected parameters.
setParametersConvergenceThreshold(double) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Set convergence threshold.
setParticipants(Map<Integer, String>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the participants.
setPatchPointComponentFreedom(int, int, boolean) - Method in class org.orekit.utils.AbstractMultipleShooting: Set a component of a patch point to free or not.
setPath(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the path.
setPath1(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the path1.
setPath2(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the path2.
setPosition(Vector3D) - Method in class org.orekit.files.sinex.Station: Set the station position.
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set position angle type.
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Set position angle type.
setPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper: Set position angle type.
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Set position angle type.
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Set position angle type.
setPredictionProvider(String) - Method in class org.orekit.files.ilrs.CRDHeader: Set the prediction provider.
setPredictionType(int) - Method in class org.orekit.files.ilrs.CRDHeader: Set the prediction type.
setPressSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Set the pressure sensor manufacturer.
setPressSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Set the pressure sensor model.
setPressSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Set the pressure sensor serial number.
setPressure(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Set the local pressure at the evaluation location
setPrevId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set identification of previous orbit determination.
setPreviousMessageEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the creation date of previous message from a given originator.
setPreviousMessageID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the unique ID identifying previous message from a given originator.
setPrf(double) - Method in class org.orekit.files.ilrs.CPFHeader: Set the Pulse Repetition Frequency (PRF).
setPrimaryWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Set the primary wavelength.
setPrmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the Unique identifier of Pointing Request Message linked to this Orbit Data Message.
setPRN(int) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Setter for the PRN number of the satellite.
setPRN(int) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Setter for the PRN number of the satellite.
setProcessingSoftwares(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Set the processing softwares.
setProcessingSoftwareVersions(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Set the processing software versions.
setProductionEpoch(DateComponents) - Method in class org.orekit.files.ilrs.ILRSHeader: Set the date component of the ephemeris production.
setProductionHour(int) - Method in class org.orekit.files.ilrs.ILRSHeader: Set the hour of ephemeris production.
setProgramName(String) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the program name.
setProgramName(String) - Method in class org.orekit.gnss.navigation.RinexNavigation: Setter for the program name.
setProxy(Proxy.Type, String, int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient: Set proxy parameters.
setPulseEnergy(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Set the pulse energy.
setPulseInOutgoingSemiTrain(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Set the number of pulses in outgoing semi-train.
setPulseWidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Set the pulse width.
setQ(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion: Set quaternion component.
setQDot(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion: Set quaternion derivative component.
setQualityIndicator(int) - Method in class org.orekit.files.ilrs.CRDHeader: Set the data quality indicator.
setQuantumEfficiency(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the quantum efficiency at applicable wavelength.
setQzssCodeOnL2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data: Set the QZSS code on L2.
setQzssFitInterval(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data: Set the QZSS fit interval.
setQzssNavigationMessage(QZSSNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data: Set the QZSS navigation message.
setQzssToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data: Set the QZSS time of clock.
setRaan(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Set the orbit right ascension of ascending node.
setRangeMode(RangeMode) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the rangeMode.
setRangeType(int) - Method in class org.orekit.files.ilrs.CRDHeader: Set the range type indicator.
setRangeUnits(RangeUnits) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the rangeUnits.
setRateFrameIsA(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Set the frame in which rates are specified.
setRateFrameIsA(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler: Set the frame in which rates are specified.
setRawCoefficients(boolean, double[][], double[][], String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Deprecated.
as of 11.1, replaced by PotentialCoefficientsReader.setRawCoefficients(boolean, Flattener, double[], double[], String)
setRawCoefficients(boolean, Flattener, double[], double[], String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the tesseral-sectorial coefficients matrix.
setRawCorrectionRange(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the raw correction for range.
setRawRangeModulus(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the raw range modulus.
setRcs(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the typical (50th percentile) radar cross-section.
setRdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the Unique identifier of Reentry Data Message linked to this Orbit Data Message.
setReadComplete(boolean) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the indicator for completed read.
setReceiveBand(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the receiveBand.
setReceiveDelays(Map<Integer, Double>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the receiveDelays.
setRecommendedOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set sime span of observation recommended for the OD of the object.
setReconnectParameters(double, double, int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient: Set Reconnect parameters.
setReductionTheory(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set reduction theory used for precession and nutation modeling.
setReferenceDate(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver: Set reference date.
setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance: Set the reference frame in which data are given.
setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata: Set the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).
setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver: Set Coordinate system for velocity increment vector.
setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Set the reference frame in which data are given: used for RADEC tracking data.
setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester: Set up reference state.
setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester: Set up reference state.
setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper: Set up reference state.
setReferenceState(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester: Set up reference state.
setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester: Set up reference state.
setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper: Set up reference state.
setReferenceTrajectories(Propagator[]) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Setter for the reference trajectories.
setReferenceValue(double) - Method in class org.orekit.utils.ParameterDriver: Set reference parameter value.
setRefFrame(Frame) - Method in class org.orekit.files.ilrs.CPFHeader: Set the reference frame.
setRefFrameId(int) - Method in class org.orekit.files.ilrs.CPFHeader: Set the reference frame identifier.
setRefFrameString(String) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver: Set Coordinate system for the torque vector, for absolute frames.
setReflectivity(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the typical (50th percentile) coefficient of reflectivity.
setRemainingDv(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the total ΔV remaining for spacecraft.
setResetAtEnd(boolean) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Allow/disallow resetting the initial state at end of propagation.
setResetAtEnd(boolean) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Allow/disallow resetting the initial state at end of propagation.
setRevAtEpoch(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Set the revolution rumber.
setRolloverReference(DateComponents) - Static method in class org.orekit.time.GNSSDate: Set a reference date for ensuring continuity across GNSS week rollover.
setRotationalAngleType(int) - Method in class org.orekit.files.ilrs.CPFHeader: Set the rotation angle type.
setRotationAngle(char, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler: Set the Euler angle about (rad).
setRotationRate(char, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler: Set the rate of Euler angle (rad/s).
setSatConfiguration(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Sets the satellite configuration.
setSatelliteID(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData: Set the satellite ID.
setSatelliteID(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData: Set the satellite ID.
setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Override the default value of the parameter.
setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Override the default value of the parameter.
setSatelliteSystem(SatelliteSystem) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the satellite system.
setSatelliteSystem(SatelliteSystem) - Method in class org.orekit.gnss.navigation.RinexNavigation: Setter for the satellite system.
setScale(double) - Method in class org.orekit.utils.ParameterDriver: Set scale.
setSclkOffsetAtEpoch(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the spacecraft clock count at OcmMetadata.getEpochT0().
setSclkSecPerSISec(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the number of spacecraft clock seconds occurring during one SI second.
setSecondsOfWeek(double) - Method in class org.orekit.files.sp3.SP3: Set the seconds of the GPS week for this SP3 file.
setSecularVariationCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField: Set the given secular variation coefficients.
setSelected(boolean) - Method in class org.orekit.utils.ParameterDriver: Configure a parameter selection status.
setSelectedCoefficients(Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Set the selected short periodic coefficients that must be stored as additional states.
setSelectedCoefficients(Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Set the selected short periodic coefficients that must be stored as additional states.
setSensors(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set description of sensors used.
setSensorsN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set number of sensors used.
setSequenceNumber(int) - Method in class org.orekit.files.ilrs.ILRSHeader: Set the ephemeris sequence number.
setShadowBodies(List<BodyFacade>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set celestial bodies casting shadows.
setShadowModel(ShadowModel) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set shadow model used for solar radiation pressure.
setShortPeriodJacobians(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper: Deprecated.
as of 11.1, replaced by DSSTJacobiansMapper.setReferenceState(SpacecraftState)
setShortPeriodTerms(List<ShortPeriodTerms>) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Override the default value short periodic terms.
setSic(String) - Method in class org.orekit.files.ilrs.ILRSHeader: Set the SIC ID.
setSigma(double[]) - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter: Set the current value of sigma.
setSisa(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Setter for the signal in space accuracy.
setSiteCode(String) - Method in class org.orekit.files.sinex.Station: Set the site code (station identifier).
setSma(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Setter for the semi-major axis.
setSnm(double[][]) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data: Set the sine parameters of spherical harmonics expansion of degree N and order M.
setSoftwareId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Set the software configuration ID.
setSoftwareRecord(CRDConfiguration.SoftwareConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Set the software configuration record.
setSolarRadArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters: Set the solar radiation pressure area.
setSolarRadCoeff(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters: Get the solar radiation pressure coefficient.
setSolidTidesModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set solid tides model.
setSolveN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set number of solved-for states.
setSolveStates(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set description of state elements solved-for.
setSource(String) - Method in class org.orekit.files.ilrs.CPFHeader: Set the ephemeris source.
setSource(String) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Sets the source of this GPS almanac.
setSource(String) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac: Sets the source of this GPS almanac.
setSpacecraftClockAndDriftApplied(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Set the spacecraft clock offset and drift applied indicator.
setSpacecraftEpochTimeScale(int) - Method in class org.orekit.files.ilrs.CRDHeader: Set the spacecraft epoch time scale.
setSpaceWeatherEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set epoch of the Space Weather data.
setSpaceWeatherSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set Space Weather data source.
setSpatialFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the spatial filter.
setSpectralFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the spectral filter.
setSphericalHarmonicsDegree(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data: Set the degree of spherical harmonic expansion.
setSphericalHarmonicsOrder(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data: Set the order of spherical harmonic expansion.
setSpinAlpha(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Set the right ascension of spin axis vector (rad).
setSpinAngle(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Set the phase of the satellite about the spin axis (rad).
setSpinAngleVel(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Set the angular velocity of satellite around spin axis (rad/s).
setSpinDelta(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Set the declination of the spin axis vector (rad).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Setter for the Square Root of Semi-Major Axis (m^1/2).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac: Sets the Square Root of Semi-Major Axis (m^1/2).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Setter for the Square Root of Semi-Major Axis (m^1/2).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSAlmanac: Setter for the Square Root of Semi-Major Axis (m^1/2).
setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac: Setter for the Square Root of Semi-Major Axis (m^1/2).
setSrpCoefficient(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the nominal SRP coefficient.
setSrpConstantArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the attitude-independent SRP area, not already into attitude-dependent area along OEB.
setSrpModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Set Solar Radiation Pressure model.
setSrpUncertainty(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the SRP coefficient 1σ uncertainty.
setSsrEpoch1s(double) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader: Set the SSR Epoch Time 1s.
setSsrMultipleMessageIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader: Set the SSR Multiple Message Indicator.
setSsrProviderId(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader: Set the SSR Provider ID.
setSsrSolutionId(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader: Set the SSR Solution ID.
setSsrUpdateInterval(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader: Set the SSR Update Interval.
setSsrUra(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data: Set the SSR User Range Accuracy (URA).
setStartDate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator: Set a start date.
setStartDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator: Set a start date.
setStartEpoch(AbsoluteDate) - Method in class org.orekit.files.ilrs.ILRSHeader: Set the staring epoch (UTC).
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Set start of total time span covered by attitude data.
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the time of the earliest data contained in the OCM.
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata: Set start of total time span covered by ephemerides data and covariance data.
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the startTime.
setStateDerivatives(int, double[]...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Set the partial derivatives of the simulated measurement with respect to state Cartesian coordinates.
setStationClockAndDriftApplied(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Set the station clock offset and drift applied indicator.
setStationIdentifier(String) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the station identifier.
setStationName(String) - Method in class org.orekit.files.ilrs.CRDHeader: Set the station name from official list.
setStationName(String) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the station name.
setStationNetword(String) - Method in class org.orekit.files.ilrs.CRDHeader: Set the station network.
setStationOscDrift(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Set the estimated station oscillator drift in parts in 10¹⁵.
setStationUTCOffset(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Set the estimated station UTC offset.
setStatus(EstimatedMeasurement.Status) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Set the status.
setStep(int) - Method in class org.orekit.files.ilrs.CPFHeader: Set the time between table entries.
setStepHandler(T, FieldOrekitFixedStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator: Set a single handler for fixed stepsizes.
setStepHandler(FieldOrekitStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator: Set a single handler for variable stepsizes.
setStepHandler(double, OrekitFixedStepHandler) - Method in interface org.orekit.propagation.Propagator: Set a single handler for fixed stepsizes.
setStepHandler(OrekitStepHandler) - Method in interface org.orekit.propagation.Propagator: Set a single handler for variable stepsizes.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Set end of total time span covered by attitude data.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the time of the latest data contained in the OCM.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata: Set end of total time span covered by ephemerides data and covariance data.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the stopTime.
setSubDailySequenceNumber(int) - Method in class org.orekit.files.ilrs.CPFHeader: Set the sub-daily ephemeris sequence number.
setSupportedNames(String) - Method in class org.orekit.data.AbstractSelfFeedingLoader: Set the supported names regular expression.
setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage: Setter for the user SV accuracy.
setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage: Setter for the user SV accuracy.
setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage: Setter for the user SV accuracy.
setSvHealth(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data: Set the satellite health status.
setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Setter for the SV health status.
setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage: Setter for the satellite health status.
setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage: Setter for the satellite health status.
setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage: Setter for the satellite health status.
setSVN(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Sets the "SVN" reference number.
setSystemId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration: Set the system configuration ID.
setSystemIdentifier(int) - Method in class org.orekit.files.ilrs.CRDHeader: Set the system identifier.
setSystemNumber(int) - Method in class org.orekit.files.ilrs.CRDHeader: Set the system number.
setSystemOccupancy(int) - Method in class org.orekit.files.ilrs.CRDHeader: Set the system occupancy.
setSystemRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Set the system configuration record.
setTaimutcT0(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the difference (TAI – UTC) in seconds at epoch OcmMetadata.getEpochT0().
setTargetClass(int) - Method in class org.orekit.files.ilrs.ILRSHeader: Set the target class.
setTargetLocation(int) - Method in class org.orekit.files.ilrs.ILRSHeader: Set the target location.
setTauC(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the GLONASS time scale correction to UTC time.
setTauGps(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the correction to GPS time relative to GLONASS time.
setTauN(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Setter for the SV clock bias.
setTdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the Unique identifier of Tracking Data Message linked to this Orbit Data Message.
setTechAddress(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the address of Technical Point Of Contact at originator.
setTechOrg(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the creating agency or operator.
setTechPhone(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the phone number of Technical Point Of Contact at originator.
setTechPOC(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the Technical Point Of Contact at originator.
setTechPosition(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the position of Technical Point Of Contact at originator.
setTemperature(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Set the local temperature at the evaluation location
setTempSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Set the temperature sensor manufacturer.
setTempSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Set the temperature sensor model.
setTempSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Set the temperature sensor serial number.
setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage: Setter for the Group Delay Differential (s).
setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage: Setter for the Group Delay Differential (s).
setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage: Setter for the Group Delay Differential (s).
setTGD1(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage: Setter for the B1/B3 Group Delay Differential (s).
setTGD2(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage: Setter for the B2/B3 Group Delay Differential (s).
setThrust(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set thrust component.
setThrustDirectionSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set one σ angular off-nominal thrust direction.
setThrustEfficiency(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set thrust efficiency η.
setThrustInterpolation(OnOff) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set interpolation mode between current and next thrust line.
setThrustIsp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set thrust specific impulse.
setThrustMagnitudeSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver: Set one σ percent error on thrust magnitude.
setTideSystem(TideSystem) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Set the TideSystem used in the gravity field.
setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Setter for the reference time of the orbit as a duration from week start.
setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Setter for the message frame time.
setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Setter for the reference time of the SBAS orbit in GPS seconds of the week.
setTimeout(int) - Method in class org.orekit.data.NetworkCrawler: Set the timeout for connection.
setTimeout(int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient: Set timeout for connections and reads.
setTimer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration: Set the timer name.
setTimerSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration: Set the timer serial number.
setTimeScale(TimeScale) - Method in class org.orekit.files.ilrs.CPF: Set the time scale.
setTimeScale(TimeScale) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the data time scale.
setTimeSinceFirstObservation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set time elapsed between first accepted observation on epoch.
setTimeSinceLastObservation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set time elapsed between last accepted observation on epoch.
setTimeSource(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration: Set the time source.
setTimeSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the span of time in seconds that the OCM covers.
setTimeSystem(TimeSystem) - Method in class org.orekit.files.ccsds.section.Metadata: Set the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.
setTimeSystem(TimeSystem) - Method in class org.orekit.files.sp3.SP3: Set the time system used in this SP3 file.
setTimeSystem(TimeSystem) - Method in class org.orekit.gnss.clock.RinexClock: Setter for the file time system.
setTimetagRef(TimetagReference) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the timetagRef.
setTimingRecord(CRDConfiguration.TimingSystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Set the timing system configuration record.
setTk(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Set the time referenced to the beginning of the frame within the current day.
setTorque(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver: Set the torque vector (N.m).
setTrackId(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the tracking data identifier.
setTrackingSoftwares(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Set the tracking softwares.
setTrackingSoftwareVersions(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Set the tracking software versions.
setTracksAvailable(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set number of sensors tracks available for the OD within the actual OD span.
setTracksUsed(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set number of sensors tracks accepted for the OD within the actual OD span.
setTrajBasis(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set basis of this trajectory state time history data.
setTrajBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set identification number of the orbit determination or simulation upon which this trajectory is based.
setTrajFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set epoch of the trajectory reference frame.
setTrajID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set trajectory identification number.
setTrajNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set identification number of next trajectory.
setTrajPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set identification number of previous trajectory.
setTrajReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set reference frame of the trajectory.
setTrajType(ElementsType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set trajectory element set type.
setTrajUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set trajectory element set units.
setTransmissionOfSpectralFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Set the percentage of transmission of spectral filter.
setTransmitBand(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the transmitBand.
setTransmitDelays(Map<Integer, Double>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the transmitDelays.
setTranspClkRef(double) - Method in class org.orekit.files.ilrs.CPFHeader: Set the transponder Clock Reference Time.
setTranspClkRefTime(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Set the transponder clock reference time.
setTransponderId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Set the transponder configuration ID.
setTransponderRecord(CRDConfiguration.TransponderConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Set the transponder configuration record.
setTranspOscDrift(double) - Method in class org.orekit.files.ilrs.CPFHeader: Set the transponder Oscillator Drift in parts.
setTranspOscDrift(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Set the estimated transponder oscillator drift in parts in 10¹⁵.
setTranspTransmitDelay(double) - Method in class org.orekit.files.ilrs.CPFHeader: Set the transponder transmit delay.
setTranspUtcOffset(double) - Method in class org.orekit.files.ilrs.CPFHeader: Set the transponder UTC offset.
setTranspUTCOffset(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Set the estimated transponder UTC offset.
setTurnaroundDenominator(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the turnaroundDenominator.
setTurnaroundNumerator(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Setter for the turnaroundNumerator.
setTypAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.
setType(SP3.SP3FileType) - Method in class org.orekit.files.sp3.SP3: Set the file type for this SP3 file.
setUpEventDetector(ODEIntegrator, EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Wrap an Orekit event detector and register it to the integrator.
setUpEventDetector(FieldODEIntegrator<T>, FieldEventDetector<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Wrap an Orekit event detector and register it to the integrator.
setupMatricesComputation(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.AbstractPropagator: Set up computation of State Transition Matrix and Jacobians matrix with respect to parameters.
setupMatricesComputation(String, RealMatrix, DoubleArrayDictionary) - Method in interface org.orekit.propagation.Propagator: Set up computation of State Transition Matrix and Jacobians matrix with respect to parameters.
setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set up State Transition Matrix and Jacobian matrix handling.
setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.numerical.NumericalPropagator: Set up State Transition Matrix and Jacobian matrix handling.
setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Set up State Transition Matrix and Jacobian matrix handling.
setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set up all user defined event detectors.
setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Set up all user defined event detectors.
setURA(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Sets the average URA number.
setURA(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage: Setter for the user range accuracy.
setURA(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Setter for the user range accuracy.
setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Set start of useable time span covered by attitude data.
setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata: Set start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Set end of useable time span covered by ephemerides data.
setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Set end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata: Set end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
setUt1mutcT0(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Set the difference (UT1 – UTC) in seconds at epoch OcmMetadata.getEpochT0().
setV(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector: Set velocity component.
setValidFrom(AbsoluteDate) - Method in class org.orekit.files.sinex.Station: Set the start of validity.
setValidUntil(AbsoluteDate) - Method in class org.orekit.files.sinex.Station: Set the end of validity.
setValue(double) - Method in class org.orekit.utils.ParameterDriver: Set parameter value.
setVelocity(Vector3D) - Method in class org.orekit.files.sinex.Station: Set the station velocity.
setVersion(int) - Method in class org.orekit.files.ilrs.ILRSHeader: Set the format version.
setVmAbsolute(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the typical (50th percentile) visual magnitude.
setVmApparent(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the typical (50th percentile) apparent visual magnitude.
setVmApparentMax(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the maximum apparent visual magnitude.
setVmApparentMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the minimum apparent visual magnitude.
setVtecQualityIndicator(double) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header: Set the VTEC quality indicator.
setWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration: Set the transmit wavelength.
setWeek(int) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Setter for the reference week of the orbit.
setWeightedRms(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Set weighted RMS residual ratio.
setWetMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties: Set the total mass at T₀.
setX(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Setter for the satellite X position.
setXDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Setter for the satellite X velocity.
setXDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Setter for the satellite X acceleration.
setY(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Setter for the satellite Y position.
setYawAngle(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data: Set the yaw angle used for computation of phase wind-up correction.
setYawRate(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data: Set the yaw rate.
setYDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Setter for the satellite Y velocity.
setYDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Setter for the satellite Y acceleration.
setYearOfCentury(int) - Method in class org.orekit.files.ilrs.CRDHeader: Set the year of century from CPF or TLE.
setZ(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Setter for the satellite Z position.
setZDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Setter for the satellite Z velocity.
setZDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Setter for the satellite Z acceleration.
SGP - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE: Identifier for SGP type of ephemeris.
SGP - Static variable in class org.orekit.propagation.analytical.tle.TLE: Identifier for SGP type of ephemeris.
SGP4 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE: Identifier for SGP4 type of ephemeris.
SGP4 - Class in org.orekit.propagation.analytical.tle: This class contains methods to compute propagated coordinates with the SGP4 model.
SGP4(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.SGP4: Constructor for a unique initial TLE.
SGP4(TLE, AttitudeProvider, double, Frame) - Constructor for class org.orekit.propagation.analytical.tle.SGP4: Constructor for a unique initial TLE.
SGP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE: Identifier for SGP4 type of ephemeris.
SGP8 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE: Identifier for SGP8 type of ephemeris.
SGP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE: Identifier for SGP8 type of ephemeris.
SGP_SGP4_THEORY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata: Constant for SGP/SGP4 mean elements theory.
ShadowModel - Enum in org.orekit.files.ccsds.ndm.odm.ocm: Shadow model for solar radiation pressure.
shapiroCorrection(TimeStampedPVCoordinates, TimeStampedPVCoordinates) - Method in class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier: Compute Shapiro path dilation between two points in a gravity field.
ShapiroInterSatellitePhaseModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical inter-satellites phase measurement with Shapiro time delay.
ShapiroInterSatellitePhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier: Simple constructor.
ShapiroInterSatelliteRangeModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical range measurement with Shapiro time delay.
ShapiroInterSatelliteRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier: Simple constructor.
ShapiroOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical one-way GNSS phase measurement with Shapiro time delay.
ShapiroOneWayGNSSPhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier: Simple constructor.
ShapiroOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical range measurement with Shapiro time delay.
ShapiroOneWayGNSSRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier: Simple constructor.
ShapiroPhaseModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical phase measurement with Shapiro time delay.
ShapiroPhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier: Simple constructor.
ShapiroRangeModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical range measurement with Shapiro time delay.
ShapiroRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier: Simple constructor.
shiftedBy(double) - Method in class org.orekit.attitudes.Attitude: Get a time-shifted attitude.
shiftedBy(double) - Method in class org.orekit.attitudes.FieldAttitude: Get a time-shifted attitude.
shiftedBy(T) - Method in class org.orekit.attitudes.FieldAttitude: Get a time-shifted attitude.
shiftedBy(double) - Method in class org.orekit.frames.FieldTransform: Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.frames.FieldTransform: Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.frames.Transform: Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.orbits.CartesianOrbit: Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.CircularOrbit: Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.EquinoctialOrbit: Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.FieldCartesianOrbit: Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.orbits.FieldCartesianOrbit: Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.FieldCircularOrbit: Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.orbits.FieldCircularOrbit: Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get a time-shifted orbit.
shiftedBy(T) - Method in class org.orekit.orbits.FieldOrbit: Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.KeplerianOrbit: Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.Orbit: Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.propagation.FieldSpacecraftState: Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.propagation.FieldSpacecraftState: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.propagation.SpacecraftState: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.time.AbsoluteDate: Get a time-shifted date.
shiftedBy(T) - Method in class org.orekit.time.FieldAbsoluteDate: Get a time-shifted date.
shiftedBy(double) - Method in class org.orekit.time.FieldAbsoluteDate: Get a time-shifted date.
shiftedBy(double) - Method in interface org.orekit.time.FieldTimeShiftable: Get a time-shifted instance.
shiftedBy(KK) - Method in interface org.orekit.time.FieldTimeShiftable: Get a time-shifted instance.
shiftedBy(double) - Method in interface org.orekit.time.TimeShiftable: Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.utils.AbsolutePVCoordinates: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.AngularCoordinates: Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldAngularCoordinates: Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.FieldAngularCoordinates: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldPVCoordinates: Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.FieldPVCoordinates: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.PVCoordinates: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedAngularCoordinates: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates: Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates: Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates: Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedPVCoordinates: Get a time-shifted state.
ShiftingTransformProvider - Class in org.orekit.frames: Transform provider using thread-safe shifts on transforms sample.
ShiftingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double) - Constructor for class org.orekit.frames.ShiftingTransformProvider: Simple constructor.
SHM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for SHM files.
SHMFormatReader - Class in org.orekit.forces.gravity.potential: Reader for the SHM gravity field format.
SHMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader: Simple constructor.
SHMFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader: Simple constructor.
SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Name of the prefix for short period coefficients keys.
SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Name of the prefix for short period coefficients keys.
SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Name of the prefix for short period coefficients keys.
ShortPeriodicsInterpolatedCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities: Interpolated short periodics coefficients.
ShortPeriodicsInterpolatedCoefficient(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient: Simple constructor.
ShortPeriodTerms - Interface in org.orekit.propagation.semianalytical.dsst.forces: Additive short period terms contributing to the mean to osculating orbit mapping.
sign(double) - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod: Return the symbol of parameter a.
SignalCode - Enum in org.orekit.gnss: Enumerate for satellite signal code.
SignalInSpaceAccuracy - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris.utils: Signal-In-Space Accuracy (SISA).
SignalInSpaceAccuracy(int) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.SignalInSpaceAccuracy: Simple constructor.
signalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement: Compute propagation delay on a link leg (typically downlink or uplink).
signalTimeOfFlight(TimeStampedFieldPVCoordinates<T>, FieldVector3D<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement: Compute propagation delay on a link leg (typically downlink or uplink).
signedAmplitude(SpacecraftState, double[]) - Method in interface org.orekit.forces.empirical.AccelerationModel: Compute the signed amplitude of the acceleration.
signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.empirical.AccelerationModel: Compute the signed amplitude of the acceleration.
signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel: Compute the signed amplitude of the acceleration.
signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel: Compute the signed amplitude of the acceleration.
signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel: Compute the signed amplitude of the acceleration.
signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel: Compute the signed amplitude of the acceleration.
SignSemantic - Enum in org.orekit.estimation.measurements.generation: Enumerate for the semantic of the g function sign during measurements generation.
SimpleExponentialAtmosphere - Class in org.orekit.models.earth.atmosphere: Simple exponential atmospheric model.
SimpleExponentialAtmosphere(BodyShape, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere: Create an exponential atmosphere.
SimpleRatioAmbiguityAcceptance - Class in org.orekit.estimation.measurements.gnss: Ambiguity acceptance test based on a ratio of the two best candidates.
SimpleRatioAmbiguityAcceptance(double) - Constructor for class org.orekit.estimation.measurements.gnss.SimpleRatioAmbiguityAcceptance: Simple constructor.
SimpleTimeStampedTableParser<T extends TimeStamped> - Class in org.orekit.data: Parser for simple tables containing time stamped data.
SimpleTimeStampedTableParser(int, SimpleTimeStampedTableParser.RowConverter<T>) - Constructor for class org.orekit.data.SimpleTimeStampedTableParser: Simple constructor.
SimpleTimeStampedTableParser.RowConverter<S extends TimeStamped> - Interface in org.orekit.data: Interface for converting a table row into time-stamped data.
SinexLoader - Class in org.orekit.files.sinex: Loader for Solution INdependent EXchange (SINEX) files.
SinexLoader(String) - Constructor for class org.orekit.files.sinex.SinexLoader: Simple constructor.
SinexLoader(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.files.sinex.SinexLoader: Construct a loader by specifying the source of SINEX auxiliary data files.
SinexLoader(DataSource) - Constructor for class org.orekit.files.sinex.SinexLoader: Simple constructor.
SinexLoader(DataSource, TimeScale) - Constructor for class org.orekit.files.sinex.SinexLoader: Loads SINEX from the given input stream using the specified auxiliary data.
SingleBodyAbsoluteAttraction - Class in org.orekit.forces.gravity: Body attraction force model computed as absolute acceleration towards a body.
SingleBodyAbsoluteAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction: Simple constructor.
SingleBodyRelativeAttraction - Class in org.orekit.forces.gravity: Body attraction force model computed as relative acceleration towards frame center.
SingleBodyRelativeAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.SingleBodyRelativeAttraction: Simple constructor.
SingleLayerModelMappingFunction - Class in org.orekit.models.earth.ionosphere: Single Layer Model (SLM) ionospheric mapping function.
SingleLayerModelMappingFunction() - Constructor for class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction: Constructor with default value.
SingleLayerModelMappingFunction(double) - Constructor for class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction: Constructor.
sini0 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: sinus original inclination.
sini0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: sinus original inclination.
siToCcsdsName(String) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator: Convert a SI unit name to a CCSDS name.
siToCcsdsName(String) - Method in interface org.orekit.files.ccsds.utils.generation.Generator: Convert a SI unit name to a CCSDS name.
siToRaw(RangeUnitsConverter, TdmMetadata, AbsoluteDate, double) - Method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType: Convert a measurement from SI units.
size() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry: Get the size of the value array.
size() - Method in class org.orekit.utils.DoubleArrayDictionary: Get the number of dictionary entries.
size() - Method in class org.orekit.utils.FieldArrayDictionary.Entry: Get the size of the value array.
size() - Method in class org.orekit.utils.FieldArrayDictionary: Get the number of dictionary entries.
SM_COEFFICIENTS - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Identifier for sMm coefficients.
SmallManeuverAnalyticalModel - Class in org.orekit.forces.maneuvers: Analytical model for small maneuvers.
SmallManeuverAnalyticalModel(SpacecraftState, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Build a maneuver defined in spacecraft frame.
SmallManeuverAnalyticalModel(SpacecraftState, Frame, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Build a maneuver defined in user-specified frame.
SmoothFieldOfView - Class in org.orekit.geometry.fov: Class representing a spacecraft sensor Field Of View with shape defined by a smooth single loop.
SmoothFieldOfView(Vector3D, Vector3D, double) - Constructor for class org.orekit.geometry.fov.SmoothFieldOfView: Build a new instance.
SoftwareConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
SOLAR_FLUX_UNIT - Static variable in class org.orekit.utils.units.Unit: Solar Flux Unit.
SOLAR_SYSTEM_BARYCENTER - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for solar system barycenter.
SolarRadiationPressure - Class in org.orekit.forces.radiation: Solar radiation pressure force model.
SolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure: Simple constructor with default reference values.
SolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure: Complete constructor.
SolidTides - Class in org.orekit.forces.gravity: Solid tides force model.
SolidTides(Frame, double, double, TideSystem, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides: Simple constructor.
SolidTides(Frame, double, double, TideSystem, boolean, double, int, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides: Simple constructor.
solveILS(int, double[], int[], RealMatrix) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Find the best solutions to an Integer Least Square problem.
solveILS(int, double[], int[], RealMatrix) - Method in interface org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolver: Find the best solutions to an Integer Least Square problem.
sort() - Method in class org.orekit.utils.ParameterDriversList: Sort the parameters lexicographically.
SourceTable - Class in org.orekit.gnss.metric.ntrip: Source table for ntrip streams retrieval.
SOUTH_POLE - Static variable in class org.orekit.bodies.GeodeticPoint: South pole.
SP3 - Class in org.orekit.files.sp3: Represents a parsed SP3 orbit file.
SP3(double, int, Function<? super String, ? extends Frame>) - Constructor for class org.orekit.files.sp3.SP3: Create a new SP3 file object.
SP3.SP3Coordinate - Class in org.orekit.files.sp3: A single record of position clock and possibly derivatives in an SP3 file.
SP3.SP3Ephemeris - Class in org.orekit.files.sp3: An ephemeris for a single satellite in a SP3 file.
SP3.SP3FileType - Enum in org.orekit.files.sp3: File type indicator.
SP3.SP3OrbitType - Enum in org.orekit.files.sp3: Orbit type indicator.
SP3_FRAME_CENTER_STRING - Static variable in class org.orekit.files.sp3.SP3: String representation of the center of ephemeris coordinate system.
SP3Coordinate(AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.files.sp3.SP3.SP3Coordinate: Create a coordinate with only position.
SP3Coordinate(AbsoluteDate, Vector3D, Vector3D, double, double) - Constructor for class org.orekit.files.sp3.SP3.SP3Coordinate: Create a coordinate with position and velocity.
SP3Ephemeris(String) - Constructor for class org.orekit.files.sp3.SP3.SP3Ephemeris: Create an ephemeris for a single satellite.
SP3Parser - Class in org.orekit.files.sp3: A parser for the SP3 orbit file format.
SP3Parser() - Constructor for class org.orekit.files.sp3.SP3Parser: Create an SP3 parser using default values.
SP3Parser(double, int, Function<? super String, ? extends Frame>) - Constructor for class org.orekit.files.sp3.SP3Parser: Create an SP3 parser and specify the extra information needed to create a Propagator from the ephemeris data.
SP3Parser(double, int, Function<? super String, ? extends Frame>, TimeScales) - Constructor for class org.orekit.files.sp3.SP3Parser: Create an SP3 parser and specify the extra information needed to create a Propagator from the ephemeris data.
SpacecraftBodyFrame - Class in org.orekit.files.ccsds.definitions: Frames used in CCSDS Attitude Data Messages for the spacecraft body.
SpacecraftBodyFrame(SpacecraftBodyFrame.BaseEquipment, String) - Constructor for class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame: Simple constructor.
SpacecraftBodyFrame.BaseEquipment - Enum in org.orekit.files.ccsds.definitions: Equipment on which the frame is located.
SpacecraftParameters - Class in org.orekit.files.ccsds.ndm.adm.apm: Container for spacecraft parameters data.
SpacecraftParameters() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters: Simple constructor.
SpacecraftParameters - Class in org.orekit.files.ccsds.ndm.odm: Container for spacecraft parameters.
SpacecraftParameters() - Constructor for class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters: Create an empty state data set.
SpacecraftParametersKey - Enum in org.orekit.files.ccsds.ndm.adm.apm: Keys for APM spacecraft parameters entries.
SpacecraftParametersKey - Enum in org.orekit.files.ccsds.ndm.odm: Keys for ODM spacecraft parameters entries.
SpacecraftParametersWriter - Class in org.orekit.files.ccsds.ndm.odm: Writer for spacecraft parameters data.
SpacecraftParametersWriter(String, String, SpacecraftParameters) - Constructor for class org.orekit.files.ccsds.ndm.odm.SpacecraftParametersWriter: Create a writer.
SpacecraftState - Class in org.orekit.propagation: This class is the representation of a complete state holding orbit, attitude and mass information at a given date.
SpacecraftState(Orbit) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from orbit only.
SpacecraftState(Orbit, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from orbit and attitude.
SpacecraftState(Orbit, double) - Constructor for class org.orekit.propagation.SpacecraftState: Create a new instance from orbit and mass.
SpacecraftState(Orbit, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from orbit, attitude and mass.
SpacecraftState(Orbit, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState: Deprecated.
as of 11.1, replaced by SpacecraftState.SpacecraftState(Orbit, DoubleArrayDictionary)
SpacecraftState(Orbit, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from orbit and additional states.
SpacecraftState(Orbit, Attitude, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState: Deprecated.
as of 11.1, replaced by SpacecraftState.SpacecraftState(Orbit, Attitude, DoubleArrayDictionary)
SpacecraftState(Orbit, Attitude, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from orbit, attitude and additional states.
SpacecraftState(Orbit, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState: Deprecated.
as of 11.1, replaced by SpacecraftState.SpacecraftState(Orbit, double, DoubleArrayDictionary)
SpacecraftState(Orbit, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState: Create a new instance from orbit, mass and additional states.
SpacecraftState(Orbit, Attitude, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState: Deprecated.
as of 11.1, replaced by SpacecraftState.SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary)
SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from orbit, attitude, mass and additional states.
SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from orbit, attitude, mass, additional states and derivatives.
SpacecraftState(AbsolutePVCoordinates) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from position-velocity-acceleration only.
SpacecraftState(AbsolutePVCoordinates, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from position-velocity-acceleration and attitude.
SpacecraftState(AbsolutePVCoordinates, double) - Constructor for class org.orekit.propagation.SpacecraftState: Create a new instance from position-velocity-acceleration and mass.
SpacecraftState(AbsolutePVCoordinates, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from position-velocity-acceleration, attitude and mass.
SpacecraftState(AbsolutePVCoordinates, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState: Deprecated.
as of 11.1, replaced by SpacecraftState.SpacecraftState(AbsolutePVCoordinates, DoubleArrayDictionary)
SpacecraftState(AbsolutePVCoordinates, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from position-velocity-acceleration and additional states.
SpacecraftState(AbsolutePVCoordinates, Attitude, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState: Deprecated.
as of 11.1, replaced by SpacecraftState.SpacecraftState(AbsolutePVCoordinates, Attitude, DoubleArrayDictionary)
SpacecraftState(AbsolutePVCoordinates, Attitude, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from position-velocity-acceleration, attitude and additional states.
SpacecraftState(AbsolutePVCoordinates, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState: Deprecated.
as of 11.1, replaced by SpacecraftState.SpacecraftState(AbsolutePVCoordinates, double, DoubleArrayDictionary)
SpacecraftState(AbsolutePVCoordinates, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState: Create a new instance from position-velocity-acceleration, mass and additional states.
SpacecraftState(AbsolutePVCoordinates, Attitude, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState: Deprecated.
as of 11.1, replaced by SpacecraftState.SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary)
SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from position-velocity-acceleration, attitude, mass and additional states.
SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState: Build a spacecraft state from position-velocity-acceleration, attitude, mass and additional states and derivatives.
SPEED_OF_LIGHT - Static variable in interface org.orekit.utils.Constants: Speed of light: 299792458.0 m/s.
SphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential: Interface used to provide spherical harmonics coefficients.
SpinStabilized - Class in org.orekit.attitudes: This class handles a spin stabilized attitude provider.
SpinStabilized(AttitudeProvider, AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.attitudes.SpinStabilized: Creates a new instance.
SpinStabilized - Class in org.orekit.files.ccsds.ndm.adm.apm: Container for Attitude Parameter Message data lines.
SpinStabilized() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Simple constructor.
SpinStabilizedKey - Enum in org.orekit.files.ccsds.ndm.adm.apm: Keys for APM spin-stabilized entries.
sqrt(String) - Method in class org.orekit.utils.units.Unit: Create root of unit.
SSA - Static variable in class org.orekit.models.earth.displacement.Tide: Ssa tide.
SsrData - Class in org.orekit.gnss.metric.messages.ssr: Container for common data in SSR message data.
SsrData() - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrData
SsrHeader - Class in org.orekit.gnss.metric.messages.ssr: Container for common data in SSR messages header.
SsrHeader() - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrHeader
SsrIgm01 - Class in org.orekit.gnss.metric.messages.ssr.igm: GNSS SSR Orbit Correction Message.
SsrIgm01(int, SatelliteSystem, SsrIgm01Header, List<SsrIgm01Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01: Constructor.
SsrIgm01Data - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for SSR IGM01 data.
SsrIgm01Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data: Constructor.
SsrIgm01Header - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for SSR IGM01 header.
SsrIgm01Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header: Constructor.
SsrIgm02 - Class in org.orekit.gnss.metric.messages.ssr.igm: GNSS SSR Clock Correction Message.
SsrIgm02(int, SatelliteSystem, SsrIgm02Header, List<SsrIgm02Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02: Constructor.
SsrIgm02Data - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for SSR IGM02 data.
SsrIgm02Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data: Constructor.
SsrIgm02Header - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for SSR IGM02 header.
SsrIgm02Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Header: Constructor.
SsrIgm03 - Class in org.orekit.gnss.metric.messages.ssr.igm: GNSS SSR Combined Orbit and Clock Correction Message.
SsrIgm03(int, SatelliteSystem, SsrIgm03Header, List<SsrIgm03Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03: Constructor.
SsrIgm03Data - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for SSR IGM03 data.
SsrIgm03Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data: Constructor.
SsrIgm03Header - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for SSR IGM03 header.
SsrIgm03Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header: Constructor.
SsrIgm04 - Class in org.orekit.gnss.metric.messages.ssr.igm: GNSS SSR High Rate Clock Correction Message.
SsrIgm04(int, SatelliteSystem, SsrIgm04Header, List<SsrIgm04Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04: Constructor.
SsrIgm04Data - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for SSR IGM04 data.
SsrIgm04Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data: Constructor.
SsrIgm04Header - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for SSR IGM04 header.
SsrIgm04Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Header: Constructor.
SsrIgm05 - Class in org.orekit.gnss.metric.messages.ssr.igm: GNSS SSR Code Bias Message.
SsrIgm05(int, SatelliteSystem, SsrIgm05Header, List<SsrIgm05Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05: Constructor.
SsrIgm05Data - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for SSR IGM05 data.
SsrIgm05Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data: Constructor.
SsrIgm05Header - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for SSR IGM05 header.
SsrIgm05Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Header: Constructor.
SsrIgm06 - Class in org.orekit.gnss.metric.messages.ssr.igm: GNSS SSR Phase Bias Message.
SsrIgm06(int, SatelliteSystem, SsrIgm06Header, List<SsrIgm06Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06: Constructor.
SsrIgm06Data - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for SSR IGM06 data.
SsrIgm06Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data: Constructor.
SsrIgm06Header - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for SSR IGM06 header.
SsrIgm06Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header: Constructor.
SsrIgm07 - Class in org.orekit.gnss.metric.messages.ssr.igm: GNSS SSR SSR URA Message.
SsrIgm07(int, SatelliteSystem, SsrIgm07Header, List<SsrIgm07Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07: Constructor.
SsrIgm07Data - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for SSR IGM07 data.
SsrIgm07Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data: Constructor.
SsrIgm07Header - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for SSR IGM07 header.
SsrIgm07Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Header: Constructor.
SsrIgmData - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for common data in IGS Generic SSR Message type.
SsrIgmData() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData: Constructor.
SsrIgmHeader - Class in org.orekit.gnss.metric.messages.ssr.igm: Container for common data in IGS Generic SSR Message type header.
SsrIgmHeader() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader: Constructor.
SsrIgmMessage<H extends SsrIgmHeader,D extends SsrIgmData> - Class in org.orekit.gnss.metric.messages.ssr.igm: The IGS Generic SSR Message types provide elements to calculate GNSS satellite corrections.
SsrIgmMessage(int, SatelliteSystem, H, List<D>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmMessage: Constructor.
SsrIm201 - Class in org.orekit.gnss.metric.messages.ssr.subtype: SSR Ionosphere VTEC Spherical Harmonics Message.
SsrIm201(int, SsrIm201Header, List<SsrIm201Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201: Constructor.
SsrIm201Data - Class in org.orekit.gnss.metric.messages.ssr.subtype: Container for SSR IM201 data.
SsrIm201Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data: Constructor.
SsrIm201Header - Class in org.orekit.gnss.metric.messages.ssr.subtype: Container for SSR IM201 header.
SsrIm201Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header: Constructor.
SsrMessage<H extends SsrHeader,D extends SsrData> - Class in org.orekit.gnss.metric.messages.ssr: Base class for SSR messages.
SsrMessage(int, H, List<D>) - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrMessage: Constructor.
SsrVtecIonosphericModel - Class in org.orekit.models.earth.ionosphere: Ionospheric model based on SSR IM201 message.
SsrVtecIonosphericModel(SsrIm201) - Constructor for class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel: Constructor.
STANDARD_ATM_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: NIST standard atmospheric pressure (Pa).
STANDARD_ATM_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: NIST standard atmospheric temperature (K).
STANDARDIZED_LOCALE - Static variable in class org.orekit.utils.AccurateFormatter: Standardized locale to use, to ensure files can be exchanged without internationalization issues.
start() - Method in class org.orekit.gnss.metric.parser.AbstractEncodedMessages: Start message extraction.
start() - Method in class org.orekit.gnss.metric.parser.ByteArrayEncodedMessages: Start message extraction.
start() - Method in interface org.orekit.gnss.metric.parser.EncodedMessage: Start message extraction.
START_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector: Default suffix for start driver.
START_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector: Default suffix for start driver.
started(TaskEvent) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
startMessage(String, String, double) - Method in interface org.orekit.files.ccsds.utils.generation.Generator: Start CCSDS message.
startMessage(String, String, double) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator: Start CCSDS message.
startMessage(String, String, double) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator: Start CCSDS message.
startParse(String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Start parsing.
StartStopEventsTrigger<A extends AbstractDetector<A>,O extends AbstractDetector<O>> - Class in org.orekit.forces.maneuvers.trigger: Maneuver triggers based on a pair of event detectors that defines firing start and stop.
StartStopEventsTrigger(A, O) - Constructor for class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger: Simple constructor.
startStreaming(String, Type, boolean, boolean) - Method in class org.orekit.gnss.metric.ntrip.NtripClient: Connect to a mount point and start streaming data from it.
STATE_DIMENSION - Static variable in class org.orekit.propagation.AbstractMatricesHarvester: State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.analytical.tle.TLEJacobiansMapper: State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.integration.AbstractJacobiansMapper: State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.numerical.AbsoluteJacobiansMapper: State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.numerical.JacobiansMapper: State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper: State dimension, fixed to 6.
stateChanged(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator: Notify about a state change.
stateChanged(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator: Notify about a state change.
StateFunction - Interface in org.orekit.utils: Interface representing a vector function depending on SpacecraftState.
StateJacobian - Interface in org.orekit.utils: Interface representing the Jacobian of a vector function depending on SpacecraftState.
StateMapper - Class in org.orekit.propagation.integration: This class maps between raw double elements and SpacecraftState instances.
StateMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.StateMapper: Simple constructor.
stateToTLE(FieldSpacecraftState<T>, FieldTLE<T>) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE: Convert Spacecraft State into TLE.
stateToTLE(FieldSpacecraftState<T>, FieldTLE<T>, TimeScale, Frame) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE: Convert Spacecraft State into TLE.
stateToTLE(FieldSpacecraftState<T>, FieldTLE<T>, TimeScale, Frame, double, int) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE: Convert Spacecraft State into TLE.
stateToTLE(SpacecraftState, TLE) - Static method in class org.orekit.propagation.analytical.tle.TLE: Convert Spacecraft State into TLE.
stateToTLE(SpacecraftState, TLE, TimeScale, Frame) - Static method in class org.orekit.propagation.analytical.tle.TLE: Convert Spacecraft State into TLE.
stateToTLE(SpacecraftState, TLE, TimeScale, Frame, double, int) - Static method in class org.orekit.propagation.analytical.tle.TLE: Convert Spacecraft State into TLE.
StateVector - Class in org.orekit.files.ccsds.ndm.odm: Container for state vector data.
StateVector() - Constructor for class org.orekit.files.ccsds.ndm.odm.StateVector: Create an empty data set.
StateVectorKey - Enum in org.orekit.files.ccsds.ndm.odm: Keys for ODM state vector container entries.
StateVectorWriter - Class in org.orekit.files.ccsds.ndm.odm: Writer for state vector data.
StateVectorWriter(String, String, StateVector, TimeConverter) - Constructor for class org.orekit.files.ccsds.ndm.odm.StateVectorWriter: Create a writer.
Station - Class in org.orekit.files.sinex: Station model.
Station() - Constructor for class org.orekit.files.sinex.Station: Constructor.
Station.ReferenceSystem - Enum in org.orekit.files.sinex: Eccentricity reference system.
StationDisplacement - Interface in org.orekit.models.earth.displacement: Interface for computing reference points displacement.
stec(AbsoluteDate, GeodeticPoint, GeodeticPoint) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel: This method allows the computation of the Stant Total Electron Content (STEC).
stec(FieldAbsoluteDate<T>, FieldGeodeticPoint<T>, FieldGeodeticPoint<T>) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel: This method allows the computation of the Stant Total Electron Content (STEC).
StepHandlerMultiplexer - Class in org.orekit.propagation.sampling: This class gathers several OrekitStepHandler instances into one.
StepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.StepHandlerMultiplexer: Simple constructor.
stillAcceptsData() - Method in interface org.orekit.data.DataLoader: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.gnss.RinexObservationLoader.Parser: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.gnss.SEMParser
stillAcceptsData() - Method in class org.orekit.gnss.YUMAParser
stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.GeoMagneticModelLoader: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader: Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
stillAcceptsData() - Method in class org.orekit.utils.InterpolationTableLoader: Check if the loader still accepts new data.
STMEquations - Class in org.orekit.propagation.numerical.cr3bp: Class calculating the state transition matrix coefficient for CR3BP Computation.
STMEquations(CR3BPSystem) - Constructor for class org.orekit.propagation.numerical.cr3bp.STMEquations: Simple constructor.
STOP_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector: Default suffix for stop driver.
STOP_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector: Default suffix for stop driver.
stopMonitoring() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor: Stop monitoring.
StopOnDecreasing<T extends EventDetector> - Class in org.orekit.propagation.events.handlers: Handle a detection event and choose what to do next.
StopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnDecreasing
StopOnEvent<T extends EventDetector> - Class in org.orekit.propagation.events.handlers: Event handler which will always return stop as a state.
StopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.StopOnEvent
StopOnIncreasing<T extends EventDetector> - Class in org.orekit.propagation.events.handlers: Handle a detection event and choose what to do next.
StopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnIncreasing
stopStreaming(int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient: Stop streaming data from all connected mount points.
StreamedMessage - Class in org.orekit.gnss.metric.ntrip: Container for streamed messages meta-data.
StreamingAemWriter - Class in org.orekit.files.ccsds.ndm.adm.aem: A writer for AEM files.
StreamingAemWriter(Generator, AemWriter, Header, AemMetadata) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter: Simple constructor.
StreamingAemWriter.SegmentWriter - Class in org.orekit.files.ccsds.ndm.adm.aem: A writer for a segment of an AEM.
StreamingCpfWriter - Class in org.orekit.files.ilrs: A writer for CPF files.
StreamingCpfWriter(Appendable, TimeScale, CPFHeader) - Constructor for class org.orekit.files.ilrs.StreamingCpfWriter: Create a CPF writer than streams data to the given output stream.
StreamingCpfWriter.HeaderLineWriter - Enum in org.orekit.files.ilrs: Writer for specific header lines.
StreamingCpfWriter.Segment - Class in org.orekit.files.ilrs: A writer for a segment of a CPF.
StreamingOemWriter - Class in org.orekit.files.ccsds.ndm.odm.oem: A writer for OEM files.
StreamingOemWriter(Generator, OemWriter, Header, OemMetadata) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter: Simple constructor.
StreamingOemWriter.SegmentWriter - Class in org.orekit.files.ccsds.ndm.odm.oem: A writer for a segment of an OEM.
StreamMonitor - Class in org.orekit.gnss.metric.ntrip: Monitor for retrieving streamed data from one mount point.
StreamMonitor(NtripClient, String, Type, boolean, boolean, double, double, int) - Constructor for class org.orekit.gnss.metric.ntrip.StreamMonitor: Build a monitor for streaming data from a mount point.
stringValue(EncodedMessage, int) - Method in interface org.orekit.gnss.metric.parser.DataField: Get the value of the field as a String.
subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates: Subtract an offset from the instance.
subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates: Subtract an offset from the instance.
subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates: Subtract an offset from the instance.
subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates: Subtract an offset from the instance.
SUN - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Sun.
SUN_RADIUS - Static variable in interface org.orekit.utils.Constants: Sun radius: 695500000 m.
SUPPORTED_NAMES - Static variable in class org.orekit.frames.ITRFVersionLoader: Regular expression for supported files names.
supportsTimeTransform() - Method in class org.orekit.models.earth.GeoMagneticField: Indicates whether this model supports time transformation or not.
switchOccurred(AttitudeProvider, AttitudeProvider, SpacecraftState) - Method in interface org.orekit.attitudes.AttitudesSequence.SwitchHandler: Method called when attitude is switched from one law to another law.
sxpInitialize(T[]) - Method in class org.orekit.propagation.analytical.tle.FieldSGP4: Initialization proper to each propagator (SGP or SDP).
sxpInitialize(T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Initialization proper to each propagator (SGP or SDP).
sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.SGP4: Initialization proper to each propagator (SGP or SDP).
sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Initialization proper to each propagator (SGP or SDP).
sxpPropagate(T, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldSGP4: Propagation proper to each propagator (SGP or SDP).
sxpPropagate(T, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Propagation proper to each propagator (SGP or SDP).
sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.SGP4: Propagation proper to each propagator (SGP or SDP).
sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Propagation proper to each propagator (SGP or SDP).
SystemConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration

T

t2cof - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: 3/2 * C1.
t2cof - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: 3/2 * C1.
TabulatedLofOffset - Class in org.orekit.attitudes: This class handles an attitude provider interpolating from a predefined table containing offsets from a Local Orbital Frame.
TabulatedLofOffset(Frame, LOFType, List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter) - Constructor for class org.orekit.attitudes.TabulatedLofOffset: Creates new instance.
TabulatedLofOffset(Frame, LOFType, List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.attitudes.TabulatedLofOffset: Creates new instance.
TabulatedProvider - Class in org.orekit.attitudes: This class handles an attitude provider interpolating from a predefined table.
TabulatedProvider(Frame, List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter) - Constructor for class org.orekit.attitudes.TabulatedProvider: Creates new instance.
TabulatedProvider(List<? extends TimeStampedAngularCoordinates>, int, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate, AttitudeBuilder) - Constructor for class org.orekit.attitudes.TabulatedProvider: Creates new instance.
TAIScale - Class in org.orekit.time: International Atomic Time.
TAIUTCDatFilesLoader - Class in org.orekit.time: Loader for UTC-TAI extracted from tai-utc.dat file from USNO.
TAIUTCDatFilesLoader(String) - Constructor for class org.orekit.time.TAIUTCDatFilesLoader: Build a loader for tai-utc.dat file from USNO.
TAIUTCDatFilesLoader(String, DataProvidersManager) - Constructor for class org.orekit.time.TAIUTCDatFilesLoader: Build a loader for tai-utc.dat file from USNO.
TAIUTCDatFilesLoader.Parser - Class in org.orekit.time: Internal class performing the parsing.
TargetPointing - Class in org.orekit.attitudes: This class handles target pointing attitude provider.
TargetPointing(Frame, Frame, Vector3D) - Constructor for class org.orekit.attitudes.TargetPointing: Creates a new instance from body frame and target expressed in Cartesian coordinates.
TargetPointing(Frame, GeodeticPoint, BodyShape) - Constructor for class org.orekit.attitudes.TargetPointing: Creates a new instance from body shape and target expressed in geodetic coordinates.
TCBScale - Class in org.orekit.time: Barycentric Coordinate Time.
TCGScale - Class in org.orekit.time: Geocentric Coordinate Time.
TDBScale - Class in org.orekit.time: Barycentric Dynamic Time.
Tdm - Class in org.orekit.files.ccsds.ndm.tdm: This class stores all the information of the CCSDS Tracking Data Message parsed by TDMParser or TDMXMLParser.
Tdm(Header, List<Segment<TdmMetadata, ObservationsBlock>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.tdm.Tdm: Simple constructor.
TdmDataKey - Enum in org.orekit.files.ccsds.ndm.tdm: Keys for TDM observations entries, except the measurements themselves.
TdmMetadata - Class in org.orekit.files.ccsds.ndm.tdm: The TDMMetadata class gathers the meta-data present in the Tracking Data Message (TDM).
TdmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Create a new TDM meta-data.
TdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.tdm: Keys for TDM container entries.
TdmParser - Class in org.orekit.files.ccsds.ndm.tdm: Class for CCSDS Tracking Data Message parsers.
TdmParser(IERSConventions, boolean, DataContext, ParsedUnitsBehavior, RangeUnitsConverter) - Constructor for class org.orekit.files.ccsds.ndm.tdm.TdmParser: Complete constructor.
TdmWriter - Class in org.orekit.files.ccsds.ndm.tdm: Writer for CCSDS Tracking Data Message.
TdmWriter(IERSConventions, DataContext, RangeUnitsConverter) - Constructor for class org.orekit.files.ccsds.ndm.tdm.TdmWriter: Complete constructor.
TESLA - Static variable in class org.orekit.utils.units.Unit: tesla unit.
tessellate(SphericalPolygonsSet, double, double, double, double, boolean, boolean) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator: Tessellate a zone of interest into tiles.
THDT - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularAzEl: Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularRaDec: Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase: Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase: Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSRange: Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.Phase: Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.InterSatellitesRange: Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement: Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Position: Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.PV: Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Range: Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.RangeRate: Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.TurnAroundRange: Estimate the theoretical value.
theoryIsSgpSdp() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata: Check if mean element theory in SGP or SDP.
theta2 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: cos io squared.
theta2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: cos io squared.
ThirdBodyAttraction - Class in org.orekit.forces.gravity: Third body attraction force model.
ThirdBodyAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.ThirdBodyAttraction: Simple constructor.
ThirdBodyAttractionEpoch - Class in org.orekit.forces.gravity: Third body attraction force model.
ThirdBodyAttractionEpoch(CelestialBody) - Constructor for class org.orekit.forces.gravity.ThirdBodyAttractionEpoch: Simple constructor.
ThreeEighthesIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for ThreeEighthesIntegrator.
ThreeEighthesIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder: Build a new instance.
THRUST - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Parameter name for thrust.
THRUST_SCALE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Thrust scaling factor.
ThrustDirectionAndAttitudeProvider - Class in org.orekit.forces.maneuvers.propulsion: This class is used in to both manage the attitude of the satellite and the direction of thrust.
ThrustDirectionProvider - Interface in org.orekit.forces.maneuvers.propulsion: Interface to compute the thrust direction of a maneuver.
ThrustPropulsionModel - Interface in org.orekit.forces.maneuvers.propulsion: Interface for a thrust-based propulsion model.
THRUSTX_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel: Parameter name for the scale factor on the X component of the thrust in S/C frame.
THRUSTY_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel: Parameter name for the scale factor on the Y component of the thrust in S/C frame.
THRUSTZ_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel: Parameter name for the scale factor on the Z component of the thrust in S/C frame.
TidalDisplacement - Class in org.orekit.models.earth.displacement: Modeling of displacement of reference points due to tidal effects.
TidalDisplacement(double, double, double, PVCoordinatesProvider, PVCoordinatesProvider, IERSConventions, boolean) - Constructor for class org.orekit.models.earth.displacement.TidalDisplacement: Simple constructor.
Tide - Class in org.orekit.models.earth.displacement: Class representing a tide.
Tide(int, int, int, int, int, int) - Constructor for class org.orekit.models.earth.displacement.Tide: Simple constructor.
Tide(int) - Constructor for class org.orekit.models.earth.displacement.Tide: Simple constructor.
TideSystem - Enum in org.orekit.forces.gravity.potential: Enumerate for tie systems.
TideSystemProvider - Interface in org.orekit.forces.gravity.potential: Interface used to provide tide systems.
Tile - Class in org.orekit.models.earth.tessellation: Simple data structure for a quadrilateral tile shape on a body surface.
Tile(GeodeticPoint, GeodeticPoint, GeodeticPoint, GeodeticPoint) - Constructor for class org.orekit.models.earth.tessellation.Tile: Create a tile.
TileAiming - Interface in org.orekit.models.earth.tessellation: Interface defining the aiming direction of tiles.
TimeComponents - Class in org.orekit.time: Class representing a time within the day broken up as hour, minute and second components.
TimeComponents(int, int, double) - Constructor for class org.orekit.time.TimeComponents: Build a time from its clock elements.
TimeComponents(int, int, double, int) - Constructor for class org.orekit.time.TimeComponents: Build a time from its clock elements.
TimeComponents(double) - Constructor for class org.orekit.time.TimeComponents: Build a time from the second number within the day.
TimeComponents(int, double) - Constructor for class org.orekit.time.TimeComponents: Build a time from the second number within the day.
TimeConverter - Class in org.orekit.files.ccsds.definitions: Dates reader/writer.
TimeConverter(TimeScale, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.definitions.TimeConverter: Build a time system.
TimeDerivativesEquations - Interface in org.orekit.propagation.numerical: Interface summing up the contribution of several forces into orbit and mass derivatives.
TimeInterpolable<T extends TimeInterpolable<T>> - Interface in org.orekit.time: This interface represents objects that can be interpolated in time.
TimeScalarFunction - Interface in org.orekit.time: This interface represents a scalar function of time.
TimeScale - Interface in org.orekit.time: Interface for time scales.
TimeScales - Interface in org.orekit.time: A collection of TimeScales.
TimeScalesFactory - Class in org.orekit.time: Factory for predefined time scales.
timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.AbsoluteDate: Compute the offset between two time scales at the current instant.
timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate: Compute the offset between two time scales at the current instant.
TimeShiftable<T extends TimeShiftable<T>> - Interface in org.orekit.time: This interface represents objects that can be shifted in time.
TimeSpanDragForce - Class in org.orekit.forces.drag: Time span atmospheric drag force model.
TimeSpanDragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.TimeSpanDragForce: Constructor with default UTC time scale for the default names of the drag parameter drivers.
TimeSpanDragForce(Atmosphere, DragSensitive, TimeScale) - Constructor for class org.orekit.forces.drag.TimeSpanDragForce: Constructor.
TimeSpanEstimatedTroposphericModel - Class in org.orekit.models.earth.troposphere: Time span estimated tropospheric model.
TimeSpanEstimatedTroposphericModel(EstimatedTroposphericModel) - Constructor for class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel: Constructor with default UTC time scale.
TimeSpanEstimatedTroposphericModel(EstimatedTroposphericModel, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel: Constructor with default UTC time scale.
TimeSpanMap<T> - Class in org.orekit.utils: Container for objects that apply to spans of time.
TimeSpanMap(T) - Constructor for class org.orekit.utils.TimeSpanMap: Create a map containing a single object, initially valid throughout the timeline.
TimeSpanMap.Span<S> - Class in org.orekit.utils: Holder for one time span.
TimeSpanMap.Transition<S> - Class in org.orekit.utils: Class holding transition times.
TimeSpanParametricAcceleration - Class in org.orekit.forces.empirical: Time span parametric acceleration model.
TimeSpanParametricAcceleration(Vector3D, boolean, AccelerationModel) - Constructor for class org.orekit.forces.empirical.TimeSpanParametricAcceleration: Simple constructor.
TimeSpanParametricAcceleration(Vector3D, AttitudeProvider, AccelerationModel) - Constructor for class org.orekit.forces.empirical.TimeSpanParametricAcceleration: Simple constructor.
TimeStamped - Interface in org.orekit.time: This interface represents objects that have a AbsoluteDate date attached to them.
TimeStampedAngularCoordinates - Class in org.orekit.utils: time-stamped version of AngularCoordinates.
TimeStampedAngularCoordinates(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates: Builds a rotation/rotation rate pair.
TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates: Build the rotation that transforms a pair of pv coordinates into another pair.
TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates: Build one of the rotations that transform one pv coordinates into another one.
TimeStampedAngularCoordinates(AbsoluteDate, FieldRotation) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates: Builds a TimeStampedAngularCoordinates from a FieldRotation<Derivative>.
TimeStampedCache<T extends TimeStamped> - Interface in org.orekit.utils: Interface for a data structure that can provide concurrent access to TimeStamped data surrounding a given date.
TimeStampedCacheException - Exception in org.orekit.errors: This class is the base class for all specific exceptions thrown by during the GenericTimeStampedCache.
TimeStampedCacheException(Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException: Simple constructor.
TimeStampedCacheException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException: Simple constructor.
TimeStampedCacheException(OrekitException) - Constructor for exception org.orekit.errors.TimeStampedCacheException: Simple constructor.
TimeStampedCacheException(MathRuntimeException) - Constructor for exception org.orekit.errors.TimeStampedCacheException: Simple constructor.
TimeStampedFieldAngularCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils: time-stamped version of FieldAngularCoordinates.
TimeStampedFieldAngularCoordinates(AbsoluteDate, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates: Build the rotation that transforms a pair of pv coordinates into another pair.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates: Build the rotation that transforms a pair of pv coordinates into another pair.
TimeStampedFieldAngularCoordinates(AbsoluteDate, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates: Builds a rotation/rotation rate pair.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates: Builds a rotation/rotation rate pair.
TimeStampedFieldAngularCoordinates(Field<T>, TimeStampedAngularCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates: Builds an instance for a regular TimeStampedAngularCoordinates.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldRotation) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates: Builds a TimeStampedFieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.
TimeStampedFieldPVCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils: time-stamped version of FieldPVCoordinates.
TimeStampedFieldPVCoordinates(AbsoluteDate, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Builds a PVCoordinates pair.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Builds a PVCoordinates pair.
TimeStampedFieldPVCoordinates(AbsoluteDate, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Basic constructor.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Basic constructor.
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Subtractive constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Subtractive constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldVector3D) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates: Builds a TimeStampedFieldPVCoordinates triplet from a FieldVector3D<FieldDerivativeStructure>.
TimeStampedGenerator<T extends TimeStamped> - Interface in org.orekit.utils: Generator to use for creating entries in time stamped caches.
TimeStampedPVCoordinates - Class in org.orekit.utils: time-stamped version of PVCoordinates.
TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates: Builds a TimeStampedPVCoordinates pair.
TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates: Build from position and velocity.
TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates: Build from position velocity acceleration coordinates.
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates: Multiplicative constructor
TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates: Subtractive constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates: Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates: Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates: Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, FieldVector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates: Builds a TimeStampedPVCoordinates triplet from a FieldVector3D<Derivative>.
TimeSystem - Enum in org.orekit.files.ccsds.definitions: The set of time systems defined in CCSDS standards (ADM, ODM, NDM).
TimeSystem - Enum in org.orekit.gnss: Enumerate for the time systems used in navigation files.
TimeSystemCorrection(String, double, double, int, int) - Constructor for class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection: Constructor.
TimetagReference - Enum in org.orekit.files.ccsds.ndm.tdm: Reference for time tag.
TimeVectorFunction - Interface in org.orekit.time: This interface represents a multi-valued function of time.
TimingSystemConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
tle - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Initial state.
TLE - Class in org.orekit.propagation.analytical.tle: This class is a container for a single set of TLE data.
TLE(String, String) - Constructor for class org.orekit.propagation.analytical.tle.TLE: Simple constructor from unparsed two lines.
TLE(String, String, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.TLE: Simple constructor from unparsed two lines using the given time scale as UTC.
TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double) - Constructor for class org.orekit.propagation.analytical.tle.TLE: Simple constructor from already parsed elements.
TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.TLE: Simple constructor from already parsed elements using the given time scale as UTC.
tle - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: Initial state.
TLEBatchLSModel - Class in org.orekit.estimation.leastsquares: Deprecated.
as of 11.1, replaced by BatchLSModel
TLEBatchLSModel(OrbitDeterminationPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Constructor for class org.orekit.estimation.leastsquares.TLEBatchLSModel: Deprecated.

Simple constructor.
TLEConstants - Class in org.orekit.propagation.analytical.tle: Constants necessary to TLE propagation.
TLEJacobiansMapper - Class in org.orekit.propagation.analytical.tle: Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
TLEJacobiansMapper(String, ParameterDriversList, TLEPropagator) - Constructor for class org.orekit.propagation.analytical.tle.TLEJacobiansMapper: Simple constructor.
TLEKalmanModel - Class in org.orekit.estimation.sequential: Deprecated.
as of 11.1, replaced by KalmanModel
TLEKalmanModel(List<OrbitDeterminationPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.TLEKalmanModel: Deprecated.

Kalman process model constructor (package private).
TLEPartialDerivativesEquations - Class in org.orekit.propagation.analytical.tle: Deprecated.
TLEPartialDerivativesEquations(String, TLEPropagator) - Constructor for class org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations: Deprecated.

Simple constructor.
TLEPropagator - Class in org.orekit.propagation.analytical.tle: This class provides elements to propagate TLE's.
TLEPropagator(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.TLEPropagator: Protected constructor for derived classes.
TLEPropagator(TLE, AttitudeProvider, double, Frame) - Constructor for class org.orekit.propagation.analytical.tle.TLEPropagator: Protected constructor for derived classes.
TLEPropagatorBuilder - Class in org.orekit.propagation.conversion: Builder for TLEPropagator.
TLEPropagatorBuilder(TLE, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder: Build a new instance.
TLEPropagatorBuilder(TLE, PositionAngle, double, DataContext) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder: Build a new instance.
TLEPropagatorBuilder(TLE, PositionAngle, double, double, int) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder: Build a new instance.
TLEPropagatorBuilder(TLE, PositionAngle, double, DataContext, double, int) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder: Build a new instance.
toAbsoluteDate() - Method in class org.orekit.time.FieldAbsoluteDate: Transform the FieldAbsoluteDate in an AbsoluteDate.
toAbsolutePVCoordinates() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates: Converts to an AbsolutePVCoordinates instance.
toAngularCoordinates() - Method in class org.orekit.utils.FieldAngularCoordinates: Convert to a regular angular coordinates.
toArray(List<List<Double>>) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Deprecated.
as of 11.1, not used anymore
toAttitude() - Method in class org.orekit.attitudes.FieldAttitude: Converts to an Attitude instance.
toCartesian(AbsoluteDate, double[], double) - Method in enum org.orekit.files.ccsds.definitions.ElementsType: Convert to Cartesian coordinates.
toCartesian(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState: Convert to Cartesian coordinates.
toDate(DateComponents) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Create a date from components.
toDate(DateComponents, TimeComponents) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Create a date from components.
toDate(TimeScale) - Method in class org.orekit.time.AbsoluteDate: Convert the instance to a Java Date.
toDate(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate: Convert the instance to a Java Date.
toDerivativeStructurePV(int) - Method in class org.orekit.utils.FieldPVCoordinates: Transform the instance to a FieldPVCoordinates<FieldDerivativeStructure>.
toDerivativeStructurePV(int) - Method in class org.orekit.utils.PVCoordinates: Transform the instance to a FieldPVCoordinates<DerivativeStructure>.
toDerivativeStructureRotation(int) - Method in class org.orekit.utils.AngularCoordinates: Transform the instance to a FieldRotation<DerivativeStructure>.
toDerivativeStructureRotation(int) - Method in class org.orekit.utils.FieldAngularCoordinates: Transform the instance to a FieldRotation<FieldDerivativeStructure>.
toDerivativeStructureVector(int) - Method in class org.orekit.utils.FieldPVCoordinates: Transform the instance to a FieldVector3D<FieldDerivativeStructure>.
toDerivativeStructureVector(int) - Method in class org.orekit.utils.PVCoordinates: Transform the instance to a FieldVector3D<DerivativeStructure>.
toEquinox(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter: Convert nutation corrections.
toFieldPVCoordinatesProvider(Field<T>) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider: Convert to a FieldPVCoordinatesProvider with a specific type.
toGeodetic(S2Point) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator: Convert a point on the unit 2-sphere to geodetic coordinates.
TokenType - Enum in org.orekit.files.ccsds.utils.lexical: Enumerate for tokens occurring during CCSDS file parsing.
tolerances(T, FieldOrbit<T>, OrbitType) - Static method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Estimate tolerance vectors for integrators.
tolerances(T, T, FieldOrbit<T>, OrbitType) - Static method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Estimate tolerance vectors for integrators when propagating in orbits.
tolerances(double, AbsolutePVCoordinates) - Static method in class org.orekit.propagation.numerical.NumericalPropagator: Estimate tolerance vectors for integrators when propagating in absolute position-velocity-acceleration.
tolerances(double, Orbit, OrbitType) - Static method in class org.orekit.propagation.numerical.NumericalPropagator: Estimate tolerance vectors for integrators when propagating in orbits.
tolerances(double, double, Orbit, OrbitType) - Static method in class org.orekit.propagation.numerical.NumericalPropagator: Estimate tolerance vectors for integrators when propagating in orbits.
tolerances(double, Orbit) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
tolerances(double, double, Orbit) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
tolerances(T, FieldOrbit<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
tolerances(T, T, FieldOrbit<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
toMap() - Method in class org.orekit.utils.DoubleArrayDictionary: Create a map from the instance.
toMap() - Method in class org.orekit.utils.FieldArrayDictionary: Create a map from the instance.
ton2a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext: 2 / (n² * a) .
ton2a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext: 2 / (n² * a) .
toNonRotating(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter: Convert nutation corrections.
toOrbit() - Method in class org.orekit.orbits.FieldCartesianOrbit
toOrbit() - Method in class org.orekit.orbits.FieldCircularOrbit: Transforms the FieldOrbit instance into an Orbit instance.
toOrbit() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Transforms the FieldOrbit instance into an Orbit instance.
toOrbit() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Transforms the FieldOrbit instance into an Orbit instance.
toOrbit() - Method in class org.orekit.orbits.FieldOrbit: Transforms the FieldOrbit instance into an Orbit instance.
toPlane(Vector3D) - Method in class org.orekit.bodies.Ellipse: Project a point to the ellipse plane.
TopocentricFrame - Class in org.orekit.frames: Topocentric frame.
TopocentricFrame(BodyShape, GeodeticPoint, String) - Constructor for class org.orekit.frames.TopocentricFrame: Simple constructor.
toPVCoordinates() - Method in class org.orekit.utils.FieldPVCoordinates: Convert to a constant position-velocity.
toSI(double) - Method in enum org.orekit.data.PolynomialParser.Unit: Convert value from instance unit to corresponding SI unit.
toSI(double) - Method in class org.orekit.utils.units.Unit: Convert a value to SI units.
toSI(Double) - Method in class org.orekit.utils.units.Unit: Convert a value to SI units.
toSpace(Vector2D) - Method in class org.orekit.bodies.Ellipse: Create a point from its ellipse-relative coordinates.
toSpacecraftState() - Method in class org.orekit.propagation.FieldSpacecraftState: To convert a FieldSpacecraftState instance into a SpacecraftState instance.
toString() - Method in class org.orekit.bodies.FieldGeodeticPoint
toString() - Method in class org.orekit.bodies.GeodeticPoint
toString() - Method in enum org.orekit.files.ccsds.definitions.ElementsType
toString() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame
toString() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
toString() - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
toString() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
toString() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory
toString() - Method in class org.orekit.frames.Frame: New definition of the java.util toString() method.
toString() - Method in class org.orekit.frames.OrphanFrame
toString() - Method in class org.orekit.gnss.metric.ntrip.GnssData
toString() - Method in enum org.orekit.gnss.metric.ntrip.NavigationSystem
toString() - Method in class org.orekit.models.earth.GeoMagneticElements
toString() - Method in class org.orekit.orbits.CartesianOrbit: Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.CircularOrbit: Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.EquinoctialOrbit: Returns a string representation of this equinoctial parameters object.
toString() - Method in class org.orekit.orbits.FieldCartesianOrbit: Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.FieldCircularOrbit: Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Returns a string representation of this equinoctial parameters object.
toString() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Returns a string representation of this Keplerian parameters object.
toString() - Method in class org.orekit.orbits.KeplerianOrbit: Returns a string representation of this Keplerian parameters object.
toString() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get a string representation of this TLE set.
toString() - Method in class org.orekit.propagation.analytical.tle.TLE: Get a string representation of this TLE set.
toString() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event
toString() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
toString() - Method in class org.orekit.propagation.FieldSpacecraftState
toString() - Method in class org.orekit.propagation.SpacecraftState
toString() - Method in class org.orekit.time.AbsoluteDate: Get a String representation of the instant location with up to 16 digits of precision for the seconds value.
toString(TimeScale) - Method in class org.orekit.time.AbsoluteDate: Get a String representation of the instant location in ISO-8601 format without the UTC offset and with up to 16 digits of precision for the seconds value.
toString(int) - Method in class org.orekit.time.AbsoluteDate: Get a String representation of the instant location for a local time.
toString(int, TimeScale) - Method in class org.orekit.time.AbsoluteDate: Get a String representation of the instant location for a local time.
toString(TimeZone) - Method in class org.orekit.time.AbsoluteDate: Get a String representation of the instant location for a time zone.
toString(TimeZone, TimeScale) - Method in class org.orekit.time.AbsoluteDate: Get a String representation of the instant location for a time zone.
toString() - Method in class org.orekit.time.BDTScale
toString() - Method in class org.orekit.time.DateComponents: Get a string representation (ISO-8601) of the date.
toString() - Method in class org.orekit.time.DateTimeComponents: Return a string representation of this pair.
toString(int) - Method in class org.orekit.time.DateTimeComponents: Return a string representation of this date-time, rounded to millisecond precision.
toString(int, int) - Method in class org.orekit.time.DateTimeComponents: Return a string representation of this date-time, rounded to the given precision.
toString() - Method in class org.orekit.time.FieldAbsoluteDate: Get a String representation of the instant location with up to 16 digits of precision for the seconds value.
toString(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate: Get a String representation of the instant location in ISO-8601 format without the UTC offset and with up to 16 digits of precision for the seconds value.
toString(int) - Method in class org.orekit.time.FieldAbsoluteDate: Get a String representation of the instant location for a local time.
toString(int, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate: Get a String representation of the instant location for a local time.
toString(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate: Get a String representation of the instant location for a time zone.
toString(TimeZone, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate: Get a String representation of the instant location for a time zone.
toString() - Method in class org.orekit.time.GalileoScale
toString() - Method in class org.orekit.time.GLONASSScale
toString() - Method in class org.orekit.time.GMSTScale
toString() - Method in class org.orekit.time.GPSScale
toString() - Method in class org.orekit.time.IRNSSScale
toString() - Method in class org.orekit.time.QZSSScale
toString() - Method in class org.orekit.time.SatelliteClockScale
toString() - Method in class org.orekit.time.TAIScale
toString() - Method in class org.orekit.time.TCBScale
toString() - Method in class org.orekit.time.TCGScale
toString() - Method in class org.orekit.time.TDBScale
toString() - Method in class org.orekit.time.TimeComponents: Get a string representation of the time including the offset from UTC.
toString() - Method in class org.orekit.time.TTScale
toString() - Method in class org.orekit.time.UT1Scale
toString() - Method in class org.orekit.time.UTCScale
toString() - Method in class org.orekit.utils.DoubleArrayDictionary: Get a string representation of the dictionary.
toString() - Method in class org.orekit.utils.FieldArrayDictionary: Get a string representation of the dictionary.
toString() - Method in class org.orekit.utils.FieldPVCoordinates: Return a string representation of this position/velocity pair.
toString() - Method in class org.orekit.utils.ImmutableTimeStampedCache
toString() - Method in class org.orekit.utils.ParameterDriver: Get a text representation of the parameter.
toString() - Method in class org.orekit.utils.PVCoordinates: Return a string representation of this position/velocity pair.
toString() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates: Return a string representation of this date, position, velocity, and acceleration.
toString(TimeScale) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates: Return a string representation of this date, position, velocity, and acceleration.
toString() - Method in class org.orekit.utils.TimeStampedPVCoordinates: Return a string representation of this date, position, velocity, and acceleration.
toString(TimeScale) - Method in class org.orekit.utils.TimeStampedPVCoordinates: Return a string representation of this date, position, velocity, and acceleration.
toString() - Method in class org.orekit.utils.units.Unit
toString() - Method in class org.orekit.utils.units.UnitsConverter
toStringRfc3339(TimeScale) - Method in class org.orekit.time.AbsoluteDate: Represent the given date as a string according to the format in RFC 3339.
toStringRfc3339() - Method in class org.orekit.time.DateTimeComponents: Represent the given date and time as a string according to the format in RFC 3339.
toStringWithoutUtcOffset(TimeScale, int) - Method in class org.orekit.time.AbsoluteDate: Return a string representation of this date-time, rounded to the given precision.
toStringWithoutUtcOffset() - Method in class org.orekit.time.DateTimeComponents: Get a string representation of the date-time without the offset from UTC.
toStringWithoutUtcOffset(int, int) - Method in class org.orekit.time.DateTimeComponents: Return a string representation of this date-time, rounded to the given precision.
toStringWithoutUtcOffset() - Method in class org.orekit.time.TimeComponents: Get a string representation of the time without the offset from UTC.
TOTAL_ELECTRON_CONTENT_UNIT - Static variable in class org.orekit.utils.units.Unit: Total Electron Content Unit.
TOTAL_ZENITH_DELAY - Static variable in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel: Name of the parameter of this model: the total zenith delay.
toTaylorProvider() - Method in class org.orekit.utils.AbsolutePVCoordinates: Create a local provider using simply Taylor expansion through AbsolutePVCoordinates.shiftedBy(double).
toTaylorProvider() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates: Create a local provider using simply Taylor expansion through FieldAbsolutePVCoordinates.shiftedBy(double).
toTaylorProvider(Frame) - Method in class org.orekit.utils.TimeStampedPVCoordinates: Create a local provider using simply Taylor expansion through TimeStampedPVCoordinates.shiftedBy(double).
toTimeStampedPVCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.StateVector: Convert to TimeStampedPVCoordinates.
toTimeStampedPVCoordinates() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates: Convert to a constant position-velocity.
toTLE() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Convert FieldTLE into TLE.
toTransform() - Method in class org.orekit.propagation.FieldSpacecraftState: Compute the transform from state defining frame to spacecraft frame.
toTransform() - Method in class org.orekit.propagation.SpacecraftState: Compute the transform from state defining frame to spacecraft frame.
toUnivariateDerivative1PV() - Method in class org.orekit.utils.FieldPVCoordinates: Transform the instance to a FieldPVCoordinates<FieldUnivariateDerivative1>.
toUnivariateDerivative1PV() - Method in class org.orekit.utils.PVCoordinates: Transform the instance to a FieldPVCoordinates<UnivariateDerivative1>.
toUnivariateDerivative1Rotation() - Method in class org.orekit.utils.AngularCoordinates: Transform the instance to a FieldRotation<UnivariateDerivative1>.
toUnivariateDerivative1Rotation() - Method in class org.orekit.utils.FieldAngularCoordinates: Transform the instance to a FieldRotation<UnivariateDerivative1>.
toUnivariateDerivative1Vector() - Method in class org.orekit.utils.FieldPVCoordinates: Transform the instance to a FieldVector3D<FieldUnivariateDerivative1>.
toUnivariateDerivative1Vector() - Method in class org.orekit.utils.PVCoordinates: Transform the instance to a FieldVector3D<UnivariateDerivative1>.
toUnivariateDerivative2PV() - Method in class org.orekit.utils.FieldPVCoordinates: Transform the instance to a FieldPVCoordinates<FieldUnivariateDerivative2>.
toUnivariateDerivative2PV() - Method in class org.orekit.utils.PVCoordinates: Transform the instance to a FieldPVCoordinates<UnivariateDerivative2>.
toUnivariateDerivative2Rotation() - Method in class org.orekit.utils.AngularCoordinates: Transform the instance to a FieldRotation<UnivariateDerivative2>.
toUnivariateDerivative2Rotation() - Method in class org.orekit.utils.FieldAngularCoordinates: Transform the instance to a FieldRotation<UnivariateDerivative2>.
toUnivariateDerivative2Vector() - Method in class org.orekit.utils.FieldPVCoordinates: Transform the instance to a FieldVector3D<FieldUnivariateDerivative2>.
toUnivariateDerivative2Vector() - Method in class org.orekit.utils.PVCoordinates: Transform the instance to a FieldVector3D<UnivariateDerivative2>.
TrackingMode - Enum in org.orekit.files.ccsds.ndm.tdm: Tracking mode.
TRAJ_LINE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm: Trajectory line element for XML messages.
TrajectoryState - Class in org.orekit.files.ccsds.ndm.odm.ocm: Trajectory state entry.
TrajectoryState(ElementsType, AbsoluteDate, String[], int, List<Unit>) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState: Simple constructor.
TrajectoryStateHistory - Class in org.orekit.files.ccsds.ndm.odm.ocm: Trajectory state history.
TrajectoryStateHistoryMetadata - Class in org.orekit.files.ccsds.ndm.odm.ocm: Metadata for trajectory state history.
TrajectoryStateHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm.ocm: Keys for rajectory state history container entries.
transform(Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape: Transform a Cartesian point to a surface-relative point.
transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape: Transform a Cartesian point to a surface-relative point.
transform(GeodeticPoint) - Method in interface org.orekit.bodies.BodyShape: Transform a surface-relative point to a Cartesian point.
transform(FieldGeodeticPoint<T>) - Method in interface org.orekit.bodies.BodyShape: Transform a surface-relative point to a Cartesian point.
transform(GeodeticPoint) - Method in class org.orekit.bodies.OneAxisEllipsoid: Transform a surface-relative point to a Cartesian point.
transform(FieldGeodeticPoint<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid: Transform a surface-relative point to a Cartesian point.
transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid: Transform a Cartesian point to a surface-relative point.
transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid: Transform a Cartesian point to a surface-relative point.
transform(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid: Transform a Cartesian point to a surface-relative point.
Transform - Class in org.orekit.frames: Transformation class in three dimensional space.
Transform(AbsoluteDate, Vector3D) - Constructor for class org.orekit.frames.Transform: Build a translation transform.
Transform(AbsoluteDate, Rotation) - Constructor for class org.orekit.frames.Transform: Build a rotation transform.
Transform(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform: Build a translation transform, with its first time derivative.
Transform(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform: Build a translation transform, with its first and second time derivatives.
Transform(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.frames.Transform: Build a translation transform, with its first time derivative.
Transform(AbsoluteDate, Rotation, Vector3D) - Constructor for class org.orekit.frames.Transform: Build a rotation transform.
Transform(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform: Build a rotation transform.
Transform(AbsoluteDate, AngularCoordinates) - Constructor for class org.orekit.frames.Transform: Build a rotation transform.
Transform(AbsoluteDate, Transform, Transform) - Constructor for class org.orekit.frames.Transform: Build a transform by combining two existing ones.
transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid: Transform a Cartesian point to a surface-relative point.
transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid: Transform a Cartesian point to a surface-relative point.
transform(GeodeticPoint) - Method in class org.orekit.models.earth.Geoid: Transform a surface-relative point to a Cartesian point.
transform(FieldGeodeticPoint<T>) - Method in class org.orekit.models.earth.Geoid: Transform a surface-relative point to a Cartesian point.
transformFromInertial(AbsoluteDate, PVCoordinates) - Method in enum org.orekit.frames.LOFType: Get the transform from an inertial frame defining position-velocity and the local orbital frame.
transformFromInertial(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType: Get the transform from an inertial frame defining position-velocity and the local orbital frame.
TransformGenerator - Class in org.orekit.frames: Generator to use transforms in GenericTimeStampedCache.
TransformGenerator(int, TransformProvider, double) - Constructor for class org.orekit.frames.TransformGenerator: simple constructor.
transformLine(Line) - Method in class org.orekit.frames.FieldTransform: Transform a line.
transformLine(FieldLine<T>) - Method in class org.orekit.frames.FieldTransform: Transform a line.
transformLine(Line) - Method in class org.orekit.frames.Transform: Transform a line.
transformModel(double) - Method in class org.orekit.models.earth.GeoMagneticField: Time transform the model coefficients from the base year of the model using secular variation coefficients.
transformModel(GeoMagneticField, double) - Method in class org.orekit.models.earth.GeoMagneticField: Time transform the model coefficients from the base year of the model using a linear interpolation with a second model.
transformPosition(Vector3D) - Method in class org.orekit.frames.FieldTransform: Transform a position vector (including translation effects).
transformPosition(FieldVector3D<T>) - Method in class org.orekit.frames.FieldTransform: Transform a position vector (including translation effects).
transformPosition(Vector3D) - Method in class org.orekit.frames.Transform: Transform a position vector (including translation effects).
transformPosition(FieldVector3D<T>) - Method in class org.orekit.frames.Transform: Transform a position vector (including translation effects).
TransformProvider - Interface in org.orekit.frames: Interface for Transform providers.
TransformProviderUtils - Class in org.orekit.frames: Utility for Transform providers.
transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.FieldTransform: Transform TimeStampedPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.FieldTransform: Transform TimeStampedPVCoordinates including kinematic effects.
transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.FieldTransform: Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.FieldTransform: Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.Transform: Transform PVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.Transform: Transform TimeStampedPVCoordinates including kinematic effects.
transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform: Transform FieldPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform: Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformVector(Vector3D) - Method in class org.orekit.frames.FieldTransform: Transform a vector (ignoring translation effects).
transformVector(FieldVector3D<T>) - Method in class org.orekit.frames.FieldTransform: Transform a vector (ignoring translation effects).
transformVector(Vector3D) - Method in class org.orekit.frames.Transform: Transform a vector (ignoring translation effects).
transformVector(FieldVector3D<T>) - Method in class org.orekit.frames.Transform: Transform a vector (ignoring translation effects).
TransponderConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
TriggerDate - Class in org.orekit.forces.maneuvers.jacobians: Generator for one column of a Jacobian matrix for special case of trigger dates.
TriggerDate(String, String, boolean, Maneuver, double) - Constructor for class org.orekit.forces.maneuvers.jacobians.TriggerDate: Simple constructor.
TroposphericGradientConverter - Class in org.orekit.estimation.measurements.modifiers: Converter for states and parameters arrays.
TroposphericGradientConverter(SpacecraftState, int, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.TroposphericGradientConverter: Simple constructor.
TroposphericModelUtils - Class in org.orekit.models.earth.troposphere: Utility class for tropospheric models.
TRUE_ANOM - Static variable in enum org.orekit.orbits.OrbitType: Name for mean anomaly.
TRUE_LAT_ARG - Static variable in enum org.orekit.orbits.OrbitType: Name for mean argument of latitude.
TRUE_LON_ARG - Static variable in enum org.orekit.orbits.OrbitType: Name for mean argument of longitude.
trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit: Computes the eccentric latitude argument from the true latitude argument.
trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit: Computes the eccentric longitude argument from the true longitude argument.
trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit: Computes the eccentric latitude argument from the true latitude argument.
trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit: Computes the eccentric longitude argument from the true longitude argument.
trueToEllipticEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit: Computes the elliptic eccentric anomaly from the true anomaly.
trueToEllipticEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit: Computes the elliptic eccentric anomaly from the true anomaly.
trueToHyperbolicEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit: Computes the hyperbolic eccentric anomaly from the true anomaly.
trueToHyperbolicEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit: Computes the hyperbolic eccentric anomaly from the true anomaly.
tryAdvance(SpacecraftState, OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState: Try to accept the current history up to the given time.
tryAdvance(FieldSpacecraftState<T>, FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState: Try to accept the current history up to the given time.
tsi - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: tsi from SPTRCK #3.
tsi - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: tsi from SPTRCK #3.
TTScale - Class in org.orekit.time: Terrestrial Time as defined by IAU(1991) recommendation IV.
TurnAroundRange - Class in org.orekit.estimation.measurements: Class modeling a turn-around range measurement using a primary ground station and a secondary ground station.
TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.TurnAroundRange: Simple constructor.
TurnAroundRangeBuilder - Class in org.orekit.estimation.measurements.generation: Builder for TurnAroundRange measurements.
TurnAroundRangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.TurnAroundRangeBuilder: Simple constructor.
TurnAroundRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical TurnAroundRange measurement with ionospheric delay.
TurnAroundRangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier: Constructor.
TurnAroundRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical turn-around TurnAroundRange measurement with tropospheric delay.
TurnAroundRangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier: Constructor.
TWO_THIRD - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: Constant 2.0 / 3.0.
TwoBodiesBaryFrame - Class in org.orekit.frames: Class creating the inertial barycenter frame from two bodies.
TwoBodiesBaryFrame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.TwoBodiesBaryFrame: Simple constructor.
Type - Enum in org.orekit.gnss.metric.ntrip: Enumerate for messages type.

U

unableToParseLine(Throwable) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader: Annotate an exception with the file context.
unFixAmbiguity(ParameterDriver) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver: Un-fix an integer ambiguity (typically after a phase cycle slip).
Unit - Class in org.orekit.utils.units: Basic handling of multiplicative units.
Unit(String, double, Fraction, Fraction, Fraction, Fraction, Fraction) - Constructor for class org.orekit.utils.units.Unit: Simple constructor.
Units - Class in org.orekit.files.ccsds.definitions: Units used in CCSDS messages.
UNITS - Static variable in class org.orekit.files.ccsds.utils.generation.XmlGenerator: Name of the units attribute.
Units - Class in org.orekit.gnss.metric.parser: Units used in RTCM and IGS SSR messages.
UnitsCache - Class in org.orekit.utils.units: Cache for parsed units.
UnitsCache() - Constructor for class org.orekit.utils.units.UnitsCache: Simple constructor.
UnitsConverter - Class in org.orekit.utils.units: Converter between units.
UnitsConverter(Unit, Unit) - Constructor for class org.orekit.utils.units.UnitsConverter: Simple constructor.
unitsListToString(List<Unit>) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator: Convert a list of units to a bracketed string.
unitsListToString(List<Unit>) - Method in interface org.orekit.files.ccsds.utils.generation.Generator: Convert a list of units to a bracketed string.
UnivariateProcessNoise - Class in org.orekit.estimation.sequential: Provider for a temporal evolution of the process noise matrix.
UnivariateProcessNoise(RealMatrix, LOFType, PositionAngle, UnivariateFunction[], UnivariateFunction[]) - Constructor for class org.orekit.estimation.sequential.UnivariateProcessNoise: Simple constructor.
UnivariateProcessNoise(RealMatrix, LOFType, PositionAngle, UnivariateFunction[], UnivariateFunction[], UnivariateFunction[]) - Constructor for class org.orekit.estimation.sequential.UnivariateProcessNoise: Simple constructor.
UnixCompressFilter - Class in org.orekit.data: Filter for Unix compressed data.
UnixCompressFilter() - Constructor for class org.orekit.data.UnixCompressFilter
UNKNOWN_OBJECT - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm: Default name for unknown object.
unmodifiableView() - Method in class org.orekit.utils.DoubleArrayDictionary: Get an unmodifiable view of the dictionary.
unmodifiableView() - Method in class org.orekit.utils.FieldArrayDictionary: Get an unmodifiable view of the dictionary.
UnnormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential: Interface used to provide un-normalized spherical harmonics coefficients.
UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential: Un-normalized spherical harmonics coefficients evaluated at a specific instant.
unwrap(MathRuntimeException) - Static method in exception org.orekit.errors.OrekitException: Recover a OrekitException, possibly embedded in a MathRuntimeException.
unwrap(OrekitException) - Static method in exception org.orekit.errors.TimeStampedCacheException: Recover a TimeStampedCacheException, possibly embedded in a OrekitException.
unwrap(MathRuntimeException) - Static method in exception org.orekit.errors.TimeStampedCacheException: Recover a TimeStampedCacheException, possibly embedded in a MathRuntimeException.
UpdatableFrame - Class in org.orekit.frames: Frame whose transform from its parent can be updated.
UpdatableFrame(Frame, Transform, String) - Constructor for class org.orekit.frames.UpdatableFrame: Build a non-inertial frame from its transform with respect to its parent.
UpdatableFrame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.UpdatableFrame: Build a frame from its transform with respect to its parent.
updateAdditionalConstraints(int, double[]) - Method in class org.orekit.utils.AbstractMultipleShooting: Update the array of additional constraints.
updateAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator: Update state by adding all additional states.
updateAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator: Update state by adding all additional states.
updateFieldShortPeriodTerms(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester: Update the short periodic terms for the "field" elements.
updateMass(double) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Update a spacecraft mass due to maneuver.
updateNominalSpacecraftState(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Update the nominal spacecraft state.
updateReferenceTrajectories(Propagator[], PropagationType, PropagationType) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel: Update the reference trajectories using the propagators as input.
updateReferenceTrajectories(Propagator[], PropagationType, PropagationType) - Method in class org.orekit.estimation.sequential.DSSTKalmanModel: Deprecated.

Update the reference trajectories using the propagators as input.
updateReferenceTrajectories(Propagator[], PropagationType, PropagationType) - Method in class org.orekit.estimation.sequential.KalmanModel: Update the reference trajectories using the propagators as input.
updateReferenceTrajectories(Propagator[], PropagationType, PropagationType) - Method in class org.orekit.estimation.sequential.TLEKalmanModel: Deprecated.

Update the reference trajectories using the propagators as input.
updateReferenceTrajectory(DSSTPropagator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Update the reference trajectories using the propagator as input.
updateShortPeriods(SpacecraftState) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Update the DSST short periodic terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Update the short period terms.
updateTransform(Frame, Frame, Transform, AbsoluteDate) - Method in class org.orekit.frames.UpdatableFrame: Update the transform from parent frame implicitly according to two other frames.
updateUnmanagedStates(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator: Update state by adding unmanaged states.
updateUnmanagedStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator: Update state by adding unmanaged states.
UpperBounds - Class in org.orekit.propagation.semianalytical.dsst.utilities: Utility class to compute upper bounds for truncation algorithms.
URANUS - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Uranus.
USER_DEFINED_PREFIX - Static variable in class org.orekit.files.ccsds.ndm.odm.UserDefined: Prefix for user defined parameters keys.
USER_DEFINED_XML_ATTRIBUTE - Static variable in class org.orekit.files.ccsds.ndm.odm.UserDefined: Attribute name for user defined parameters keys.
USER_DEFINED_XML_TAG - Static variable in class org.orekit.files.ccsds.ndm.odm.UserDefined: Tag name for user defined parameters keys.
UserDefined - Class in org.orekit.files.ccsds.ndm.odm: Container for user defined data.
UserDefined() - Constructor for class org.orekit.files.ccsds.ndm.odm.UserDefined: Create an empty data set.
UserDefinedWriter - Class in org.orekit.files.ccsds.ndm.odm: Writer for user defined parameters data.
UserDefinedWriter(String, String, UserDefined) - Constructor for class org.orekit.files.ccsds.ndm.odm.UserDefinedWriter: Create a writer.
UserDefinedXmlTokenBuilder - Class in org.orekit.files.ccsds.utils.lexical: Builder for user-defined parameters.
UserDefinedXmlTokenBuilder() - Constructor for class org.orekit.files.ccsds.utils.lexical.UserDefinedXmlTokenBuilder
UserRangeAccuracy - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris.utils: User Range Accuracy.
UserRangeAccuracy(int) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.UserRangeAccuracy: Simple constructor.
usesInterpolation() - Method in class org.orekit.frames.EOPHistory: Check if the instance uses interpolation on tidal corrections.
UT1Scale - Class in org.orekit.time: Universal Time 1.
UT1Scale(EOPHistory, UTCScale) - Constructor for class org.orekit.time.UT1Scale: Simple constructor.
utc - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: UTC time scale.
utc - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: UTC time scale.
UTCScale - Class in org.orekit.time: Coordinated Universal Time.
UTCTAIBulletinAFilesLoader - Class in org.orekit.time: Loader for UTC-TAI extracted from bulletin A files.
UTCTAIBulletinAFilesLoader(String) - Constructor for class org.orekit.time.UTCTAIBulletinAFilesLoader: Build a loader for IERS bulletins A files.
UTCTAIBulletinAFilesLoader(String, DataProvidersManager) - Constructor for class org.orekit.time.UTCTAIBulletinAFilesLoader: Build a loader for IERS bulletins A files.
UTCTAIHistoryFilesLoader - Class in org.orekit.time: Loader for UTC versus TAI history files.
UTCTAIHistoryFilesLoader() - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader: Build a loader for UTC-TAI history file.
UTCTAIHistoryFilesLoader(DataProvidersManager) - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader: Build a loader for UTC-TAI history file.
UTCTAIHistoryFilesLoader.Parser - Class in org.orekit.time: Internal class performing the parsing.
UTCTAIOffset - Class in org.orekit.time: Offset between UTC and TAI time scales.
UTCTAIOffsetsLoader - Interface in org.orekit.time: Interface for loading UTC-TAI offsets data files.
UTCTAIOffsetsLoader.Parser - Interface in org.orekit.time: Interface for parsing UTC-TAI offsets from a stream.
UTF8Control() - Constructor for class org.orekit.errors.OrekitMessages.UTF8Control

V

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

W

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

X

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

Y

YawCompensation - Class in org.orekit.attitudes: This class handles yaw compensation attitude provider.
YawCompensation(Frame, GroundPointing) - Constructor for class org.orekit.attitudes.YawCompensation: Creates a new instance.
YawSteering - Class in org.orekit.attitudes: This class handles yaw steering law.
YawSteering(Frame, GroundPointing, PVCoordinatesProvider, Vector3D) - Constructor for class org.orekit.attitudes.YawSteering: Creates a new instance.
YEAR - Static variable in class org.orekit.utils.units.Unit: Julian year unit.
yield(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.Duration: Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate: Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate: Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider: Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider: Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(SpacecraftState) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider: Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(SpacecraftState) - Method in class org.orekit.propagation.integration.AdditionalEquationsAdapter: Deprecated.

Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider: Check if this provider should yield so another provider has an opportunity to add missing parts.
yield(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.integration.FieldAdditionalEquationsAdapter: Deprecated.

Check if this provider should yield so another provider has an opportunity to add missing parts.
YUMAParser - Class in org.orekit.gnss: This class reads Yuma almanac files and provides GPS almanacs.
YUMAParser(String) - Constructor for class org.orekit.gnss.YUMAParser: Simple constructor.
YUMAParser(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.gnss.YUMAParser: Create a YUMA loader/parser with the given source for YUMA auxiliary data files.

Z

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

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z