Index (OREKIT 13.0-SNAPSHOT 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
All Classes All Packages

A

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.
A - org.orekit.gnss.SignalCode: Galileo A PRS / IRNSS A SPS / GLONASS L1OCd and L2CSI / Beidou B1A and B3A codes.
A - Static variable in enum org.orekit.orbits.OrbitType: Name for semi major axis.
A_SBAS - org.orekit.files.rinex.navigation.SbasId: African Satellite-Based Augmentation System (ASECNA).
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.AttitudeEndpoints: Constant for A → B diraction.
A3OVK2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: A3OVK2.
AberrationModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical angular measurement with (the inverse of) stellar aberration.
AberrationModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.AberrationModifier: Empty constructor.
AberrationModifier(DataContext) - Constructor for class org.orekit.estimation.measurements.modifiers.AberrationModifier: Constructor.
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(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, int, int, int, int, TimeOffset, 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, 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, TimeOffset, 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(String, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location (parsed from a string) in a time scale.
AbsoluteDate(Instant) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from an instant in utc time scale.
AbsoluteDate(Instant, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from an instant in a time scale.
AbsoluteDate(Instant, UTCScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from an instant in the 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 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.
AbsoluteDate(AbsoluteDate, long, TimeUnit) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from an elapsed duration since another instant.
AbsoluteDate(AbsoluteDate, TimeOffset) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from an elapsed duration since another instant.
AbsoluteDate(AbsoluteDate, TimeOffset, 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.
AbsoluteDate(DateComponents, TimeComponents, 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(DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(TimeOffset) - Constructor for class org.orekit.time.AbsoluteDate: Build a date from an offset since a reference epoch.
AbsolutePVCoordinates - Class in org.orekit.utils: Position - Velocity - Acceleration linked to a date and a frame.
AbsolutePVCoordinates(Frame, AbsoluteDate, FieldVector3D) - Constructor for class org.orekit.utils.AbsolutePVCoordinates: Builds a AbsolutePVCoordinates triplet from a FieldVector3D<Derivative>.
AbsolutePVCoordinates(Frame, AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AbsolutePVCoordinates: Build from position and velocity.
AbsolutePVCoordinates(Frame, AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AbsolutePVCoordinates: Build from position, velocity, acceleration.
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, 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(AbsoluteDate, AbsolutePVCoordinates, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates: Subtractive constructor
AbsolutePVCoordinatesHermiteInterpolator - Class in org.orekit.utils: Class using a Hermite interpolator to interpolate absolute position-velocity-acceleration coordinates.
AbsolutePVCoordinatesHermiteInterpolator(int, double, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator: Constructor.
AbsolutePVCoordinatesHermiteInterpolator(int, Frame) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator: Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
AbsolutePVCoordinatesHermiteInterpolator(int, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator: Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
AbsolutePVCoordinatesHermiteInterpolator(Frame) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator: Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
ABSORPTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive: Parameter name for absorption coefficient.
AbstractAlfriend1999 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod: Abstract class for Alfriend1999 normal and maximised methods as they share lots of similarities.
AbstractAlfriend1999(String) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractAlfriend1999: Default constructor.
AbstractAlmanac<O extends AbstractAlmanac<O>> - Class in org.orekit.propagation.analytical.gnss.data: Base class for GNSS almanacs.
AbstractAlmanac(double, double, int, TimeScales, SatelliteSystem) - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac: Constructor.
AbstractAlmanac(FieldAbstractAlmanac<T, A>) - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac: Constructor from field instance.
AbstractAnalyticalGradientConverter - Class in org.orekit.propagation.analytical: Converter for analytical orbit propagator.
AbstractAnalyticalGradientConverter(AbstractAnalyticalPropagator, 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.
AbstractAnalyticalPropagatorBuilder<T extends AbstractAnalyticalPropagator> - Class in org.orekit.propagation.conversion: Abstract class for propagator builders of analytical models (except for ephemeris i.e. interpolated ones).
AbstractAnalyticalPropagatorBuilder(Orbit, PositionAngleType, double, boolean, AttitudeProvider, double) - Constructor for class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder: Build a new instance.
AbstractAveragedOrbitalState - Class in org.orekit.propagation.conversion.averaging: Abstract class representing averaged orbital state.
AbstractAveragedOrbitalState(AbsoluteDate, Frame) - Constructor for class org.orekit.propagation.conversion.averaging.AbstractAveragedOrbitalState: Protected constructor.
AbstractBatchLSModel - Class in org.orekit.estimation.leastsquares: Bridge between measurements and least squares problems.
AbstractBatchLSModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Constructor for class org.orekit.estimation.leastsquares.AbstractBatchLSModel: Constructor.
AbstractBodyAttraction - Class in org.orekit.forces.gravity: Abstract class for non-central body attraction force model.
AbstractBodyAttraction(ExtendedPositionProvider, String, double) - Constructor for class org.orekit.forces.gravity.AbstractBodyAttraction: Simple constructor.
AbstractBuilder<T extends AbstractBuilder<T>> - Class in org.orekit.files.ccsds.ndm: Abstract builder for all CCSDS Message files parsers/writers.
AbstractBuilder(IERSConventions, double, double, DataContext, AbsoluteDate, RangeUnitsConverter) - Constructor for class org.orekit.files.ccsds.ndm.AbstractBuilder: Complete constructor.
AbstractCartesianAdjointEquationTerm - Class in org.orekit.control.indirect.adjoint: Abstract class to define terms in the adjoint equations and Hamiltonian for Cartesian coordinates.
AbstractCartesianAdjointEquationTerm() - Constructor for class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm
AbstractCartesianAdjointGravitationalTerm - Class in org.orekit.control.indirect.adjoint: Abstract class for common computations regarding adjoint dynamics and gravity for Cartesian coordinates.
AbstractCartesianAdjointGravitationalTerm(double) - Constructor for class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointGravitationalTerm: Constructor.
AbstractCartesianAdjointNewtonianTerm - Class in org.orekit.control.indirect.adjoint: Abstract class for common computations regarding adjoint dynamics and Newtonian gravity for Cartesian coordinates.
AbstractCartesianAdjointNewtonianTerm(double) - Constructor for class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNewtonianTerm: Constructor.
AbstractCartesianAdjointNonCentralBodyTerm - Class in org.orekit.control.indirect.adjoint: Abstract class defining the contributions of a point-mass, single body gravity in the adjoint equations for Cartesian coordinates.
AbstractCartesianAdjointNonCentralBodyTerm(double, ExtendedPositionProvider) - Constructor for class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm: Constructor.
AbstractCartesianCost - Class in org.orekit.control.indirect.adjoint.cost: Abstract class for cost with Cartesian coordinates.
AbstractCartesianCost(String, double) - Constructor for class org.orekit.control.indirect.adjoint.cost.AbstractCartesianCost: Constructor.
AbstractChaoMappingFunction - Class in org.orekit.models.earth.troposphere: Chao mapping function for radio wavelengths.
AbstractChaoMappingFunction(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.AbstractChaoMappingFunction: Builds a new instance.
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: Constructor with default control cost type.
AbstractConstantThrustPropulsionModel(double, double, Vector3D, Control3DVectorCostType, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Generic constructor.
AbstractConstituentParser<H extends Header,T extends NdmConstituent<H,?>,P extends AbstractConstituentParser<H,T,?>> - Class in org.orekit.files.ccsds.utils.parsing: Parser for CCSDS messages.
AbstractConstituentParser(String, String, IERSConventions, boolean, DataContext, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - 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) - Constructor for class org.orekit.propagation.events.AbstractDetector: Build a new instance.
AbstractDetector(EventDetectionSettings, EventHandler) - 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 with default value for finite differences flag.
AbstractDragForceModel(Atmosphere, boolean) - 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.
AbstractEncodedMessage - Class in org.orekit.gnss.metric.parser: Encoded messages as a sequence of bytes.
AbstractEncodedMessage() - Constructor for class org.orekit.gnss.metric.parser.AbstractEncodedMessage: Empty constructor.
AbstractEncounterLOF - Class in org.orekit.frames.encounter: Abstract class for encounter frame between two objects.
AbstractEncounterLOF(FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.encounter.AbstractEncounterLOF: Constructor with FieldPVCoordinates.
AbstractEncounterLOF(PVCoordinates) - Constructor for class org.orekit.frames.encounter.AbstractEncounterLOF: Constructor with PVCoordinates.
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.
AbstractFieldOrbitInterpolator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.orbits: Abstract class for orbit interpolator.
AbstractFieldOrbitInterpolator(int, double, Frame) - Constructor for class org.orekit.orbits.AbstractFieldOrbitInterpolator: Constructor.
AbstractFieldTimeInterpolator<T extends FieldTimeStamped<KK>,KK extends CalculusFieldElement<KK>> - Class in org.orekit.time: Abstract class for time interpolator.
AbstractFieldTimeInterpolator(int, double) - Constructor for class org.orekit.time.AbstractFieldTimeInterpolator: Constructor.
AbstractFieldTimeInterpolator.InterpolationData - Class in org.orekit.time: Nested class used to store interpolation data.
AbstractFixedBoundaryCartesianSingleShooting - Class in org.orekit.control.indirect.shooting: Abstract class for indirect single shooting methods with Cartesian coordinates for fixed time fixed boundary.
AbstractFixedBoundaryCartesianSingleShooting(ShootingPropagationSettings, FixedTimeBoundaryOrbits, CartesianBoundaryConditionChecker) - Constructor for class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting: Constructor with boundary conditions as orbits.
AbstractFixedBoundaryCartesianSingleShooting(ShootingPropagationSettings, FixedTimeCartesianBoundaryStates, CartesianBoundaryConditionChecker) - Constructor for class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting: Constructor with boundary conditions as orbits.
AbstractFixedInitialCartesianSingleShooting - Class in org.orekit.control.indirect.shooting: Abstract class for indirect single shooting methods with fixed initial Cartesian state.
AbstractFixedInitialCartesianSingleShooting(ShootingPropagationSettings, SpacecraftState) - Constructor for class org.orekit.control.indirect.shooting.AbstractFixedInitialCartesianSingleShooting: Constructor with boundary conditions as orbits.
AbstractFixedSingleStepIntegratorBuilder<T extends FixedStepRungeKuttaIntegrator> - Class in org.orekit.propagation.conversion: Abstract class for fixed-step, single-step integrator builder.
AbstractFixedSingleStepIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.AbstractFixedSingleStepIntegratorBuilder: Constructor.
AbstractFixedStepFieldIntegratorBuilder<T extends CalculusFieldElement<T>,W extends AbstractFieldIntegrator<T>> - Class in org.orekit.propagation.conversion: Abstract class for integrator builder using fixed step size.
AbstractFixedStepFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.AbstractFixedStepFieldIntegratorBuilder: Constructor.
AbstractFixedStepFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.AbstractFixedStepFieldIntegratorBuilder: Constructor using a "fielded" step.
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, double, boolean) - Constructor for class org.orekit.files.ccsds.utils.generation.AbstractGenerator: Deprecated.
since 13.0, since does not allow user to specify formatter. This defaults to AccurateFormatter Use AbstractGenerator(Appendable, String, double, boolean, Formatter) instead.
AbstractGenerator(Appendable, String, double, boolean, Formatter) - Constructor for class org.orekit.files.ccsds.utils.generation.AbstractGenerator: Simple constructor.
AbstractGlobalPressureTemperature - Class in org.orekit.models.earth.weather: Base class for Global Pressure and Temperature 2, 2w and 3 models.
AbstractGlobalPressureTemperature(DataSource, SeasonalModelType...) - Constructor for class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature: Constructor with source of GPTn auxiliary data given by user.
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.
AbstractImpulseManeuver - Class in org.orekit.forces.maneuvers: Abstract class for impulsive maneuvers.
AbstractImpulseManeuver(AttitudeProvider, Control3DVectorCostType) - Constructor for class org.orekit.forces.maneuvers.AbstractImpulseManeuver: Protected constructor.
AbstractIndirectShooting - Class in org.orekit.control.indirect.shooting: Abstract class for indirect shooting methods with numerical propagation.
AbstractIndirectShooting(ShootingPropagationSettings) - Constructor for class org.orekit.control.indirect.shooting.AbstractIndirectShooting: 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).
AbstractIntegratedPropagatorBuilder<T extends AbstractIntegratedPropagator> - Class in org.orekit.propagation.conversion: Abstract class for builders for integrator-based propagators.
AbstractIntegratedPropagatorBuilder(Orbit, ODEIntegratorBuilder, PositionAngleType, double, PropagationType, AttitudeProvider, double) - Constructor for class org.orekit.propagation.conversion.AbstractIntegratedPropagatorBuilder: Build a new instance.
AbstractIntegratorBuilder<T extends AbstractIntegrator> - Class in org.orekit.propagation.conversion: Abstract class for integrator builder.
AbstractIntegratorBuilder() - Constructor for class org.orekit.propagation.conversion.AbstractIntegratorBuilder
AbstractInterSatellitesMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.gnss: Base class for measurement between two satellites that are both estimated.
AbstractInterSatellitesMeasurement(AbsoluteDate, double, double, double, ObservableSatellite, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractInterSatellitesMeasurement: Constructor.
AbstractKalmanEstimator - Class in org.orekit.estimation.sequential: Base class for Kalman estimators.
AbstractKalmanEstimator(MatrixDecomposer, List<? extends PropagatorBuilder>) - Constructor for class org.orekit.estimation.sequential.AbstractKalmanEstimator: Constructor.
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.
AbstractLightFluxModel - Class in org.orekit.forces.radiation: Abstract class for light flux models.
AbstractLightFluxModel(ExtendedPositionProvider) - Constructor for class org.orekit.forces.radiation.AbstractLightFluxModel: Constructor.
AbstractLimitedVariableStepFieldIntegratorBuilder<T extends CalculusFieldElement<T>,W extends MultistepFieldIntegrator<T>> - Class in org.orekit.propagation.conversion: Abstract class for integrator using a limited number of variable steps.
AbstractLimitedVariableStepFieldIntegratorBuilder(int, double, double, ToleranceProvider) - Constructor for class org.orekit.propagation.conversion.AbstractLimitedVariableStepFieldIntegratorBuilder: 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 multi-dimensional measurements.
AbstractMeasurement(AbsoluteDate, double, double, double, List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement: Simple constructor for mono-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, Function<ParseToken, List<ParseToken>>[]) - 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>, double, int, boolean, String) - Constructor for class org.orekit.utils.AbstractMultipleShooting: Simple Constructor.
AbstractNavigationMessage<O extends AbstractNavigationMessage<O>> - Class in org.orekit.propagation.analytical.gnss.data: Base class for GNSS navigation messages.
AbstractNavigationMessage(double, double, int, TimeScales, SatelliteSystem) - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Constructor.
AbstractNavigationMessage(FieldAbstractNavigationMessage<T, A>) - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Constructor from field instance.
AbstractOnBoardMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.gnss: Base class modeling a measurement where receiver is a satellite.
AbstractOnBoardMeasurement(AbsoluteDate, double, double, double, List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement: Constructor.
AbstractOneWayGNSSMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.gnss: Base class for one-way GNSS measurement.
AbstractOneWayGNSSMeasurement(PVCoordinatesProvider, QuadraticClockModel, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractOneWayGNSSMeasurement: Simple constructor.
AbstractOrbitInterpolator - Class in org.orekit.orbits: Abstract class for orbit interpolator.
AbstractOrbitInterpolator(int, double, Frame) - Constructor for class org.orekit.orbits.AbstractOrbitInterpolator: Constructor.
AbstractParametricAcceleration - Class in org.orekit.forces.empirical: Abstract class for parametric acceleration.
AbstractParametricAcceleration(Vector3D, boolean, AttitudeProvider) - Constructor for class org.orekit.forces.empirical.AbstractParametricAcceleration
AbstractPropagator - Class in org.orekit.propagation: Common handling of Propagator methods for propagators.
AbstractPropagator() - Constructor for class org.orekit.propagation.AbstractPropagator: Build a new instance.
AbstractPropagatorBuilder<T extends AbstractPropagator> - Class in org.orekit.propagation.conversion: Base class for propagator builders.
AbstractPropagatorBuilder(Orbit, PositionAngleType, double, boolean) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Build a new instance.
AbstractPropagatorBuilder(Orbit, PositionAngleType, double, boolean, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Build a new instance.
AbstractPropagatorBuilder(Orbit, PositionAngleType, double, boolean, AttitudeProvider, double) - 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(ExtendedPositionProvider, OneAxisEllipsoid, EventDetectionSettings) - 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.
AbstractRelativisticClockOnBoardRangeRateModifier<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical range-rate measurement with relativistic frequency deviation.
AbstractRelativisticClockOnBoardRangeRateModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockOnBoardRangeRateModifier: Simple constructor.
AbstractRelativisticJ2ClockModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical measurements with relativistic J2 clock correction.
AbstractRelativisticJ2ClockModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractRelativisticJ2ClockModifier: Constructor for the Relativistic J2 Clock modifier.
AbstractScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation: Base implementation of Scheduler managing dates selection.
AbstractScheduler(MeasurementBuilder<T>, DatesSelector, Predicate<EstimatedMeasurementBase<T>>) - 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.
AbstractShortTermEncounter1DNumerical2DPOCMethod - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod: This abstract class serves as a foundation to create 1D numerical 2D probability of collision computing method.
AbstractShortTermEncounter1DNumerical2DPOCMethod(String, UnivariateIntegrator, int) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod: Customizable constructor.
AbstractShortTermEncounter2DPOCMethod - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod: This abstract class serves as a foundation to create 2D probability of collision computing method assuming a short term encounter model.
AbstractShortTermEncounter2DPOCMethod(String) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod: Constructor.
AbstractSinex - Class in org.orekit.files.sinex: Base container for Solution INdependent EXchange (SINEX) files.
AbstractSinex(TimeScales, AbsoluteDate, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.files.sinex.AbstractSinex: Simple constructor.
AbstractSinexParser<T extends AbstractSinex,P extends ParseInfo<T>> - Class in org.orekit.files.sinex: Base parser for Solution INdependent EXchange (SINEX) files.
AbstractSinexParser(TimeScales) - Constructor for class org.orekit.files.sinex.AbstractSinexParser: 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.
AbstractSolarActivityData<L extends AbstractSolarActivityDataLoader.LineParameters,D extends AbstractSolarActivityDataLoader<L>> - Class in org.orekit.models.earth.atmosphere.data: Abstract class for solar activity data.
AbstractSolarActivityData(String, D, DataProvidersManager, TimeScale, int, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData
AbstractSolarActivityData(DataSource, D, TimeScale, int, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData: Simple constructor.
AbstractSolarActivityData.LocalSolarActivity - Class in org.orekit.models.earth.atmosphere.data: Container for weather parameters around current date.
AbstractSolarActivityData.SolarActivityGenerator - Class in org.orekit.models.earth.atmosphere.data: Generator used in the weather data cache.
AbstractSolarActivityDataLoader<L extends AbstractSolarActivityDataLoader.LineParameters> - Class in org.orekit.models.earth.atmosphere.data: Abstract class for solar activity data loader.
AbstractSolarActivityDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader: Constructor.
AbstractSolarActivityDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data: Container class for Solar activity indexes.
AbstractSolarLightFluxModel - Class in org.orekit.forces.radiation: Abstract class for the definition of the solar flux model with a single occulting body of spherical shape.
AbstractSolarLightFluxModel(double, ExtendedPositionProvider, double, EventDetectionSettings) - Constructor for class org.orekit.forces.radiation.AbstractSolarLightFluxModel: Constructor.
AbstractSolarLightFluxModel(ExtendedPositionProvider, double, EventDetectionSettings) - Constructor for class org.orekit.forces.radiation.AbstractSolarLightFluxModel: Constructor with default value for reference flux.
AbstractStateCovarianceInterpolator - Class in org.orekit.propagation: Abstract class for orbit and state covariance interpolator.
AbstractStateCovarianceInterpolator(int, double, TimeInterpolator<Orbit>, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.AbstractStateCovarianceInterpolator: Constructor.
AbstractStateCovarianceInterpolator(int, double, TimeInterpolator<Orbit>, LOFType) - Constructor for class org.orekit.propagation.AbstractStateCovarianceInterpolator: Constructor.
AbstractStateModifier - Class in org.orekit.propagation: Abstract base class for modifying state during propagation.
AbstractStateModifier() - Constructor for class org.orekit.propagation.AbstractStateModifier
AbstractSunInfluencedAtmosphere - Class in org.orekit.models.earth.atmosphere: Abstract class for atmospheric models using the Sun's position.
AbstractSunInfluencedAtmosphere(ExtendedPositionProvider) - Constructor for class org.orekit.models.earth.atmosphere.AbstractSunInfluencedAtmosphere: Constructor.
AbstractTimeInterpolator<T extends TimeStamped> - Class in org.orekit.time: Abstract class for time interpolator.
AbstractTimeInterpolator(int, double) - Constructor for class org.orekit.time.AbstractTimeInterpolator: Constructor.
AbstractTimeInterpolator.InterpolationData - Class in org.orekit.time: Nested class used to store interpolation data.
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.
AbstractVariableStepFieldIntegratorBuilder<T extends CalculusFieldElement<T>,W extends AdaptiveStepsizeFieldIntegrator<T>> - Class in org.orekit.propagation.conversion: Abstract class for integrator builder using variable step size.
AbstractVariableStepFieldIntegratorBuilder(double, double, ToleranceProvider) - Constructor for class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder: Constructor with expected velocity error.
AbstractVariableStepIntegratorBuilder<T extends AdaptiveStepsizeIntegrator> - Class in org.orekit.propagation.conversion: Abstract class for integrator builder using variable step size.
AbstractVariableStepIntegratorBuilder(double, double, ToleranceProvider) - Constructor for class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder: Constructor.
AbstractVienna - Class in org.orekit.models.earth.troposphere: The Vienna tropospheric delay model for radio techniques.
AbstractVienna(ViennaAProvider, AzimuthalGradientProvider, TroposphericModel, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.AbstractVienna: Build a new instance.
AbstractWindUp<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.gnss: Base class for wind-up effect computation.
AbstractWindUp(Dipole, Dipole) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractWindUp: 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.
ACC - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment: Accelerometer.
ACC_DIR_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: One σ off-nominal acceleration direction.
ACC_INTERP - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Interpolation mode between current and next acceleration line.
ACC_MAG_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: One σ percent error on acceleration magnitude.
ACC_X - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Acceleration along X axis.
ACC_Y - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Acceleration along Y axis.
ACC_Z - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Acceleration along Z axis.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.DragForce: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.TimeSpanDragForce: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.ParametricAcceleration: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.ForceModel: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.ForceModelModifier: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.DeSitterRelativity: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.J2OnlyPerturbation: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.LenseThirringRelativity: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.Relativity: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.inertia.InertialForces: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.Maneuver: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.ECOM2: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.RadiationPressureModel: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.DragForce: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.TimeSpanDragForce: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.ParametricAcceleration: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in interface org.orekit.forces.ForceModel: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in interface org.orekit.forces.ForceModelModifier: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.DeSitterRelativity: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.J2OnlyPerturbation: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.LenseThirringRelativity: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.Relativity: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.inertia.InertialForces: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.Maneuver: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.ECOM2: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.RadiationPressureModel: Compute acceleration.
acceleration(SpacecraftState, double[]) - 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_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation: Suffix for ground clock drift parameters name.
AccelerationModel - Interface in org.orekit.forces.empirical: Acceleration model used by empirical force.
accept(boolean) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.BooleanConsumer: Consume a boolean.
accept(char) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CharConsumer: Consume a character.
accept(char, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.LabeledDoubleConsumer: Consume an indexed double.
accept(double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DoubleConsumer: Consume a double.
accept(double[]) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DoubleArrayConsumer: Consume an array of doubles.
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(int, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedDoubleConsumer: Consume an indexed double.
accept(int, double[]) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedDoubleArrayConsumer: Consume an indexed double array.
accept(int, int) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedIntConsumer: Consume an integer.
accept(int, int, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DoublyIndexedDoubleConsumer: Consume a doubly indexed double.
accept(int, String) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedStringConsumer: Consume an indexed string.
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(List<BodyFacade>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CenterListConsumer: Consume a body center.
accept(List<Unit>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.UnitListConsumer: Consume a list of units.
accept(List<T>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.EnumListConsumer: Consume an enum.
accept(RotationOrder) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.RotationOrderConsumer: Consume a data.
accept(Vector3D) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.VectorConsumer: Consume a vector.
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(BodyFacade) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CenterConsumer: Consume a body center.
accept(FrameFacade) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.FrameConsumer: Consume a frame.
accept(TimeSystem) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.TimeSystemConsumer: Consume a time system.
accept(Maneuvrable) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.ManeuvrableConsumer: Consume a Maneuvrable.
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(MessageParser<T>) - Method in class org.orekit.files.ccsds.utils.lexical.XmlLexicalAnalyzer: Parse a CCSDS Message.
accept(AbsoluteDate) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DateConsumer: Consume a date.
accept(T) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.EnumConsumer: Consume an enum.
acceptComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer: Check if container is still accepting comments.
acceptStep(FieldAbstractAnalyticalPropagator.FieldBasicStepInterpolator, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Accept a step, triggering events and step handlers.
acceptStep(OrekitStepInterpolator, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Accept a step, triggering events and step handlers.
AccuracyProvider - Interface in org.orekit.gnss.metric.messages.common: This interface represents an accuracy providerused to validate RTCM ephemeris messages.
accurateDurationFrom(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate: Compute the physically elapsed duration between two instants.
AccurateFormatter - Class in org.orekit.utils: Formatter used to produce strings from data with high accuracy.
AccurateFormatter() - Constructor for class org.orekit.utils.AccurateFormatter: Public constructor.
accurateOffsetFrom(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.
Acm - Class in org.orekit.files.ccsds.ndm.adm.acm: This class gathers the informations present in the Attitude Comprehensive Message (ACM).
Acm(AdmHeader, List<Segment<AcmMetadata, AcmData>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.Acm: Simple constructor.
ACM_DATA_ELEMENTS - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey: List of elements of information data blocks included in this message.
AcmData - Class in org.orekit.files.ccsds.ndm.adm.acm: Data container for Attitude Comprehensive Messages.
AcmData(List<AttitudeStateHistory>, AttitudePhysicalProperties, List<AttitudeCovarianceHistory>, List<AttitudeManeuver>, AttitudeDetermination, UserDefined) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmData: Simple constructor.
AcmDataSubStructureKey - Enum in org.orekit.files.ccsds.ndm.adm.acm: Keywords for ACM data sub-structure.
AcmElements - Enum in org.orekit.files.ccsds.ndm.adm.acm: Data elements types used in CCSDS Attitude Comprehensive Messages.
AcmMetadata - Class in org.orekit.files.ccsds.ndm.adm.acm: Meta-data for Attitude Comprehensive Message.
AcmMetadata(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata: Create a new meta-data.
AcmMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.acm: Keys for ACM container entries.
AcmParser - Class in org.orekit.files.ccsds.ndm.adm.acm: A parser for the CCSDS ACM (Attitude Comprehensive Message).
AcmParser(IERSConventions, boolean, DataContext, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmParser: Complete constructor.
AcmSatelliteEphemeris - Class in org.orekit.files.ccsds.ndm.adm.acm: ACM ephemeris blocks for a single satellite.
AcmSatelliteEphemeris(String, List<AttitudeStateHistory>) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmSatelliteEphemeris: Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.
AcmWriter - Class in org.orekit.files.ccsds.ndm.adm.acm: Writer for CCSDS Attitude Comprehensive Message.
AcmWriter(IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmWriter: Complete constructor.
ACTUAL_OD_SPAN - org.orekit.files.ccsds.ndm.cdm.ODParametersKey: Based on the observations available and the RECOMMENDED_OD_SPAN, the actual time span used for the OD of the object.
ACTUAL_OD_SPAN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey: Actual time span used for the OD of the object.
ACTUATOR - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment: Actuator: could denote reaction wheels, solar arrays, thrusters, etc..
ACTUATOR_USED - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey: Actuator used.
ad - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey: Orbit determination section.
AD - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey: Attitude determination section.
AD - org.orekit.files.ccsds.ndm.adm.acm.AcmElements: Attitude determination.
AD_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey: Identification number.
AD_METHOD - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey: Attitude determination method.
AD_PREV_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey: Identification of previous attitude determination.
AdamsBashforthFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion: Builder for AdamsBashforthFieldIntegrator.
AdamsBashforthFieldIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthFieldIntegratorBuilder: Build a new instance using default integration tolerances.
AdamsBashforthFieldIntegratorBuilder(int, double, double, ToleranceProvider) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthFieldIntegratorBuilder: Build a new instance.
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 using default integration tolerances.
AdamsBashforthIntegratorBuilder(int, double, double, ToleranceProvider) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder: Build a new instance.
AdamsMoultonFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion: Builder for AdamsMoultonFieldIntegrator.
AdamsMoultonFieldIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonFieldIntegratorBuilder: Build a new instance.
AdamsMoultonFieldIntegratorBuilder(int, double, double, ToleranceProvider) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonFieldIntegratorBuilder: 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 using default integration tolerances.
AdamsMoultonIntegratorBuilder(int, double, double, ToleranceProvider) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder: Build a new instance using default integration tolerances.
AdaptableInterval - Interface in org.orekit.propagation.events.intervals: This interface represents an event checking interval that depends on state.
AdapterDetector - Class in org.orekit.propagation.events: Deprecated.
since 13.0. Use DetectorModifier instead.
AdapterDetector(EventDetector) - Constructor for class org.orekit.propagation.events.AdapterDetector: Deprecated.

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.
ADBARV - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType: Spherical 6-element set (α,δ,β,A,r,v).
add(double, OrekitFixedStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer: Add a handler for fixed size step.
add(IIRVVector) - Method in class org.orekit.files.iirv.IIRVMessage: Adds an IIRVVector to the message (see ArrayList.add(Object)).
add(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer: Add a handler for variable size step.
add(OrekitStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer: Add a handler for variable size step.
add(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix: Add the argument matrix with the current matrix.
add(TimeOffset) - Method in class org.orekit.time.TimeOffset: Build a time by adding two times.
add(ParameterDriver) - Method in class org.orekit.utils.ParameterDriversList: Add a driver.
add(T, FieldOrekitFixedStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer: Add a handler for fixed size step.
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.
addAdditionalData(String, Object) - Method in class org.orekit.propagation.FieldSpacecraftState: Add an additional data.
addAdditionalData(String, Object) - Method in class org.orekit.propagation.SpacecraftState: Add an additional data.
addAdditionalDataProvider(AdditionalDataProvider<?>) - Method in class org.orekit.propagation.AbstractPropagator: Add a set of user-specified data to be computed along with the orbit propagation.
addAdditionalDataProvider(AdditionalDataProvider<?>) - Method in interface org.orekit.propagation.Propagator: Add a set of user-specified data to be computed along with the orbit propagation.
addAdditionalDataProvider(FieldAdditionalDataProvider<?, T>) - Method in class org.orekit.propagation.FieldAbstractPropagator: Add a set of user-specified data to be computed along with the orbit propagation.
addAdditionalDataProvider(FieldAdditionalDataProvider<?, T>) - Method in interface org.orekit.propagation.FieldPropagator: Add a set of user-specified data to be computed along with the orbit propagation.
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.
addAdditionalStateDerivative(String, double...) - Method in class org.orekit.propagation.SpacecraftState: Add an additional state derivative.
addAdditionalStateDerivative(String, T...) - Method in class org.orekit.propagation.FieldSpacecraftState: Add an additional state derivative.
addAnglesData(CRD.AnglesMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Add an entry to the list of angles data.
addAntennaKeyValidBefore(AntennaKey, AbsoluteDate) - Method in class org.orekit.files.sinex.Station: Add a antenna key entry valid before a limit date.
Using addAntennaKeyValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
addAppliedDCBS(AppliedDCBS) - Method in class org.orekit.files.rinex.clock.RinexClock: Add an applied differencial code bias corrections.
addAppliedDCBS(AppliedDCBS) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Add applied differential code bias corrections.
addAppliedPCVS(AppliedPCVS) - Method in class org.orekit.files.rinex.clock.RinexClock: Add an applied phase center variations.
addAppliedPCVS(AppliedPCVS) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Add antenna center variation corrections.
addBDGIMMessage(IonosphereBDGIMMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Add an ionosphere BDGIM message.
addBeidouCivilianNavigationMessage(BeidouCivilianNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Add a Beidou navigation message to the list.
addBeidouLegacyNavigationMessage(BeidouLegacyNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Add a Beidou navigation message to the list.
addBias(ObservationType, ObservationType, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.files.sinex.DifferentialSignalBias: Add a bias.
addBias(ObservationType, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.files.sinex.ObservableSpecificSignalBias: Add a bias.
addCalibrationData(CRD.Calibration) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Add an entry to the list of calibration data.
addCalibrationDetailData(CRD.CalibrationDetail) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Add an entry to the list of calibration detail data.
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.files.rinex.clock.RinexClock: Add a clock data line to a specified receiver/satellite.
addClockDataType(RinexClock.ClockDataType) - Method in class org.orekit.files.rinex.clock.RinexClock: Add a clock data types.
addCodeBias(CodeBias) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data: Add a code bias value for the current satellite.
addComment(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Set comment for relative metadata.
addComment(String) - Method in class org.orekit.files.ccsds.ndm.NdmParser: Add comment.
addComment(String) - Method in class org.orekit.files.ccsds.section.CommentsContainer: Add comment.
addComment(String) - Method in class org.orekit.files.rinex.clock.RinexClock: Add a comment line.
addComment(String) - Method in class org.orekit.files.sp3.SP3Header: Add a comment.
addComment(RinexComment) - Method in class org.orekit.files.rinex.RinexFile: Add a comment.
addConfigurationRecord(CRDConfiguration.BaseConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Add a configuration record, such as SystemConfiguation, LaserConfiguration, DetectorConfiguration, etc.
addConstraint(int, int, double) - Method in class org.orekit.utils.AbstractMultipleShooting: Add a constraint on one component of one patch point.
addContribution(BodiesElements, double[][], double[][]) - Method in class org.orekit.forces.gravity.potential.OceanTidesWave: Add the contribution of the wave to Stokes coefficients.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - 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 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.maneuvers.Maneuver: Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - 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(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.maneuvers.Maneuver: Compute the contribution of the force model to the perturbing acceleration.
addCoordinate(SP3Coordinate) - Method in class org.orekit.files.sp3.SP3Segment: Adds a new P/V coordinate.
addCoordinate(SP3Coordinate, double) - Method in class org.orekit.files.sp3.SP3Ephemeris: Adds a new P/V coordinate.
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) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies: 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, String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies: Add the default loaders for celestial bodies.
addDefaultEOP1980HistoryLoaders(String, 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, String) - Method in class org.orekit.frames.LazyLoadedFrames: Add the default loaders EOP history (IAU 1980 precession/nutation).
addDefaultEOP1980HistoryLoaders(String, String, String, String, String, String, Supplier<TimeScale>) - Method in class org.orekit.frames.LazyLoadedEop: Add the default loaders EOP history (IAU 1980 precession/nutation).
addDefaultEOP2000HistoryLoaders(String, 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, String) - Method in class org.orekit.frames.LazyLoadedFrames: Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).
addDefaultEOP2000HistoryLoaders(String, 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).
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).
addEarthOrientationParameter(EarthOrientationParameterMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Add an Earth orientation parameter.
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(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(D) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Add an event detector.
addEventDetector(EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Add an event detector.
addEventDetector(T) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: 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(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.conversion.DSSTPropagatorBuilder: Add a force model to the global perturbation 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.files.rinex.navigation.RinexNavigation: Add a Galileo navigation message to the list.
addGlonassChannel(GlonassSatelliteChannel) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Add GLONASS satellite/channel association.
addGlonassNavigationMessage(GLONASSNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Add a Glonass navigation message to the list.
addGPSCivilianNavigationMessage(GPSCivilianNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Add a GPS civilian navigation message to the list.
addGPSLegacyNavigationMessage(GPSLegacyNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Add a GPS legacy navigation message to the list.
addGridPoint(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient: Add a point to the interpolation grid.
addGridPoint(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient: Add a point to the interpolation grid.
addHandler(EventHandler) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler: Add one handler to the managed handlers list.
addHandlers(EventHandler...) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler: Add several handlers to the managed handlers list.
addImpulseManeuver(ImpulseManeuver) - Method in class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder: Add impulse maneuver.
addImpulseManeuver(ImpulseManeuver) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Add impulse maneuver.
addInput(T) - Method in class org.orekit.data.AbstractListCrawler: Add an input to the supported list.
addIRNSSNavigationMessage(IRNSSNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Add a IRNSS navigation message to the list.
ADDITIONAL_STATE_BAD_TYPE - org.orekit.errors.OrekitMessages: ADDITIONAL_STATE_BAD_TYPE.
ADDITIONAL_STATE_NAME_ALREADY_IN_USE - org.orekit.errors.OrekitMessages: ADDITIONAL_STATE_NAME_ALREADY_IN_USE.
AdditionalCovarianceMetadata - Class in org.orekit.files.ccsds.ndm.cdm: Container for the additional covariance metadata (optional).
AdditionalCovarianceMetadata() - Constructor for class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata: Simple constructor.
AdditionalCovarianceMetadataKey - Enum in org.orekit.files.ccsds.ndm.cdm: Keys for covariance metadatail y a entries.
AdditionalDataProvider<T> - Interface in org.orekit.propagation: This interface allows to modify SpacecraftState and set up additional data.
AdditionalDerivativesProvider - Interface in org.orekit.propagation.integration: Provider for additional derivatives.
additionalParameters - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey: Additional Parameter section.
AdditionalParameters - Class in org.orekit.files.ccsds.ndm.cdm: Container for additional parameters data block.
AdditionalParameters() - Constructor for class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Simple constructor.
AdditionalParametersKey - Enum in org.orekit.files.ccsds.ndm.cdm: Keys for CDM additional parameters entries.
AdditionalParametersWriter - Class in org.orekit.files.ccsds.ndm.cdm: Writer for additional parameters data block for CCSDS Conjunction Data Messages.
addKeplerContribution(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations: Add the contribution of the Kepler evolution.
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.CartesianOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.CircularOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.EquinoctialOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.KeplerianOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.Orbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldCartesianOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldCircularOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldKeplerianOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldOrbit: 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.
addKlobucharMessage(IonosphereKlobucharMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Add an ionosphere Klobuchar message.
addManeuver(Maneuver) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData: Add a maneuver.
addMassDerivative(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations: Add the contribution of the flow rate (dm/dt).
addMassDerivative(T) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations: 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<MultiplexedMeasurement>) - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder: Add a modifier.
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.
addNequickGMessage(IonosphereNequickGMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Add an ionosphere Nequick-G message.
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>, 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>, 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.
addObservationDataSet(ObservationDataSet) - Method in class org.orekit.files.rinex.observation.RinexObservation: Add an observations data set.
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(OneAxisEllipsoid) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Add a new occulting body.
addOccultingBody(ExtendedPositionProvider, 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(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates: Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates: Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates: Add an offset from the instance.
addOptionalSubInterpolatorIfDefined(FieldTimeInterpolator<? extends FieldTimeStamped<S>, S>, List<FieldTimeInterpolator<? extends FieldTimeStamped<S>, S>>) - Method in class org.orekit.time.AbstractFieldTimeInterpolator: Add all lowest level sub interpolators to the sub interpolator list.
addOptionalSubInterpolatorIfDefined(TimeInterpolator<? extends TimeStamped>, List<TimeInterpolator<? extends TimeStamped>>) - Method in class org.orekit.time.AbstractTimeInterpolator: Add all lowest level sub interpolators to the sub interpolator list.
addPadding(String, char, int, boolean) - Static method in class org.orekit.files.iirv.terms.IIRVTermUtils: Add padding characters to a string.
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.
addPhaseShiftCorrection(PhaseShiftCorrection) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Add phase shift correction used to generate phases consistent w/r to cycle shifts.
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(DSSTPropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder: Add a propagation configuration.
addPropagationConfiguration(DSSTPropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder: Add a propagation configuration.
addPropagationConfiguration(PropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder: Add a propagation configuration.
addPropagationConfiguration(PropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder: Add a propagation configuration.
addPropagator(Propagator) - Method in class org.orekit.estimation.measurements.generation.Generator: Add a propagator.
addPropagator(Propagator, String) - 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.
addPsdCorrectionValidAfter(PsdCorrection, AbsoluteDate) - Method in class org.orekit.files.sinex.Station: Add a Post-Seismic Deformation entry valid after a limit date.
Using addPsdCorrectionValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addPVProviderAfter(AbsoluteDate, PVCoordinatesProvider, boolean) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder: Add a PVCoordinatesProvider to the collection.
addPVProviderBefore(AbsoluteDate, PVCoordinatesProvider, boolean) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder: Add a PVCoordinatesProvider to the collection.
addQZSSCivilianNavigationMessage(QZSSCivilianNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Add a QZSS navigation message to the list.
addQZSSLegacyNavigationMessage(QZSSLegacyNavigationMessage) - Method in class org.orekit.files.rinex.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.
addRangeSupplementData(CRD.RangeSupplement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Add an entry to the list of range supplement 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.files.rinex.clock.RinexClock: Add a new receiver to the list of stored receivers.
addReferenceClockList(List<RinexClock.ReferenceClock>, AbsoluteDate) - Method in class org.orekit.files.rinex.clock.RinexClock: Add a list of reference clocks which will be used after a specified date.
addResetter(Field<T>, FieldManeuverTriggersResetter<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers: Add a resetter.
addResetter(Field<T>, FieldManeuverTriggersResetter<T>) - Method in interface org.orekit.forces.maneuvers.trigger.ResettableManeuverTriggers: Add a resetter.
addResetter(ManeuverTriggersResetter) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers: Add a resetter.
addResetter(ManeuverTriggersResetter) - Method in interface org.orekit.forces.maneuvers.trigger.ResettableManeuverTriggers: 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.rinex.clock.RinexClock: Add a new satellite with a given identifier to the list of stored satellites.
addSatellite(String) - Method in class org.orekit.files.sp3.SP3: Add a new satellite with a given identifier to the list of stored satellites.
addSatelliteCoordinate(String, CPF.CPFCoordinate) - Method in class org.orekit.files.ilrs.CPF: Add a new P/V coordinates to the satellite.
addSatelliteCoordinates(String, List<CPF.CPFCoordinate>) - Method in class org.orekit.files.ilrs.CPF: Adds a set of P/V coordinates to the satellite.
addSatelliteVelocityToCPFCoordinate(String, Vector3D) - Method in class org.orekit.files.ilrs.CPF: Add the velocity to the last CPF coordinate entry.
addSatId(String) - Method in class org.orekit.files.sp3.SP3Header: Add a satellite identifier.
addSBASNavigationMessage(SBASNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Add a SBAS navigation message to the list.
addScaleFactorCorrection(SatelliteSystem, ScaleFactorCorrection) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Add scale factor correction.
addScheduler(Scheduler<T>) - Method in class org.orekit.estimation.measurements.generation.Generator: Add a sequences generator for a specific measurement type.
addSensor(AttitudeDeterminationSensor) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination: Add a sensor used.
addSessionStatisticsData(CRD.SessionStatistics) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Add an entry to the list of session statistics data.
addSolution(long[], double) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod: Add a new solution.
addSpanAtDate(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver: Create a new span in values and names time span map given a start date.
addSpans(AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.ParameterDriver: Cut values and names time span map given orbit determination start and end and driver periodicity.
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).
addSubscriber(GeneratedMeasurementSubscriber) - Method in class org.orekit.estimation.measurements.generation.Generator: Add a subscriber.
addSupportedParameters(List<ParameterDriver>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Add supported parameters.
addSwitchingCondition(AttitudeProvider, AttitudeProvider, T, boolean, boolean, double, AngularDerivativesFilter, AttitudeSwitchHandler) - Method in class org.orekit.attitudes.AttitudesSequence: Add a switching condition between two attitude providers.
addSwitchingCondition(AttitudeProvider, AttitudeProvider, T, boolean, boolean, AttitudeSwitchHandler) - Method in class org.orekit.attitudes.AttitudesSwitcher: Add a switching condition between two attitude providers.
addSystemObservationType(SatelliteSystem, ObservationType) - Method in class org.orekit.files.rinex.clock.RinexClock: Add an observation type for a specified satellite system.
addSystemTimeOffset(SystemTimeOffsetMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Add a system time offset.
addTimeSystemCorrections(TimeSystemCorrection) - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader: 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(EstimatedModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel: Add a EstimatedTroposphericModel entry valid after a limit date.
Using addTroposphericModelValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addTroposphericModelValidBefore(EstimatedModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel: 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, AbsoluteDate, boolean) - Method in class org.orekit.utils.TimeSpanMap: Add an entry valid after a limit date.
addValidAfter(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap: Add an entry valid after a limit date.
addValidBefore(T, AbsoluteDate, boolean) - Method in class org.orekit.utils.TimeSpanMap: Add an entry valid before a limit date.
addValidBefore(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap: 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.
addWaypoint(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.utils.WaypointPVBuilder: Add a waypoint.
addWeightedPoint(AbsoluteDate, double, double) - Method in class org.orekit.utils.SecularAndHarmonic: Add a weighted fitting point.
AdjointDynamicsProvider - Interface in org.orekit.control.indirect.shooting.propagation: Interface for adjoint derivatives provider (both standard and Field).
ADM_MSG_LINK - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey: Unique identifier of Attitude Data Message(s) that are linked (relevant) to this Conjunction Data Message.
ADM_MSG_LINK - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey: Unique identifier of Attitude Data Message linked to this Orbit Data Message.
AdmCommonMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm: Keys for APM and AEM entries.
AdmCommonMetadataWriter - Class in org.orekit.files.ccsds.ndm.adm: Writer for Common metadata for CCSDS Attitude Parameter/Ephemeris Messages.
AdmCommonMetadataWriter(AdmMetadata) - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmCommonMetadataWriter: Simple constructor.
AdMethodType - Enum in org.orekit.files.ccsds.definitions: Type of attitude determination method used in CCSDS Attitude Comprehensive Messages.
AdmHeader - Class in org.orekit.files.ccsds.ndm.adm: Header of a CCSDS Attitude Data Message.
AdmHeader() - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmHeader: Constructor.
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.
AdmParser<T extends NdmConstituent<AdmHeader,?>,P extends AbstractConstituentParser<AdmHeader,T,?>> - Class in org.orekit.files.ccsds.ndm.adm: Base class for Attitude Data Message parsers.
AdmParser(String, String, IERSConventions, boolean, DataContext, AbsoluteDate, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmParser: Complete constructor.
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(AdmHeader, 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, Function<ParseToken, List<ParseToken>>[]) - 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.
AF0 - Static variable in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Name for zero-th order clock correction parameter.
AF1 - Static variable in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Name for first order clock correction parameter.
AF2 - Static variable in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Name for second order clock correction parameter.
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.
AggregateBoundedPropagator(NavigableMap<AbsoluteDate, ? extends BoundedPropagator>, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.propagation.analytical.AggregateBoundedPropagator: Create a propagator from several constituent propagators.
AggregatedClockModel - Class in org.orekit.time: Offset clock model aggregating several other clock models.
AggregatedClockModel(TimeSpanMap<ClockModel>) - Constructor for class org.orekit.time.AggregatedClockModel: Simple constructor.
AggregatedPVCoordinatesProvider - Class in org.orekit.utils: Aggregate multiple PVCoordinatesProvider instances together.
AggregatedPVCoordinatesProvider(TimeSpanMap<PVCoordinatesProvider>) - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider: Class constructor.
AggregatedPVCoordinatesProvider(TimeSpanMap<PVCoordinatesProvider>, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider: Class constructor.
AggregatedPVCoordinatesProvider.Builder - Class in org.orekit.utils: Builder class for AggregatedPVCoordinatesProvider.
AggregatedPVCoordinatesProvider.InvalidPVProvider - Class in org.orekit.utils: Implementation of PVCoordinatesProvider that throws an OrekitException exception.
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.
AGOM - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey: SGP4-XP solar radiation pressure-like coefficient.
AH - org.orekit.models.earth.weather.SeasonalModelType: ah coefficient model.
AKELLAALFRIEND_2000 - org.orekit.files.ccsds.definitions.PocMethodType: Akella and Alfriend - 2000 method.
ALBEDO_GRID_SIZE - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Albedo grid size.
ALBEDO_MODEL - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Albedo model.
ALFANO_2005 - org.orekit.files.ccsds.definitions.PocMethodType: Alfano 2005 method.
ALFANO_2005 - org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType: Probability of collision computing method described in :"S.
ALFANO_MAX_PROBABILITY - org.orekit.files.ccsds.definitions.PocMethodType: Maximum conjunction probability method from Alfano.
ALFANO_PARAL_2007 - org.orekit.files.ccsds.definitions.PocMethodType: Adjoining parallelepipeds method from Alfano.
ALFANO_TUBES_2007 - org.orekit.files.ccsds.definitions.PocMethodType: Adjoining tubes method from Alfano.
ALFANO_VOXELS_2006 - org.orekit.files.ccsds.definitions.PocMethodType: Voxels method from Alfano.
Alfano2005 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod: Compute the probability of collision using the method described in :"S.
Alfano2005() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005: Empty constructor.
ALFRIEND_1999 - org.orekit.files.ccsds.definitions.PocMethodType: Alfriend 1999 method.
ALFRIEND_1999 - org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType: Probability of collision computing method described in :"Kyle Alfriend, Maruthi Akella, Joseph Frisbee, James Foster, Deok-Jin Lee, and Matthew Wilkins.
ALFRIEND_1999_MAX - org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType: Probability of collision computing method described in :"Kyle Alfriend, Maruthi Akella, Joseph Frisbee, James Foster, Deok-Jin Lee, and Matthew Wilkins.
Alfriend1999 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod: Compute the probability of collision using the method described in : "Kyle Alfriend, Maruthi Akella, Joseph Frisbee, James Foster, Deok-Jin Lee, and Matthew Wilkins.
Alfriend1999() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999: Empty constructor.
Alfriend1999Max - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod: Compute the probability of collision assuming the worst case described in : "Kyle Alfriend, Maruthi Akella, Joseph Frisbee, James Foster, Deok-Jin Lee, and Matthew Wilkins.
Alfriend1999Max() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max: Empty constructor.
alias(String) - Method in class org.orekit.utils.units.Unit: Create an alias for a unit.
AlignedAndConstrained - Class in org.orekit.attitudes: Attitude provider with one satellite vector aligned and another one constrained to two targets.
AlignedAndConstrained(Vector3D, TargetProvider, Vector3D, TargetProvider, Frame, ExtendedPositionProvider, OneAxisEllipsoid) - Constructor for class org.orekit.attitudes.AlignedAndConstrained: Simple constructor.
AlignedAndConstrained(Vector3D, TargetProvider, Vector3D, TargetProvider, ExtendedPositionProvider, OneAxisEllipsoid) - Constructor for class org.orekit.attitudes.AlignedAndConstrained: Constructor with default inertial frame.
AlignmentDetector - Class in org.orekit.propagation.events: Finder for satellite/body alignment events in orbital plane.
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.
AlignmentDetector(Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector: Build a new alignment detector.
AlignmentDetector(EventDetectionSettings, EventHandler, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector: Protected constructor with full parameters.
AlignmentDetector(EventDetectionSettings, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector: Build a new alignment detector.
ALL_VECTORS - org.orekit.files.iirv.IIRVMessage.IncludeMessageMetadata: Include message metadata fields from all vectors in a given IIRV message file.
allowedNextParsers(T) - Method in interface org.orekit.files.sinex.LineParser: Get allowed next line parsers.
ALMOST_CRITICALLY_INCLINED_ORBIT - org.orekit.errors.OrekitMessages: ALMOST_CRITICALLY_INCLINED_ORBIT.
ALMOST_EQUATORIAL_ORBIT - org.orekit.errors.OrekitMessages: ALMOST_EQUATORIAL_ORBIT.
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.
ALT_COV_REF_FRAME - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey: Name of the reference frame in which the alternate covariance data are given.
ALT_COV_TYPE - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey: Flag indicating the type of alternate covariance information provided.
AltCovarianceType - Enum in org.orekit.files.ccsds.ndm.cdm: Flag indicating the type of alternate covariance information provided.
ALTERNATE_NAMES - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey: Alternate names fir this space object.
ALTITUDE_BELOW_ALLOWED_THRESHOLD - org.orekit.errors.OrekitMessages: ALTITUDE_BELOW_ALLOWED_THRESHOLD.
AltitudeDetector - Class in org.orekit.propagation.events: Finder for satellite altitude crossing events.
AltitudeDetector(double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector: Build a new altitude detector.
AltitudeDetector(double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector: Build a new altitude detector.
AltitudeDetector(EventDetectionSettings, EventHandler, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector: Protected constructor with full parameters.
AmbiguityAcceptance - Interface in org.orekit.estimation.measurements.gnss: Interface defining ambiguity acceptance tests.
AmbiguityCache - Class in org.orekit.estimation.measurements.gnss: Cache for AmbiguityDriver.
AmbiguityCache() - Constructor for class org.orekit.estimation.measurements.gnss.AmbiguityCache: Simple constructor.
AmbiguityDriver - Class in org.orekit.estimation.measurements.gnss: Specialized ParameterDriver for ambiguity.
AmbiguityDriver(String, String, double) - Constructor for class org.orekit.estimation.measurements.gnss.AmbiguityDriver: Simple constructor.
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.
AnalyticalSolarPositionProvider - Class in org.orekit.bodies: Class computing low-fidelity positions for the Sun.
AnalyticalSolarPositionProvider() - Constructor for class org.orekit.bodies.AnalyticalSolarPositionProvider: Constructor with default data context.
AnalyticalSolarPositionProvider(DataContext) - Constructor for class org.orekit.bodies.AnalyticalSolarPositionProvider: Constructor.
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.
andCombine(Collection<? extends FieldEventDetector<T>>) - Static method in class org.orekit.propagation.events.FieldBooleanDetector: Create a new event detector that is the logical AND of the given event detectors.
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(FieldEventDetector<T>...) - Static method in class org.orekit.propagation.events.FieldBooleanDetector: Create a new event detector that is the logical AND of the given event detectors.
ANGLE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType: Angles.
ANGLE_1 - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Rotation about first axis.
ANGLE_1 - org.orekit.files.ccsds.ndm.adm.apm.EulerKey: First body rotation angle entry.
ANGLE_1 - org.orekit.files.ccsds.ndm.tdm.ObservationType: Data: ANGLE_1 in degrees and in [-180, +360[ [deg].
ANGLE_1_DOT - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Rotation about first axis.
ANGLE_1_DOT - org.orekit.files.ccsds.ndm.adm.apm.EulerKey: First body rotation rate entry.
ANGLE_2 - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Rotation about second axis.
ANGLE_2 - org.orekit.files.ccsds.ndm.adm.apm.EulerKey: Second body rotation angle entry.
ANGLE_2 - org.orekit.files.ccsds.ndm.tdm.ObservationType: Data: ANGLE_2 in degrees and in [-180, +360[ [deg].
ANGLE_2_DOT - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Rotation about second axis.
ANGLE_2_DOT - org.orekit.files.ccsds.ndm.adm.apm.EulerKey: Second body rotation rate entry.
ANGLE_3 - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Rotation about third axis.
ANGLE_3 - org.orekit.files.ccsds.ndm.adm.apm.EulerKey: Third body rotation angle entry.
ANGLE_3_DOT - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Rotation about third axis.
ANGLE_3_DOT - org.orekit.files.ccsds.ndm.adm.apm.EulerKey: Third body rotation rate entry.
ANGLE_ANGVEL - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType: Angles and angular velocities.
ANGLE_GYROBIAS - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType: Angles and gyro biases.
ANGLE_TYPE - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Angle type entry.
ANGLE_TYPE_NOT_SUPPORTED - org.orekit.errors.OrekitMessages: ANGLE_TYPE_NOT_SUPPORTED.
angles(FieldSpacecraftState<T>) - Method in class org.orekit.utils.OccultationEngine: Compute the occultation angles as seen from a spacecraft.
angles(SpacecraftState) - Method in class org.orekit.utils.OccultationEngine: Compute the occultation angles as seen from a spacecraft.
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(FieldRotation) - Constructor for class org.orekit.utils.AngularCoordinates: Builds a AngularCoordinates from a FieldRotation<Derivative>.
AngularCoordinates(Rotation) - Constructor for class org.orekit.utils.AngularCoordinates: Builds angular coordinates with the given rotation, zero angular velocity, and zero angular acceleration.
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) - Constructor for class org.orekit.utils.AngularCoordinates: Build one of the rotations that transform one pv coordinates into another one.
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.
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 a 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 tropospheric 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(EventDetectionSettings, EventHandler, PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationDetector: Protected constructor with full parameters.
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(EventDetectionSettings, EventHandler, PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector: Protected constructor with full parameters.
AngularSeparationFromSatelliteDetector(PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector: Build a new angular detachment detector.
AngularVelocity - Class in org.orekit.files.ccsds.ndm.adm.apm: Container for Attitude Parameter Message data lines.
AngularVelocity() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity: Simple constructor.
AngularVelocityKey - Enum in org.orekit.files.ccsds.ndm.adm.apm: Keys for APM angular velocity entries.
angVel - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Angular velocity sub-sub-section.
ANGVEL - org.orekit.files.ccsds.ndm.adm.acm.RateElementsType: Angular velocity.
ANGVEL_FRAME - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey: Reference frame for angular velocities.
ANGVEL_FRAME - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey: Frame in which angular velocity is defined.
ANGVEL_X - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Angular velocity about X axis.
ANGVEL_X - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey: Angular velocity around X axis.
ANGVEL_Y - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Angular velocity about Y axis.
ANGVEL_Y - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey: Angular velocity around Y axis.
ANGVEL_Z - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Angular velocity about Z axis.
ANGVEL_Z - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey: Angular velocity around Z axis.
ANT_NB_TYPE - org.orekit.files.rinex.section.RinexLabels: Antenna number and type.
Antenna - Class in org.orekit.gnss.antenna: GNSS antenna model.
Antenna(String, String, Map<RadioWave, FrequencyPattern>) - Constructor for class org.orekit.gnss.antenna.Antenna: Simple constructor.
ANTENNA_B_SIGHT_XYZ - org.orekit.files.rinex.section.RinexLabels: Antenna bore sight.
ANTENNA_DELTA_H_E_N - org.orekit.files.rinex.section.RinexLabels: Antenna reference point.
ANTENNA_DELTA_X_Y_Z - org.orekit.files.rinex.section.RinexLabels: Antenna reference point.
ANTENNA_PHASE_CENTER - org.orekit.files.rinex.section.RinexLabels: Antenna phase center.
ANTENNA_ZERODIR_AZI - org.orekit.files.rinex.section.RinexLabels: Antenna zero direction.
ANTENNA_ZERODIR_XYZ - org.orekit.files.rinex.section.RinexLabels: Antenna zero direction.
AntennaKey - Class in org.orekit.files.sinex: Key for antenna.
AntennaKey(String, String, String) - Constructor for class org.orekit.files.sinex.AntennaKey: 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 a DataProvidersManager.
AntexLoader(DataSource, TimeScale) - Constructor for class org.orekit.gnss.antenna.AntexLoader: Construct a loader by specifying the source of ANTEX auxiliary data files.
ANTICIPATED - org.orekit.files.ccsds.ndm.odm.ocm.ManBasis: Non-cooperative future maneuver that is anticipated (i.e. likely) to occur.
anticipateNext(ProcessingState) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser: Anticipate what next processing state should be.
ANY_PRN - Static variable in class org.orekit.gnss.SatInSystem: Value representing all PRNs in the system.
ANY_SERIAL_NUMBER - Static variable in class org.orekit.files.sinex.AntennaKey: Constant matching any serial numbers.
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(AdmHeader, 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, AbsoluteDate, ApmQuaternion, Euler, AngularVelocity, SpinStabilized, Inertia) - 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, Function<ParseToken, List<ParseToken>>[]) - 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.
APOAPSIS_ALTITUDE - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey: The distance of the furthest point in the objects orbit above the equatorial radius of the central body.
AppliedDCBS - Class in org.orekit.files.rinex: Corrections of Differential Code Biases (DCBs) applied.
AppliedDCBS(SatelliteSystem, String, String) - Constructor for class org.orekit.files.rinex.AppliedDCBS: Simple constructor.
AppliedPCVS - Class in org.orekit.files.rinex: Corrections of antenna phase center variations (PCVs) applied.
AppliedPCVS(SatelliteSystem, String, String) - Constructor for class org.orekit.files.rinex.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(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.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(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.
applyDynamicOutlierFilter(EstimatedMeasurement<T>, RealMatrix) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil: Set and apply a dynamic outlier filter on a measurement.
applyRelevantFilters(DataSource) - Method in class org.orekit.data.FiltersManager: Apply all the relevant data filters, taking care of layers.
applyResetters(FieldSpacecraftState<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers: Apply resetters.
applyResetters(SpacecraftState) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers: Apply resetters.
applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates: 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(PVCoordinates) - 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(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates: Apply the rotation to a pv coordinates.
applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates: Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.AngularCoordinates: Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates: Apply the rotation to a pv coordinates.
APPROACH_ANGLE - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey: The approach angle computed between Objects 1 and 2 in the RTN coordinate frame relative to object 1.
APPROX_POSITION_XYZ - org.orekit.files.rinex.section.RinexLabels: Approximative position.
approximateAsPolynomialOnly(int, AbsoluteDate, int, int, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic: Approximate an already fitted model to polynomial only terms.
APRIL - org.orekit.time.Month: April.
ApsideDetectionAdaptableIntervalFactory - Class in org.orekit.propagation.events.intervals: Factory class for AdaptableInterval suitable for apside detection on eccentric orbits.
ApsideDetector - Class in org.orekit.propagation.events: Finder for apside crossing events.
ApsideDetector(double) - 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.
ApsideDetector(Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector: Build a new instance.
ApsideDetector(EventDetectionSettings, EventHandler) - Constructor for class org.orekit.propagation.events.ApsideDetector: Public constructor with full parameters.
AR - org.orekit.files.rinex.clock.RinexClock.ClockDataType: Data analysis for receiver clocks.
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 - org.orekit.data.PolynomialParser.Unit: Arc-seconds angles.
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.
AREA_ALONG_OEB_INT - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey: Cross-sectional area of Optimally Enclosing Box when viewed along the intermediate OEB direction.
AREA_ALONG_OEB_INT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Cross-sectional area of Optimally Enclosing Box along Y-OEB.
AREA_ALONG_OEB_MAX - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey: Cross-sectional area of Optimally Enclosing Box when viewed along the maximum OEB direction.
AREA_ALONG_OEB_MAX - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Cross-sectional area of Optimally Enclosing Box along X-OEB.
AREA_ALONG_OEB_MIN - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey: Cross-sectional area of Optimally Enclosing Box when viewed along the minimum OEB direction.
AREA_ALONG_OEB_MIN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Cross-sectional area of Optimally Enclosing Box along Z-OEB.
AREA_DRG - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey: The effective area of the object exposed to atmospheric drag.
AREA_MAX_FOR_PC - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Maximum cross-sectional area for collision probability estimation purposes.
AREA_MIN_FOR_PC - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Minimum cross-sectional area for collision probability estimation purposes.
AREA_PC - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey: The actual area of the object.
AREA_PC_MAX - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey: Maximum area (or cross-section) of the object to be used in the calculation of the probability of collision.
AREA_PC_MIN - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey: Minimum area (or cross-section) of the object to be used in the calculation of the probability of collision.
AREA_SRP - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey: The effective area of the object exposed to solar radiation pressure.
AREA_TYP_FOR_PC - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Typical (50th percentile) cross-sectional area for collision probability estimation purposes.
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.
ARG_OF_PERICENTER - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey: Orbit argument of pericenter.
ARGUMENT_OF_PERIGEE - Static variable in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Name for argument of perigee parameter.
AS - org.orekit.files.rinex.clock.RinexClock.ClockDataType: Data analysis for satellite clocks.
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.
AskneNordiusModel - Class in org.orekit.models.earth.troposphere: The Askne Nordius model.
AskneNordiusModel(TroposphereMappingFunction) - Constructor for class org.orekit.models.earth.troposphere.AskneNordiusModel: Create a new Askne Nordius model.
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.
AST - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment: Autonomous Star Tracker.
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.
ATMOSPHERIC_MODEL - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey: Name of atmospheric model.
ATMOSPHERIC_MODEL - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Name of atmospheric model.
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.
att - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey: Trajectory state time history section.
ATT - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey: Attitude state time history section.
ATT - org.orekit.files.ccsds.ndm.adm.acm.AcmElements: Attitude state time history.
ATT_ACTUATOR_TYPE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Type of actuator for attitude control.
ATT_BASIS - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey: Basis of this attitude state time history data.
ATT_BASIS_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey: Identification number of the attitude determination or simulation upon which this attitude is based.
ATT_CONTROL - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Accuracy of attitude control.
ATT_CONTROL_MODE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Attitude control mode.
ATT_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey: Attitude identification number.
ATT_KNOWLEDGE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Accuracy of attitude knowledge.
ATT_LINE - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.Acm: Attitude line element for XML messages.
ATT_POINTING - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Overall accuracy of spacecraft to maintain attitude.
ATT_PREV_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey: Identification number of previous attitude.
ATT_TYPE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey: Attitude element set type.
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.
ATTEMPT_TO_GENERATE_MALFORMED_FILE - org.orekit.errors.OrekitMessages: ATTEMPT_TO_GENERATE_MALFORMED_FILE.
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, Rotation, Vector3D, Vector3D) - 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_DIR - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey: Rotation direction entry.
ATTITUDE_POINTING_LAW_DOES_NOT_POINT_TO_GROUND - org.orekit.errors.OrekitMessages: ATTITUDE_POINTING_LAW_DOES_NOT_POINT_TO_GROUND.
ATTITUDE_SOURCE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey: Source of attitude estimate.
ATTITUDE_STATES - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey: Attitude states.
ATTITUDE_TYPE - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey: Format of the data line entry.
AttitudeBuilder - Interface in org.orekit.attitudes: This interface represents a builder for attitude.
AttitudeCovariance - Class in org.orekit.files.ccsds.ndm.adm.acm: Covariance entry.
AttitudeCovariance(AttitudeCovarianceType, AbsoluteDate, String[], int) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovariance: Simple constructor.
AttitudeCovarianceHistory - Class in org.orekit.files.ccsds.ndm.adm.acm: Covariance history.
AttitudeCovarianceHistory(AttitudeCovarianceHistoryMetadata, List<AttitudeCovariance>) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistory: Simple constructor.
AttitudeCovarianceHistoryMetadata - Class in org.orekit.files.ccsds.ndm.adm.acm: Metadata for covariance history.
AttitudeCovarianceHistoryMetadata() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata: Empty constructor.
AttitudeCovarianceHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.acm: Keys for covariance history container entries.
AttitudeCovarianceType - Enum in org.orekit.files.ccsds.ndm.adm.acm: Attitude covariance set type used in CCSDS Attitude Comprehensive Messages.
AttitudeDetermination - Class in org.orekit.files.ccsds.ndm.adm.acm: Attitude determination data.
AttitudeDetermination() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination: Simple constructor.
AttitudeDeterminationKey - Enum in org.orekit.files.ccsds.ndm.adm.acm: Keys for attitude determination data entries.
AttitudeDeterminationSensor - Class in org.orekit.files.ccsds.ndm.adm.acm: Attitude determination sensor data.
AttitudeDeterminationSensor() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor: Simple constructor.
AttitudeDeterminationSensorKey - Enum in org.orekit.files.ccsds.ndm.adm.acm: Keys for attitude determination data sensor entries.
AttitudeElementsType - Enum in org.orekit.files.ccsds.ndm.adm.acm: Attitude element set type used in CCSDS Attitude Comprehensive Messages.
AttitudeEndpoints - Class in org.orekit.files.ccsds.ndm.adm: Endpoints for attitude definition.
AttitudeEndpoints() - Constructor for class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints: Empty constructor.
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.
AttitudeInterpolator - Class in org.orekit.attitudes: Class for attitude interpolation.
AttitudeInterpolator(Frame, TimeInterpolator<TimeStampedAngularCoordinates>) - Constructor for class org.orekit.attitudes.AttitudeInterpolator: Constructor.
AttitudeManeuver - Class in org.orekit.files.ccsds.ndm.adm.acm: Maneuver entry.
AttitudeManeuver() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver: Build an uninitialized maneuver.
AttitudeManeuverKey - Enum in org.orekit.files.ccsds.ndm.adm.acm: Keys for attitude maneuver entries.
AttitudePhysicalProperties - Class in org.orekit.files.ccsds.ndm.adm.acm: Spacecraft physical properties.
AttitudePhysicalProperties() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties: Simple constructor.
AttitudePhysicalPropertiesKey - Enum in org.orekit.files.ccsds.ndm.adm.acm: Keys for physical properties data entries.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.FieldGnssPropagatorBuilder: Sets the attitude provider.
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.
AttitudeProvider - Interface in org.orekit.attitudes: This interface represents an attitude provider model set.
AttitudeProviderModifier - Interface in org.orekit.attitudes: This interface represents an attitude provider that modifies/wraps another underlying provider.
AttitudeRotationModel - Interface in org.orekit.attitudes: Interface for (attitude) rotation models taking as inputs a spacecraft state and model parameters.
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.Switch - Class in org.orekit.attitudes: Switch specification.
AttitudesSwitcher - Class in org.orekit.attitudes: This classes manages a sequence of different attitude providers that are activated in turn according to switching events.
AttitudesSwitcher() - Constructor for class org.orekit.attitudes.AttitudesSwitcher: Constructor for an initially empty sequence.
AttitudesSwitcher.InstantaneousSwitch - Class in org.orekit.attitudes: Switch specification.
AttitudeState - Class in org.orekit.files.ccsds.ndm.adm.acm: Attitude state entry.
AttitudeState(AttitudeElementsType, RateElementsType, AbsoluteDate, String[], int) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState: Simple constructor.
AttitudeStateHistory - Class in org.orekit.files.ccsds.ndm.adm.acm: Attitude state history.
AttitudeStateHistory(AttitudeStateHistoryMetadata, List<AttitudeState>) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory: Simple constructor.
AttitudeStateHistoryMetadata - Class in org.orekit.files.ccsds.ndm.adm.acm: Metadata for attitude state history.
AttitudeStateHistoryMetadata() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata: Simple constructor.
AttitudeStateHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.acm: Keys for attitude state history container entries.
AttitudeSwitchHandler - 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, AdmHeader, AemMetadata, FileFormat, String, double, 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.
AttitudeWriter(AemWriter, AdmHeader, AemMetadata, FileFormat, String, double, int, Formatter) - 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.
ATTOSECOND - Static variable in class org.orekit.time.TimeOffset: Split time representing 1 attosecond.
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.AbstractBodyAttraction: Suffix for parameter name for attraction coefficient enabling Jacobian processing.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.DeSitterRelativity: Suffix for parameter name for attraction coefficient enabling Jacobian processing.
AUGUST - org.orekit.time.Month: August.
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.
AVERAGE - org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel: Average level of activity.
AveragedCircularWithMeanAngle - Class in org.orekit.propagation.conversion.averaging.elements: Immutable class containing values of averaged circular elements from any applicable theory (with MEAN as PositionAngleType).
AveragedCircularWithMeanAngle(double, double, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle: Constructor.
AveragedEquinoctialWithMeanAngle - Class in org.orekit.propagation.conversion.averaging.elements: Immutable class containing values of averaged equinoctial elements from any applicable theory (with MEAN as PositionAngleType).
AveragedEquinoctialWithMeanAngle(double, double, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle: Constructor.
AveragedKeplerianWithMeanAngle - Class in org.orekit.propagation.conversion.averaging.elements: Immutable class containing values of averaged Keplerian elements from any applicable theory (with MEAN as PositionAngleType).
AveragedKeplerianWithMeanAngle(double, double, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle: Constructor.
AveragedOrbitalElements - Interface in org.orekit.propagation.conversion.averaging.elements: Interface for storing averaged orbital elements.
AveragedOrbitalState - Interface in org.orekit.propagation.conversion.averaging: Interface representing averaged orbital elements at a specific instant.
AVG_MANEUVER_FREQ - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Average number of orbit or attitude maneuvers per year.
AW - org.orekit.models.earth.weather.SeasonalModelType: aw coefficient model.
AZEL - org.orekit.files.ccsds.ndm.tdm.AngleType: Azimuth, elevation.
AzimuthalGradientCoefficients - Class in org.orekit.models.earth.troposphere: Container for the azimuthal gradient coefficients gn_h, ge_h, gn_w and ge_w.
AzimuthalGradientCoefficients(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.AzimuthalGradientCoefficients: Simple constructor.
AzimuthalGradientProvider - Interface in org.orekit.models.earth.troposphere: Provider for AzimuthalGradientCoefficients and FieldAzimuthalGradientCoefficients.
azimuthBetweenPoints(FieldGeodeticPoint<T>, FieldGeodeticPoint<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid: Compute the azimuth angle from local north between the two points.
azimuthBetweenPoints(GeodeticPoint, GeodeticPoint) - Method in class org.orekit.bodies.OneAxisEllipsoid: Compute the azimuth angle from local north between the two points.

B

B - org.orekit.gnss.SignalCode: Galileo B I/NAV and B C/NAV / IRNSS B RS / GLONASS L1OCp and LO2Cp codes.
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.
B01 - org.orekit.gnss.PredefinedGnssSignal: Beidou B1 (1561.098 MHz).
B02 - org.orekit.gnss.PredefinedGnssSignal: Beidou B2 (1207.14 MHz).
B03 - org.orekit.gnss.PredefinedGnssSignal: Beidou B3 (1268.52 MHz).
B08 - org.orekit.gnss.PredefinedGnssSignal: Beidou B2 (B2a + B2b) (1191.795MHz).
B1A - org.orekit.gnss.PredefinedGnssSignal: Beidou B1A (1575.42 MHz).
B1C - org.orekit.gnss.PredefinedGnssSignal: Beidou B1C (1575.42 MHz).
B2A - org.orekit.gnss.PredefinedGnssSignal: Beidou B2a (1176.45 MHz).
B2A - Static variable in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints: Constant for A ← B direction.
B2B - org.orekit.gnss.PredefinedGnssSignal: Beidou B2b (1207.14 MHz).
B3A - org.orekit.gnss.PredefinedGnssSignal: Beidou B3A (1268.52 MHz).
BACKUP - org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus: Backup object.
backwardsSmooth() - Method in class org.orekit.estimation.sequential.RtsSmoother
BAR - Static variable in class org.orekit.utils.units.Unit: Bar unit.
BaseConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration: Empty constructor.
BaseRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Base class modifying theoretical range measurement with ionospheric delay.
BaseRangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier: Constructor.
BaseRangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Base class modifying theoretical range-rate measurement with ionospheric delay.
BaseRangeRateIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier: Constructor.
BaseRangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Baselass modifying theoretical range-rate measurements with tropospheric delay.
BaseRangeRateTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier: Constructor.
BaseRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Base class modifying theoretical range measurements with tropospheric delay.
BaseRangeTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier: Constructor.
BASIC - org.orekit.gnss.metric.ntrip.Authentication: Basic.
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.
BasicConstantThrustPropulsionModel(double, double, Vector3D, Control3DVectorCostType, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Generic 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: Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Propagate an orbit without any fancy features.
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.
BATCH - org.orekit.files.ccsds.definitions.AdMethodType: Batch least squares.
BatchLSEstimator - Class in org.orekit.estimation.leastsquares: Least squares estimator for orbit determination.
BatchLSEstimator(LeastSquaresOptimizer, PropagatorBuilder...) - 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(PropagatorBuilder[], 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.
BCT - org.orekit.files.sp3.SP3OrbitType: broadcast.
BDS - org.orekit.files.rinex.navigation.IonosphericCorrectionType: Beidou α/β.
BDS - org.orekit.gnss.metric.ntrip.NavigationSystem: Beidou.
BDSBAS - org.orekit.files.rinex.navigation.SbasId: BeiDou Satellite-based Augmentation System.
BDT - org.orekit.gnss.ObservationTimeScale: Beidou time scale.
BDTScale - Class in org.orekit.time: Beidou system time scale.
beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Method called just before integration.
beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: 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.
BEIDOU - org.orekit.gnss.SatelliteSystem: Beidou system.
BEIDOU - org.orekit.gnss.TimeSystem: Beidou.
BEIDOU - org.orekit.time.GNSSDate.GNSSDateType: BeiDou.
BEIDOU_2G - org.orekit.gnss.antenna.SatelliteType: BeiDou-2 GEO.
BEIDOU_2I - org.orekit.gnss.antenna.SatelliteType: BeiDou-2 IGSO.
BEIDOU_2M - org.orekit.gnss.antenna.SatelliteType: BeiDou-2 MEO.
BEIDOU_3G_CAST - org.orekit.gnss.antenna.SatelliteType: BeiDou-3.
BEIDOU_3I - org.orekit.gnss.antenna.SatelliteType: BeiDou-3 IGSO.
BEIDOU_3M_CAST - org.orekit.gnss.antenna.SatelliteType: BeiDou-3.
BEIDOU_3M_SECM - org.orekit.gnss.antenna.SatelliteType: BeiDou-3.
BEIDOU_3SI_CAST - org.orekit.gnss.antenna.SatelliteType: BeiDou-3.
BEIDOU_3SI_SECM - org.orekit.gnss.antenna.SatelliteType: BeiDou-3.
BEIDOU_3SM_CAST - org.orekit.gnss.antenna.SatelliteType: BeiDou-3.
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(FieldBeidouAlmanac<T>) - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac: Constructor from field instance.
BeidouAlmanac(TimeScales, SatelliteSystem) - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac: Build a new almanac.
BeidouCivilianNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a Beidou civilian navigation message.
BeidouCivilianNavigationMessage(RadioWave, TimeScales, SatelliteSystem) - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Constructor.
BeidouCivilianNavigationMessage(FieldBeidouCivilianNavigationMessage<T>) - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Constructor from field instance.
BeidouGeo - Class in org.orekit.gnss.attitude: Attitude providers for Beidou geostationary orbit navigation satellites.
BeidouGeo(AbsoluteDate, AbsoluteDate, ExtendedPositionProvider, 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, ExtendedPositionProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouIGSO: Simple constructor.
BeidouLegacyNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a BeiDou navigation message.
BeidouLegacyNavigationMessage(FieldBeidouLegacyNavigationMessage<T>) - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage: Constructor from field instance.
BeidouLegacyNavigationMessage(TimeScales, SatelliteSystem) - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage: Constructor.
BeidouMeo - Class in org.orekit.gnss.attitude: Attitude providers for Beidou Medium Earth Orbit navigation satellites.
BeidouMeo(AbsoluteDate, AbsoluteDate, ExtendedPositionProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouMeo: Simple constructor.
BeidouSatelliteType - Enum in org.orekit.propagation.analytical.gnss.data: Enumerate for Beidou satellite type.
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.
BetaAngleDetector - Class in org.orekit.propagation.events: Finder for beta angle crossing events.
BetaAngleDetector(double) - Constructor for class org.orekit.propagation.events.BetaAngleDetector: Solar beta angle constructor.
BetaAngleDetector(double, PVCoordinatesProvider, Frame) - Constructor for class org.orekit.propagation.events.BetaAngleDetector: Class constructor.
BetaAngleDetector(EventDetectionSettings, EventHandler, double, PVCoordinatesProvider, Frame) - Constructor for class org.orekit.propagation.events.BetaAngleDetector: Protected constructor with full parameters.
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.
BiasDescription - Class in org.orekit.files.sinex: Class to store the bias description parameters.
BiasDescription() - Constructor for class org.orekit.files.sinex.BiasDescription: Simple constructor.
BIG_TRUNCATION_TOLERANCE - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Truncation tolerance for big, eccentric orbits.
BINEX - org.orekit.gnss.metric.ntrip.DataFormat: BINEX.
BistaticRange - Class in org.orekit.estimation.measurements: Class modeling a bistatic range measurement using an emitter ground station and a receiver ground station.
BistaticRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.BistaticRange: Simple constructor.
BistaticRangeBuilder - Class in org.orekit.estimation.measurements.generation: Builder for BistaticRange measurements.
BistaticRangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.BistaticRangeBuilder: Simple constructor.
BistaticRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical bistatic range measurement with ionospheric delay.
BistaticRangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeIonosphericDelayModifier: Constructor.
BistaticRangeRate - Class in org.orekit.estimation.measurements: Class modeling a bistatic range rate measurement using an emitter ground station and a receiver ground station.
BistaticRangeRate(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.BistaticRangeRate: Simple constructor.
BistaticRangeRateBuilder - Class in org.orekit.estimation.measurements.generation: Builder for BistaticRangeRate measurements.
BistaticRangeRateBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.BistaticRangeRateBuilder: Simple constructor.
BistaticRangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical bistatic range-rate measurement with ionospheric delay.
BistaticRangeRateIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeRateIonosphericDelayModifier: Constructor.
BistaticRangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical bistatic range-rate measurements with tropospheric delay.
BistaticRangeRateTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeRateTroposphericDelayModifier: Constructor.
BistaticRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical bistatic range measurement with tropospheric delay.
BistaticRangeTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeTroposphericDelayModifier: Constructor.
BIT_1 - org.orekit.gnss.metric.parser.DataType: 1 bit.
BIT_10 - org.orekit.gnss.metric.parser.DataType: 10 bits.
BIT_12 - org.orekit.gnss.metric.parser.DataType: 12 bits.
BIT_2 - org.orekit.gnss.metric.parser.DataType: 2 bits.
BIT_24 - org.orekit.gnss.metric.parser.DataType: 24 bits.
BIT_3 - org.orekit.gnss.metric.parser.DataType: 3 bits.
BIT_32 - org.orekit.gnss.metric.parser.DataType: 32 bits.
BIT_4 - org.orekit.gnss.metric.parser.DataType: 4 bits.
BIT_6 - org.orekit.gnss.metric.parser.DataType: 6 bits.
BIT_7 - org.orekit.gnss.metric.parser.DataType: 7 bits.
BIT_8 - org.orekit.gnss.metric.parser.DataType: 8 bits.
blendArithmeticallyWith(FieldPVCoordinates<T>, T) - Method in class org.orekit.utils.FieldPVCoordinates
blendArithmeticallyWith(PVCoordinates, double) - Method in class org.orekit.utils.PVCoordinates
BLOCK_I - org.orekit.gnss.antenna.SatelliteType: GPS Block I : SVN 01-11.
BLOCK_II - org.orekit.gnss.antenna.SatelliteType: GPS Block II : SVN 13-21.
BLOCK_IIA - org.orekit.gnss.antenna.SatelliteType: GPS Block IIA : SVN 22-40.
BLOCK_IIF - org.orekit.gnss.antenna.SatelliteType: GPS Block IIF : SVN 62-73.
BLOCK_IIIA - org.orekit.gnss.antenna.SatelliteType: GPS Block IIIA : SVN 74-81.
BLOCK_IIR_A - org.orekit.gnss.antenna.SatelliteType: GPS Block IIR : SVN 41, 43-46, 51, 54, 56.
BLOCK_IIR_B - org.orekit.gnss.antenna.SatelliteType: GPS Block IIR : SVN 47, 59-61.
BLOCK_IIR_M - org.orekit.gnss.antenna.SatelliteType: GPS Block IIR-M : SVN 48-50, 52-53, 55, 57-58.
BlockWriter() - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter.BlockWriter: Empty 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.
body - org.orekit.files.ccsds.section.XmlStructureKey: Body structure.
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.
BooleanDetector(List<EventDetector>, BooleanDetector.Operator, EventDetectionSettings, EventHandler) - Constructor for class org.orekit.propagation.events.BooleanDetector: Protected constructor with all the parameters.
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.
BoundedCartesianEnergy - Class in org.orekit.control.indirect.adjoint.cost: Class for bounded energy cost with Cartesian coordinates.
BoundedCartesianEnergy(String, double, double) - Constructor for class org.orekit.control.indirect.adjoint.cost.BoundedCartesianEnergy: Constructor.
BoundedCartesianEnergy(String, double, double, EventDetectionSettings) - Constructor for class org.orekit.control.indirect.adjoint.cost.BoundedCartesianEnergy: Constructor.
BoundedPropagator - Interface in org.orekit.propagation: This interface is intended for ephemerides valid only during a time range.
BOX - org.orekit.files.ccsds.ndm.cdm.ScreenVolumeShape: Box.
BoxAndSolarArraySpacecraft - Class in org.orekit.forces: Class representing the features of a classical satellite with a convex body shape.
BoxAndSolarArraySpacecraft(double, double, double, ExtendedPositionProvider, double, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft: Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(List<Panel>) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft: Build a spacecraft model.
BrouwerLyddaneOrbitalState - Class in org.orekit.propagation.conversion.averaging: Class representing an averaged orbital state as in the Brouwer-Lyddane theory.
BrouwerLyddaneOrbitalState(AbsoluteDate, AveragedKeplerianWithMeanAngle, Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.averaging.BrouwerLyddaneOrbitalState: Constructor.
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, 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, 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, double, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Build a propagator from orbit, mass 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, 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, AttitudeProvider, double, double, double, double, double, double, double, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Build a propagator from orbit, attitude provider, mass and potential.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, PropagationType, double, double, int) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Build a propagator from orbit, attitude provider, mass and potential.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, PropagationType, double, OsculatingToMeanConverter) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Build a propagator from orbit, attitude provider, mass 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, 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, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Build a propagator from orbit, attitude provider and potential provider.
BrouwerLyddanePropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Build a propagator from orbit and potential provider.
BrouwerLyddanePropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Build a propagator from orbit and potential provider.
BrouwerLyddanePropagatorBuilder - Class in org.orekit.propagation.conversion: Builder for Brouwer-Lyddane propagator.
BrouwerLyddanePropagatorBuilder(Orbit, double, double, TideSystem, double, double, double, double, OrbitType, PositionAngleType, double, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder: Build a new instance.
BrouwerLyddanePropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngleType, double, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder: Build a new instance.
BrouwerLyddanePropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngleType, double, AttitudeProvider, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder: Build a new instance.
BrouwerLyddaneTheory - Class in org.orekit.propagation.conversion.osc2mean: Brouwer-Lyddane theory for osculating to mean orbit conversion.
BrouwerLyddaneTheory(double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.osc2mean.BrouwerLyddaneTheory: Constructor.
BrouwerLyddaneTheory(UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.conversion.osc2mean.BrouwerLyddaneTheory: Constructor.
BSTAR - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey: SGP/SGP4 drag-like coefficient.
BTERM - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey: SGP4-XP drag-like coefficient.
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.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder: Construct a SemiAnalyticalUnscentedKalmanEstimator from the data in this builder.
build() - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder: Construct a UnscentedKalmanEstimator from the data in this builder.
build() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser: Build the file from parsed entries.
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() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser: Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.NdmParser: Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Build the file from parsed entries.
build() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser: Build the file from parsed entries.
build() - Method in class org.orekit.files.sinex.ParseInfo: Build the parsed file.
build() - Method in class org.orekit.files.sinex.SinexBiasParseInfo: Build the parsed file.
build() - Method in class org.orekit.files.sinex.SinexParseInfo: Build the parsed file.
build() - Method in class org.orekit.propagation.analytical.gnss.FieldGnssPropagatorBuilder: Finalizes the build.
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.
build() - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder: Build the aggregated PVCoordinatesProvider.
build() - Method in class org.orekit.utils.WaypointPVBuilder: Build a PVCoordinatesProvider from the waypoints added to this builder.
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(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in interface org.orekit.attitudes.AttitudeBuilder: Build a filtered attitude.
build(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in class org.orekit.attitudes.FixedFrameBuilder: Build a filtered attitude.
build(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints: Build a filtered attitude.
build(Frame, PVCoordinatesProvider, TimeStampedAngularCoordinates) - 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, PVCoordinatesProvider, TimeStampedAngularCoordinates) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints: Build a filtered attitude.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder: Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder: Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder: Generate a single measurement.
build(AbsoluteDate, SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder: Generate a single measurement.
buildAcmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder: Build a parser for Attitude Comprehensive Messages.
buildAcmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder: Build a writer for Attitude Comprehensive Messages.
buildAdditionalDerivativesProvider() - Method in interface org.orekit.control.indirect.shooting.propagation.AdjointDynamicsProvider: Builds adjoint derivatives provider.
buildAdditionalDerivativesProvider() - Method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProvider: Builds adjoint derivatives provider.
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, ExtendedPositionProvider, Frame, int) - Method in enum org.orekit.gnss.antenna.SatelliteType: Build an attitude provider suitable for this satellite type.
buildBasicGradientSpacecraftState(SpacecraftState, int, AttitudeProvider) - Static method in class org.orekit.propagation.integration.AbstractGradientConverter: Process a state into a Gradient version without force model parameter.
buildBoundedEnergyProvider(String, double, double, EventDetectionSettings, CartesianAdjointEquationTerm...) - Static method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProviderFactory: Method building a provider with bounded Cartesian energy as cost.
buildBoundedFuelCostProvider(String, double, double, EventDetectionSettings, CartesianAdjointEquationTerm...) - Static method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProviderFactory: Method building a provider with bounded Cartesian fuel as cost.
buildBox(double, double, double, double, double, double, double) - Static method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Build the panels of a simple parallelepipedic box.
buildCdmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder: Build a parser for Conjunction Data Messages.
buildCdmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder: Build a writer for Conjunction Data Messages.
buildEphemerisFile(List<C>) - Method in class org.orekit.files.iirv.IIRVBuilder: Constructs an IIRVEphemerisFile from the inputted list of TimeStampedPVCoordinates, inferring the start year from the first coordinate's AbsoluteDate.
Builder() - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder: Create a builder using the AggregatedPVCoordinatesProvider.InvalidPVProvider as the initial provider.
Builder(PVCoordinatesProvider) - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder: Create a builder using the provided initial provider.
buildFieldAdditionalDerivativesProvider(Field<T>) - Method in interface org.orekit.control.indirect.shooting.propagation.AdjointDynamicsProvider: Builds Field adjoint derivatives provider.
buildFieldAdditionalDerivativesProvider(Field<T>) - Method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProvider: Builds Field adjoint derivatives provider.
buildFieldGradientCartesianVector(T[]) - Static method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm: Build a Cartesian vector whose components are independent variables for automatic differentiation at order 1.
buildFieldIntegrator(FieldSpacecraftState<T>) - Method in class org.orekit.control.indirect.shooting.AbstractIndirectShooting: Create Field integrator.
buildFieldODE(FieldAbsoluteDate<T>) - Method in class org.orekit.control.indirect.shooting.AbstractFixedInitialCartesianSingleShooting: Build Ordinary Differential Equation for Field.
buildFlatArray(Flattener, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Build a coefficients array in flat form.
buildFlightDurationProvider(String, double, double, CartesianAdjointEquationTerm...) - Static method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProviderFactory: Method building a provider with unbounded Cartesian energy and vanishing mass flow as cost.
buildGradientCartesianVector(double[]) - Static method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm: Build a Cartesian vector whose components are independent variables for automatic differentiation at order 1.
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.
buildIIRVMessage(List<C>) - Method in class org.orekit.files.iirv.IIRVBuilder: Constructs an IIRVMessage where each IIRVVector in initialized from the inputted list of TimeStampedPVCoordinates.
buildIntegrator(double[][]) - Method in class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder: Builds an integrator from input absolute and relative tolerances.
buildIntegrator(double[][]) - Method in class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder: Builds an integrator from input absolute and relative tolerances.
buildIntegrator(double[][]) - Method in class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder: Builds an integrator from input absolute and relative tolerances.
buildIntegrator(double[][]) - Method in class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder: Builds an integrator from input absolute and relative tolerances.
buildIntegrator(double[][]) - Method in class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder: Builds an integrator from input absolute and relative tolerances.
buildIntegrator(double[][]) - Method in class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder
buildIntegrator(double[][]) - Method in class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder: Builds an integrator from input absolute and relative tolerances.
buildIntegrator(Field<T>, double[][]) - Method in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder: Build integrator from absolute and relative tolerances.
buildIntegrator(Field<T>, double[][]) - Method in class org.orekit.propagation.conversion.AdamsBashforthFieldIntegratorBuilder: Build integrator from absolute and relative tolerances.
buildIntegrator(Field<T>, double[][]) - Method in class org.orekit.propagation.conversion.AdamsMoultonFieldIntegratorBuilder: Build integrator from absolute and relative tolerances.
buildIntegrator(Field<T>, double[][]) - Method in class org.orekit.propagation.conversion.DormandPrince54FieldIntegratorBuilder: Build integrator from absolute and relative tolerances.
buildIntegrator(Field<T>, double[][]) - Method in class org.orekit.propagation.conversion.DormandPrince853FieldIntegratorBuilder: Build integrator from absolute and relative tolerances.
buildIntegrator(Field<T>, double[][]) - Method in class org.orekit.propagation.conversion.HighamHall54FieldIntegratorBuilder: Build integrator from absolute and relative tolerances.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.FieldAbstractIntegratorBuilder: Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in interface org.orekit.propagation.conversion.FieldExplicitRungeKuttaIntegratorBuilder: Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in interface org.orekit.propagation.conversion.FieldODEIntegratorBuilder: Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder: Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.ClassicalRungeKuttaFieldIntegratorBuilder: Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.EulerFieldIntegratorBuilder: Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.FieldAbstractIntegratorBuilder: Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType, PositionAngleType) - Method in interface org.orekit.propagation.conversion.FieldExplicitRungeKuttaIntegratorBuilder: Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType, PositionAngleType) - Method in interface org.orekit.propagation.conversion.FieldODEIntegratorBuilder: Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.GillFieldIntegratorBuilder: Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.LutherFieldIntegratorBuilder: Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.MidpointFieldIntegratorBuilder: Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.ThreeEighthesFieldIntegratorBuilder: Build a first order integrator.
buildIntegrator(FieldOrbit<T>, OrbitType) - Method in class org.orekit.propagation.conversion.FieldAbstractIntegratorBuilder: Build a first order integrator.
buildIntegrator(FieldOrbit<T>, OrbitType) - Method in interface org.orekit.propagation.conversion.FieldExplicitRungeKuttaIntegratorBuilder: Build a first order integrator.
buildIntegrator(FieldOrbit<T>, OrbitType) - Method in interface org.orekit.propagation.conversion.FieldODEIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AbstractIntegratorBuilder
buildIntegrator(Orbit, OrbitType) - Method in interface org.orekit.propagation.conversion.ExplicitRungeKuttaIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in interface org.orekit.propagation.conversion.ODEIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.AbstractIntegratorBuilder
buildIntegrator(Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.EulerIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType, PositionAngleType) - Method in interface org.orekit.propagation.conversion.ExplicitRungeKuttaIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.GillIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.LutherIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.MidpointIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType, PositionAngleType) - Method in interface org.orekit.propagation.conversion.ODEIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder: Build a first order integrator.
buildIntegrator(AbsolutePVCoordinates) - Method in class org.orekit.propagation.conversion.AbstractIntegratorBuilder
buildIntegrator(AbsolutePVCoordinates) - Method in class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder: Build a first order integrator.
buildIntegrator(AbsolutePVCoordinates) - Method in interface org.orekit.propagation.conversion.ExplicitRungeKuttaIntegratorBuilder: Build a first order integrator.
buildIntegrator(AbsolutePVCoordinates) - Method in interface org.orekit.propagation.conversion.ODEIntegratorBuilder: Build a first order integrator.
buildIntegrator(FieldAbsolutePVCoordinates<T>) - Method in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder: Build a first order integrator.
buildIntegrator(FieldAbsolutePVCoordinates<T>) - Method in class org.orekit.propagation.conversion.FieldAbstractIntegratorBuilder: Build a first order integrator.
buildIntegrator(FieldAbsolutePVCoordinates<T>) - Method in interface org.orekit.propagation.conversion.FieldExplicitRungeKuttaIntegratorBuilder: Build a first order integrator.
buildIntegrator(FieldAbsolutePVCoordinates<T>) - Method in interface org.orekit.propagation.conversion.FieldODEIntegratorBuilder: Build a first order integrator.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder: Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder: Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.EphemerisPropagatorBuilder: Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Build a new batch least squares model.
buildLine1(boolean) - Method in class org.orekit.files.iirv.IIRVVector: Builds the first line of the IIRV vector, not including ASCII carriage returns and line feeds.
buildLine2() - Method in class org.orekit.files.iirv.IIRVVector: Builds the second line of the IIRV vector, not including ASCII carriage returns and line feeds.
buildLine3() - Method in class org.orekit.files.iirv.IIRVVector: Builds the third line of the IIRV vector, not including ASCII carriage returns and line feeds.
buildLine4() - Method in class org.orekit.files.iirv.IIRVVector: Builds the fourth line of the IIRV vector, not including ASCII carriage returns and line feeds.
buildLine5() - Method in class org.orekit.files.iirv.IIRVVector: Builds the fifth line of the IIRV vector, not including ASCII carriage returns and line feeds.
buildLine6() - Method in class org.orekit.files.iirv.IIRVVector: Builds the sixth line of the IIRV vector, not including ASCII carriage returns and line feeds.
buildLogarithmicBarrierFuelCostProvider(String, double, double, double, CartesianAdjointEquationTerm...) - Static method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProviderFactory: Method building a provider with bounded Cartesian fuel penalized with a logarithmic barrier.
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.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.AngularAzElBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.AngularRaDecBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.BistaticRangeBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.BistaticRangeRateBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.FDOABuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesOneWayRangeRateBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesPhaseBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesRangeBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.OneWayGNSSPhaseBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.OneWayGNSSRangeBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.OneWayGNSSRangeRateBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.PositionBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.PVBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.RangeBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.RangeRateBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.TDOABuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.TurnAroundRangeBuilder: Build a dummy observed measurement.
buildObserved(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.gnss.PhaseBuilder: Build a dummy observed measurement.
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.
buildPanels(double, double, double, ExtendedPositionProvider, double, Vector3D, double, double, double, double) - Static method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Build the panels of a simple parallelepiped box plus one solar array panel.
buildParseInfo() - Method in class org.orekit.files.sinex.AbstractSinexParser: Build the container for parsing info.
buildParseInfo() - Method in class org.orekit.files.sinex.SinexBiasParser: Build the container for parsing info.
buildParseInfo() - Method in class org.orekit.files.sinex.SinexParser: Build the container for parsing info.
buildPropagator() - Method in class org.orekit.propagation.conversion.AbstractIntegratedPropagatorBuilder: Build a propagator from current value of selected normalized parameters.
buildPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Build a propagator from current value of selected normalized parameters.
buildPropagator() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Build a propagator from current value of selected normalized parameters.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.AbstractIntegratedPropagatorBuilder: Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Build a propagator.
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.EphemerisPropagatorBuilder: 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.
buildPropagator(SpacecraftState) - Method in class org.orekit.control.indirect.shooting.AbstractFixedInitialCartesianSingleShooting: Create numerical propagator.
buildPropagator(SpacecraftState) - Method in class org.orekit.control.indirect.shooting.AbstractIndirectShooting: Create numerical propagator.
buildQuadraticPenaltyFuelCostProvider(String, double, double, double, EventDetectionSettings, CartesianAdjointEquationTerm...) - Static method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProviderFactory: Method building a provider with bounded Cartesian fuel penalized with a quadratic term.
buildReferenceSlot(O) - Method in class org.orekit.orbits.WalkerConstellation: Create the reference slot, which is satellite 0 in plane 0.
buildRegularSlots(O) - Method in class org.orekit.orbits.WalkerConstellation: Create the regular slots.
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).
buildSlot(WalkerConstellationSlot<O>, int, double) - Method in class org.orekit.orbits.WalkerConstellation: Create one offset slot from an already existing slot.
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, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.ndm.adm.RotationXmlTokenBuilder: Create a list of parse tokens.
buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.MessageVersionXmlTokenBuilder: Create a list of parse tokens.
buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.RegularXmlTokenBuilder: Create a list of parse tokens.
buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.UserDefinedXmlTokenBuilder: Create a list of parse tokens.
buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in interface org.orekit.files.ccsds.utils.lexical.XmlTokenBuilder: Create a list of parse tokens.
buildUnboundedEnergyProvider(String, double, EventDetectionSettings, CartesianAdjointEquationTerm...) - Static method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProviderFactory: Method building a provider with unbounded Cartesian energy as cost.
buildUnboundedEnergyProviderNeglectingMass(String, CartesianAdjointEquationTerm...) - Static method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProviderFactory: Method building a provider with unbounded Cartesian energy and vanishing mass flow as cost.
buildUncachedITRF(EOPHistory, UTCScale) - Static method in class org.orekit.frames.FramesFactory: Build an uncached International Terrestrial Reference Frame with specific EOP history.
buildUncachedITRF(UT1Scale) - Method in class org.orekit.frames.AbstractFrames
buildUncachedITRF(UT1Scale) - Method in interface org.orekit.frames.Frames: Build an uncached International Terrestrial Reference Frame with specific EOP history.
buildVector(DayOfYearTerm, VectorEpochTerm, PositionVectorComponentTerm, PositionVectorComponentTerm, PositionVectorComponentTerm, VelocityVectorComponentTerm, VelocityVectorComponentTerm, VelocityVectorComponentTerm) - Method in class org.orekit.files.iirv.IIRVBuilder: Constructs an IIRV object using the configured parameters.
buildVector(TimeStampedPVCoordinates) - Method in class org.orekit.files.iirv.IIRVBuilder: Constructs an IIRV vector using the configured parameters, with position, velocity, and time variables derived from instances of TimeStampedPVCoordinates and AbsoluteDate.
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.
BUS_MODEL - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Bus model name.
BWLS - org.orekit.files.ccsds.definitions.OdMethodType: Batch Weighted Least Squares.
ByteArrayEncodedMessage - Class in org.orekit.gnss.metric.parser: Encoded message as a byte array.
ByteArrayEncodedMessage(byte[]) - Constructor for class org.orekit.gnss.metric.parser.ByteArrayEncodedMessage: Simple constructor.

C

C - org.orekit.gnss.SignalCode: GPS C/A / GLONASS C/A / Galileo C / SBAS C/A / QZSS C/A / QZSS C/B / IRNSS C RS(P) codes.
C_2FASX4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: C_2FASX4.
C_3FASX6 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: C_3FASX6.
C_FASX2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: C_FASX2.
C_G22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: C_G22.
C_G32 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: C_G32.
C_G44 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: C_G44.
C_G52 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: C_G52.
C_G54 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: C_G54.
C0 - org.orekit.gnss.PredefinedObservationType: Pseudorange for Rinex3.
C01 - org.orekit.gnss.PredefinedGnssSignal: In the ANTEX files, both C01 and C02 refer to Beidou B1 signal (1561.098 MHz).
C02 - org.orekit.gnss.PredefinedGnssSignal: In the ANTEX files, both C01 and C02 refer to Beidou B1 signal (1561.098 MHz).
C05 - org.orekit.gnss.PredefinedGnssSignal: In the ANTEX files, C05 appears without much reference for consistency with Rinex 4 tables, we assume it is B2a (1176.45 MHz).
C06 - org.orekit.gnss.PredefinedGnssSignal: In the ANTEX files, C06 appears without much reference, we assume it is B2 (1207.14 MHz).
C07 - org.orekit.gnss.PredefinedGnssSignal: In the ANTEX files, C07 seems to refer to a signal close to E06, probably B3... (1268.52 MHz).
C08 - org.orekit.gnss.PredefinedGnssSignal: In the ANTEX files, C08 appears without much reference for consistency with Rinex 4 tables, we assume it is B2 (B2a+B2b) (1191.795 MHz).
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.
C1 - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.
C1A - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E1 A / Beidou B1A for Rinex3.
C1B - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E1 I/NAV OS/CS/SoL / QZSS geo signal for Rinex3.
C1C - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.
C1D - org.orekit.gnss.PredefinedObservationType: Pseudorange Beidou B1 Data for Rinex3.
C1E - org.orekit.gnss.PredefinedObservationType: Pseudorange QZSS L1 C/B for Rinex4.
C1I - org.orekit.gnss.PredefinedObservationType: Pseudorange Beidou B1 I for Rinex3.02.
C1L - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3, Beidou B1A for Rinex3.03.
C1L - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: C1L.
C1M - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L1 M for Rinex3.
C1P - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L1 P(AS off) / GLONASS G1 P / Beidou C1 Pilot for Rinex3.
C1Q - org.orekit.gnss.PredefinedObservationType: Pseudorange Beidou B1 Q for Rinex3.02.
C1S - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3, Beidou B1A for Rinex3.03.
C1SS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: C1SS.
C1W - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L1 Z-tracking and similar (AS on) for Rinex3.
C1X - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) / Beidou B1 Data+Pilot for Rinex3.
C1Y - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L1 Y for Rinex3.
C1Z - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3, Beidou B1A for Rinex3.03.
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.
C2 - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L2 / GLONASS G2 / Beidou B02 for Rinex2.
C2C - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L2 C/A / GLONASS G2 C/A for Rinex3.
C2D - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.
C2I - org.orekit.gnss.PredefinedObservationType: Pseudorange Beidou B1 I for Rinex3.03.
C2L - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.
C2M - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L2 M for Rinex3.
C2P - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L2 P(AS off) / GLONASS G2 P for Rinex3.
C2Q - org.orekit.gnss.PredefinedObservationType: Pseudorange Beidou B1 Q for Rinex3.03.
C2S - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.
C2W - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L2 Z-tracking and similar (AS on) for Rinex3.
C2X - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3, Beidou B1 I+Q for Rinex3.03.
C2Y - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L2 Y for Rinex3.
C3I - org.orekit.gnss.PredefinedObservationType: Pseudorange GLONASS G3 I for Rinex3.
C3Q - org.orekit.gnss.PredefinedObservationType: Pseudorange GLONASS G3 Q for Rinex3.
C3X - org.orekit.gnss.PredefinedObservationType: Pseudorange GLONASS G3 I+Q for Rinex3.
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.
C4A - org.orekit.gnss.PredefinedObservationType: Pseudorange GLONASS G1a L1OCd for Rinex3.
C4B - org.orekit.gnss.PredefinedObservationType: Pseudorange GLONASS G1a L1OCp for Rinex3.
C4X - org.orekit.gnss.PredefinedObservationType: Pseudorange GLONASS G1a L1OCd+L1OCd for Rinex3.
C5 - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L5 / Galileo E5a / SBAS L5 for Rinex2.
C5A - org.orekit.gnss.PredefinedObservationType: Pseudorange IRNSS L5 A for Rinex3.
C5B - org.orekit.gnss.PredefinedObservationType: Pseudorange IRNSS L5 B for Rinex3.
C5C - org.orekit.gnss.PredefinedObservationType: Pseudorange IRNSS L5 C for Rinex3.
C5D - org.orekit.gnss.PredefinedObservationType: Pseudorange QZSS L5 D / Beidou B2a Data for Rinex3.
C5I - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.
C5P - org.orekit.gnss.PredefinedObservationType: Pseudorange QZSS L5 P / Beidou B2a Pilot for Rinex3.
C5Q - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.
C5X - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C / Beidou B2a Data+Pilot for Rinex3.
C5Z - org.orekit.gnss.PredefinedObservationType: Pseudorange QZSS L5 D+P for Rinex3.
C6 - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E6 / Beidou B03 for Rinex2.
C6A - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E6 A PRS / GLONASS G2a L2CSI / Beidou B3A for Rinex3.
C6B - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E6 B C/NAV CS / GLONASS G2a L2OCp for Rinex3.
C6C - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E6 C no data for Rinex3.
C6D - org.orekit.gnss.PredefinedObservationType: Pseudorange Beidou B3A for Rinex3.
C6E - org.orekit.gnss.PredefinedObservationType: Pseudorange QZSS L6E for Rinex3.
C6I - org.orekit.gnss.PredefinedObservationType: Pseudorange Beidou B3 I for Rinex3.
C6L - org.orekit.gnss.PredefinedObservationType: Pseudorange QZSS LEX(6) L for Rinex3.
C6P - org.orekit.gnss.PredefinedObservationType: Pseudorange Beidou B3A for Rinex3.
C6Q - org.orekit.gnss.PredefinedObservationType: Pseudorange Beidou B3 Q for Rinex3.
C6S - org.orekit.gnss.PredefinedObservationType: Pseudorange QZSS LEX(6) S for Rinex3.
C6X - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q / GLONASS G2a L2CSI+L2OCp for Rinex3.
C6Z - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E6 A+B+C / QZSS L6(D+E) / Beidou B3A for Rinex3.
C7 - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E5b / Beidou B02 for Rinex2.
C7D - org.orekit.gnss.PredefinedObservationType: Pseudorange Beidou B2b Data for Rinex3.
C7I - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.
C7P - org.orekit.gnss.PredefinedObservationType: Pseudorange Beidou B2b Pilot for Rinex3.
C7Q - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo Q no data / Beidou B2 Q for Rinex3.
C7X - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.
C7Z - org.orekit.gnss.PredefinedObservationType: Pseudorange Beidou B2b Data+Pilot for Rinex3.
C8 - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E5a+b for Rinex2.
C8D - org.orekit.gnss.PredefinedObservationType: Pseudorange Beidou B2(B2a+B2b) Data for Rinex3.
C8I - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E5(E5a+E5b) I for Rinex3.
C8P - org.orekit.gnss.PredefinedObservationType: Pseudorange Beidou B2(B2a+B2b) Pilot for Rinex3.
C8Q - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E5(E5a+E5b) Q for Rinex3.
C8X - org.orekit.gnss.PredefinedObservationType: Pseudorange Galileo E5(E5a+E5b) I+Q / Beidou B2(B2a+B2b) Data+Pilot for Rinex3.
C9A - org.orekit.gnss.PredefinedObservationType: Pseudorange IRNSS S A for Rinex3.
C9B - org.orekit.gnss.PredefinedObservationType: Pseudorange IRNSS S B for Rinex3.
C9C - org.orekit.gnss.PredefinedObservationType: Pseudorange IRNSS S C for Rinex3.
C9X - org.orekit.gnss.PredefinedObservationType: Pseudorange IRNSS S B+C for Rinex3.
CA - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L1 C/A / GLONASS G1 C/A for Rinex2.
cacheAngularWindUp(TimeStampedPVCoordinates[], Rotation, Rotation) - Method in class org.orekit.estimation.measurements.gnss.AbstractWindUp: Cache angular wind-up.
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.
cachesTidalCorrection() - Method in class org.orekit.frames.EOPHistory: Check if the instance caches tidal corrections.
calculateBetaAngle(FieldSpacecraftState<T>, FieldPVCoordinatesProvider<T>) - Static method in class org.orekit.propagation.events.FieldBetaAngleDetector: Calculate the beta angle between the orbit plane and the celestial body.
calculateBetaAngle(FieldSpacecraftState<T>, FieldPVCoordinatesProvider<T>, Frame) - Static method in class org.orekit.propagation.events.FieldBetaAngleDetector: Calculate the beta angle between the orbit plane and the celestial body.
calculateBetaAngle(SpacecraftState, PVCoordinatesProvider) - Static method in class org.orekit.propagation.events.BetaAngleDetector: Calculate the beta angle between the orbit plane and the celestial body.
calculateBetaAngle(SpacecraftState, PVCoordinatesProvider, Frame) - Static method in class org.orekit.propagation.events.BetaAngleDetector: Calculate the beta angle between the orbit plane and the celestial body.
CALCULATED - org.orekit.files.ccsds.ndm.cdm.CovarianceMethod: Calculated covariance.
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.
calculatePointAlongArc(double) - Method in class org.orekit.bodies.LoxodromeArc: Calculate a point at a specific percentage along the arc.
Calibration(AbsoluteDate, int, String, int, int, double, double, double, double, double, double, double, int, int, int, int, double) - Constructor for class org.orekit.files.ilrs.CRD.Calibration: Constructor.
CalibrationDetail(AbsoluteDate, int, String, int, int, double, double, double, double, double, double, double, int, int, int, int, double) - Constructor for class org.orekit.files.ilrs.CRD.CalibrationDetail: Constructor.
CalibrationTargetConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration: Empty constructor.
canAdd(int, int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Check if coefficients can be added.
CANDIDATE - org.orekit.files.ccsds.ndm.odm.ocm.ManBasis: Proposed operational or hypothetical future maneuver.
CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_LOF - org.orekit.errors.OrekitMessages: CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_LOF.
CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_NON_INERTIAL_FRAME - org.orekit.errors.OrekitMessages: CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_NON_INERTIAL_FRAME.
CANNOT_COMPUTE_AIMING_AT_SINGULAR_POINT - org.orekit.errors.OrekitMessages: CANNOT_COMPUTE_AIMING_AT_SINGULAR_POINT.
CANNOT_COMPUTE_LAGRANGIAN - org.orekit.errors.OrekitMessages: CANNOT_COMPUTE_LAGRANGIAN.
CANNOT_ESTIMATE_PRECESSION_WITHOUT_PROPER_DERIVATIVES - org.orekit.errors.OrekitMessages: CANNOT_ESTIMATE_PRECESSION_WITHOUT_PROPER_DERIVATIVES.
CANNOT_FIND_SATELLITE_IN_SYSTEM - org.orekit.errors.OrekitMessages: CANNOT_FIND_SATELLITE_IN_SYSTEM.
CANNOT_PARSE_BOTH_TAU_AND_GAMMA - org.orekit.errors.OrekitMessages: CANNOT_PARSE_BOTH_TAU_AND_GAMMA.
CANNOT_PARSE_DATA - org.orekit.errors.OrekitMessages: CANNOT_PARSE_DATA.
CANNOT_PARSE_GNSS_DATA - org.orekit.errors.OrekitMessages: CANNOT_PARSE_GNSS_DATA.
CANNOT_PARSE_SOURCETABLE - org.orekit.errors.OrekitMessages: CANNOT_PARSE_SOURCETABLE.
CANNOT_START_PROPAGATION_FROM_INFINITY - org.orekit.errors.OrekitMessages: CANNOT_START_PROPAGATION_FROM_INFINITY.
CANONICAL_I_J - Static variable in class org.orekit.estimation.measurements.gnss.Dipole: Canonical dipole, with primary vector set to Vector3D.PLUS_I and secondary vector set to Vector3D.PLUS_J.
CanonicalSaastamoinenModel - Class in org.orekit.models.earth.troposphere: The canonical Saastamoinen model.
CanonicalSaastamoinenModel() - Constructor for class org.orekit.models.earth.troposphere.CanonicalSaastamoinenModel: Create a new Saastamoinen model for the troposphere using the given environmental conditions and table from the reference book.
canReceiveNMEA() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Check if caster can receive NMEA messages.
CARRIER_PHASE - org.orekit.gnss.MeasurementType: Carrier-phase measurement.
CARRIER_POWER - org.orekit.files.ccsds.ndm.tdm.ObservationType: Data: Carrier power [dBW].
CarrierPhase - Enum in org.orekit.gnss.metric.ntrip: Enumerate for carrier phase in DataStreamRecord.
CARTESIAN - org.orekit.orbits.OrbitType: Type for orbital representation in CartesianOrbit and FieldCartesianOrbit parameters.
CartesianAdjointDerivativesProvider - Class in org.orekit.control.indirect.adjoint: Class defining the adjoint dynamics, as defined in the Pontryagin Maximum Principle, in the case where Cartesian coordinates in an inertial frame are the dependent variable.
CartesianAdjointDerivativesProvider(CartesianCost, CartesianAdjointEquationTerm...) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointDerivativesProvider: Constructor.
CartesianAdjointDynamicsProvider - Class in org.orekit.control.indirect.shooting.propagation: Abstract class for Cartesian adjoint derivatives provider.
CartesianAdjointDynamicsProvider(String, int) - Constructor for class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProvider: Constructor.
CartesianAdjointDynamicsProviderFactory - Class in org.orekit.control.indirect.shooting.propagation: Factory for common Cartesian adjoint dynamics providers.
CartesianAdjointEquationTerm - Interface in org.orekit.control.indirect.adjoint: Interface to define terms in the adjoint equations and Hamiltonian for Cartesian coordinates.
CartesianAdjointInertialTerm - Class in org.orekit.control.indirect.adjoint: Class defining inertial forces' contributions in the adjoint equations for Cartesian coordinates.
CartesianAdjointInertialTerm(Frame) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm: Constructor.
CartesianAdjointJ2Term - Class in org.orekit.control.indirect.adjoint: Class defining a (constant) J2 contributions in the adjoint equations for Cartesian coordinates.
CartesianAdjointJ2Term(double, double, double, Frame) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term: Constructor.
CartesianAdjointKeplerianTerm - Class in org.orekit.control.indirect.adjoint: Class defining the Keplerian contributions in the adjoint equations for Cartesian coordinates.
CartesianAdjointKeplerianTerm(double) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointKeplerianTerm: Constructor.
CartesianAdjointSingleBodyTerm - Class in org.orekit.control.indirect.adjoint: Class defining the contributions of a point-mass, single body gravity in the adjoint equations for Cartesian coordinates.
CartesianAdjointSingleBodyTerm(double, ExtendedPositionProvider) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointSingleBodyTerm: Constructor.
CartesianAdjointThirdBodyTerm - Class in org.orekit.control.indirect.adjoint: Class defining the contributions of a point-mass, third body in the adjoint equations for Cartesian coordinates.
CartesianAdjointThirdBodyTerm(double, ExtendedPositionProvider) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointThirdBodyTerm: Constructor.
CartesianBoundaryConditionChecker - Interface in org.orekit.control.indirect.shooting.boundary: Interface defining convergence criterion when the terminal condition is on a Cartesian state.
cartesianBuilder(OneAxisEllipsoid) - Static method in class org.orekit.utils.WaypointPVBuilder: Construct a waypoint builder interpolating points using a linear cartesian interpolation.
CartesianCost - Interface in org.orekit.control.indirect.adjoint.cost: Interface to definite cost function in the frame of Pontryagin's Maximum Principle using Cartesian coordinates.
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.
CartesianCovarianceUtils - Class in org.orekit.utils: Utility class for conversions related to Cartesian covariance matrices.
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.
CartesianFlightDurationCost - Class in org.orekit.control.indirect.adjoint.cost: Class for minimizing the flight duration (a.k.a. time of flight) with Cartesian coordinates.
CartesianFlightDurationCost(String, double, double) - Constructor for class org.orekit.control.indirect.adjoint.cost.CartesianFlightDurationCost: Constructor.
CartesianFuelCost - Class in org.orekit.control.indirect.adjoint.cost: Class for fuel cost with Cartesian coordinates.
CartesianFuelCost(String, double, double) - Constructor for class org.orekit.control.indirect.adjoint.cost.CartesianFuelCost: Constructor with default detection settings.
CartesianFuelCost(String, double, double, EventDetectionSettings) - Constructor for class org.orekit.control.indirect.adjoint.cost.CartesianFuelCost: Constructor.
CartesianOrbit - Class in org.orekit.orbits: This class holds Cartesian orbital parameters.
CartesianOrbit(Orbit) - Constructor for class org.orekit.orbits.CartesianOrbit: Constructor from any kind of orbital parameters.
CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CartesianOrbit: Constructor from Cartesian parameters.
CartesianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CartesianOrbit: Constructor from Cartesian parameters.
CartesianToleranceProvider - Interface in org.orekit.propagation: Interface to define integration tolerances for adaptive schemes (like the embedded Runge-Kutta ones) propagating the position-velocity vector and the mass, for a total of 7 primary dependent variables (in that order).
CARTP - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType: Cartesian 3-element position (X, Y, Z).
CARTPV - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType: Cartesian 6-element position and velocity (X, Y, Z, XD, YD, ZD).
CARTPVA - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType: Cartesian 9-element position, velocity and acceleration (X, Y, Z, XD, YD, ZD, XDD, YDD, ZDD).
CAS - org.orekit.gnss.metric.ntrip.RecordType: Casters.
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.
CATALOG_NAME - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey: Specification of satellite catalog source.
CATALOG_NAME - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey: Satellite catalog used for the object.
CATALOG_NAME - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey: Specification of satellite catalog source.
CB - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L1C for Rinex2.
CC - org.orekit.gnss.PredefinedObservationType: Pseudorange GPS L2C for Rinex2.
CCSDS_ACM_VERS - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.AcmWriter: Version number implemented.
CCSDS_AEM_VERS - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.AemWriter: Version number implemented.
CCSDS_APM_VERS - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter: Version number implemented.
CCSDS_CDM_VERS - Static variable in class org.orekit.files.ccsds.ndm.cdm.CdmWriter: Version number implemented.
CCSDS_DATE_INVALID_LENGTH_TIME_FIELD - org.orekit.errors.OrekitMessages: CCSDS_DATE_INVALID_LENGTH_TIME_FIELD.
CCSDS_DATE_INVALID_PREAMBLE_FIELD - org.orekit.errors.OrekitMessages: CCSDS_DATE_INVALID_PREAMBLE_FIELD.
CCSDS_DATE_MISSING_AGENCY_EPOCH - org.orekit.errors.OrekitMessages: CCSDS_DATE_MISSING_AGENCY_EPOCH.
CCSDS_DIFFERENT_LVLH_DEFINITION - org.orekit.errors.OrekitMessages: CCSDS_DIFFERENT_LVLH_DEFINITION.
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_INCOMPATIBLE_KEYS_BOTH_USED - org.orekit.errors.OrekitMessages: CCSDS_INCOMPATIBLE_KEYS_BOTH_USED.
CCSDS_INCOMPLETE_DATA - org.orekit.errors.OrekitMessages: CCSDS_INCOMPLETE_DATA.
CCSDS_INCONSISTENT_NUMBER_OF_ATTITUDE_STATES - org.orekit.errors.OrekitMessages: CCSDS_INCONSISTENT_NUMBER_OF_ATTITUDE_STATES.
CCSDS_INCONSISTENT_TIME_SYSTEMS - org.orekit.errors.OrekitMessages: CCSDS_INCONSISTENT_TIME_SYSTEMS.
CCSDS_INVALID_FRAME - org.orekit.errors.OrekitMessages: CCSDS_INVALID_FRAME.
CCSDS_INVALID_ROTATION_SEQUENCE - org.orekit.errors.OrekitMessages: CCSDS_INVALID_ROTATION_SEQUENCE.
CCSDS_KEYWORD_NOT_ALLOWED_IN_VERSION - org.orekit.errors.OrekitMessages: CCSDS_KEYWORD_NOT_ALLOWED_IN_VERSION.
CCSDS_MANEUVER_MISSING_TIME - org.orekit.errors.OrekitMessages: CCSDS_MANEUVER_MISSING_TIME.
CCSDS_MANEUVER_UNITS_WRONG_NB_COMPONENTS - org.orekit.errors.OrekitMessages: CCSDS_MANEUVER_UNITS_WRONG_NB_COMPONENTS.
CCSDS_MISSING_KEYWORD - org.orekit.errors.OrekitMessages: CCSDS_MISSING_KEYWORD.
CCSDS_MISSING_SENSOR_INDEX - org.orekit.errors.OrekitMessages: CCSDS_MISSING_SENSOR_INDEX.
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_SENSOR_INDEX_ALREADY_USED - org.orekit.errors.OrekitMessages: CCSDS_SENSOR_INDEX_ALREADY_USED.
CCSDS_TDM_KEYWORD_NOT_FOUND - org.orekit.errors.OrekitMessages: CCSDS_TDM_KEYWORD_NOT_FOUND.
CCSDS_TDM_MISSING_RANGE_UNITS_CONVERTER - org.orekit.errors.OrekitMessages: CCSDS_TDM_MISSING_RANGE_UNITS_CONVERTER.
CCSDS_TDM_VERS - Static variable in class org.orekit.files.ccsds.ndm.tdm.TdmWriter: Version number implemented.
CCSDS_TIME_SYSTEM_NOT_IMPLEMENTED - org.orekit.errors.OrekitMessages: CCSDS_TIME_SYSTEM_NOT_IMPLEMENTED.
CCSDS_TIME_SYSTEM_NOT_READ_YET - org.orekit.errors.OrekitMessages: CCSDS_TIME_SYSTEM_NOT_READ_YET.
CCSDS_UNEXPECTED_KEYWORD - org.orekit.errors.OrekitMessages: CCSDS_UNEXPECTED_KEYWORD.
CCSDS_UNKNOWN_ATTITUDE_TYPE - org.orekit.errors.OrekitMessages: CCSDS_UNKNOWN_ATTITUDE_TYPE.
CCSDS_UNKNOWN_CONVENTIONS - org.orekit.errors.OrekitMessages: CCSDS_UNKNOWN_CONVENTIONS.
CCSDS_UNKNOWN_GM - org.orekit.errors.OrekitMessages: CCSDS_UNKNOWN_GM.
CCSDS_UNKNOWN_SPACECRAFT_MASS - org.orekit.errors.OrekitMessages: CCSDS_UNKNOWN_SPACECRAFT_MASS.
CCSDS_UNSUPPORTED_ELEMENT_SET_TYPE - org.orekit.errors.OrekitMessages: CCSDS_UNSUPPORTED_ELEMENT_SET_TYPE.
CCSDS_UNSUPPORTED_RETROGRADE_EQUINOCTIAL - org.orekit.errors.OrekitMessages: CCSDS_UNSUPPORTED_RETROGRADE_EQUINOCTIAL.
CD - org.orekit.gnss.PredefinedObservationType: Pseudorange GLONASS G2 for Rinex2.
CD_AREA_OVER_MASS - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey: The object’s Cd x A/m used to propagate the state vector and covariance to TCA.
Cdm - Class in org.orekit.files.ccsds.ndm.cdm: This class stores all the information of the Conjunction Data Message (CDM) File parsed by CdmParser.
Cdm(CdmHeader, List<CdmSegment>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.cdm.Cdm: Simple constructor.
CDM_MSG_LINK - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey: Unique identifier of Conjunction Data Message linked to this Orbit Data Message.
CdmData - Class in org.orekit.files.ccsds.ndm.cdm: Container for Conjunction Data Message data.
CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData: Constructor with RTN covariance.
CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance, AdditionalCovarianceMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData: Constructor with RTN covariance.
CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance, SigmaEigenvectorsCovariance, AdditionalCovarianceMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData: Constructor with RTN and sigma/eigenvector covariance.
CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance, XYZCovariance, AdditionalCovarianceMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData: Constructor with RTN and XYZ covariance.
CdmHeader - Class in org.orekit.files.ccsds.ndm.cdm: Header of a CCSDS Conjunction Data Message.
CdmHeader() - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmHeader: Constructor.
CdmHeaderKey - Enum in org.orekit.files.ccsds.ndm.cdm: Keywords allowed in CdmHeader.
CdmHeaderProcessingState - Class in org.orekit.files.ccsds.ndm.cdm: ProcessingState for CDM header.
CdmHeaderProcessingState(CdmParser) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmHeaderProcessingState: Simple constructor.
CdmMessageWriter - Class in org.orekit.files.ccsds.ndm.cdm: Cdm message writer.
CdmMessageWriter(String, String, double, ContextBinding) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter: Constructor used to create a new NDM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
CdmMetadata - Class in org.orekit.files.ccsds.ndm.cdm: This class gathers the meta-data present in the Conjunction Data Message (CDM).
CdmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Simple constructor.
CdmMetadata(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Simple constructor.
CdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.cdm: Keys for CDM container entries.
CdmMetadataWriter - Class in org.orekit.files.ccsds.ndm.cdm: Writer for Metadata for CCSDS Conjunction Data Messages.
CdmMetadataWriter(CdmMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMetadataWriter: Simple constructor.
CdmParser - Class in org.orekit.files.ccsds.ndm.cdm: Base class for Conjunction Data Message parsers.
CdmParser(IERSConventions, boolean, DataContext, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmParser: Complete constructor.
CdmRelativeMetadata - Class in org.orekit.files.ccsds.ndm.cdm: This class gathers the relative meta-data present in the Conjunction Data Message (CDM).
CdmRelativeMetadata() - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Simple constructor.
CdmRelativeMetadataKey - Enum in org.orekit.files.ccsds.ndm.cdm: Keys for CDM container entries.
CdmSegment - Class in org.orekit.files.ccsds.ndm.cdm: This class stores the metadata and data for one object.
CdmSegment(CdmMetadata, CdmData) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmSegment: Simple constructor.
CdmWriter - Class in org.orekit.files.ccsds.ndm.cdm: Writer for CCSDS Conjunction Data Message.
CdmWriter(IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmWriter: Complete constructor.
CDRG_DRG - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [7,7].
CDRG_DRG - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [7,7].
CDRG_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [7,3].
CDRG_NDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [7,6].
CDRG_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [7,1].
CDRG_RDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [7,4].
CDRG_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [7,2].
CDRG_TDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [7,5].
CDRG_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [7,1].
CDRG_XDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [7,4].
CDRG_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [7,2].
CDRG_YDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [7,5].
CDRG_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [7,3].
CDRG_ZDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [7,6].
CELESTIAL_SOURCE - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey: Source and version of celestial body (e.g.
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, ExtendedPositionProvider, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.CelestialBodyPointed: Creates new instance.
CellInterpolator - Class in org.orekit.models.earth.weather: Interpolator within a grid cell.
CENTER_NAME - org.orekit.files.ccsds.ndm.adm.AdmMetadataKey: Center name entry.
CENTER_NAME - org.orekit.files.ccsds.ndm.odm.CommonMetadataKey: Center name entry.
CENTER_NAME - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey: Origin of the reference frame of the trajectory.
CENTER_OF_MASS_XYZ - org.orekit.files.rinex.section.RinexLabels: Center of mass.
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.
CENTRAL_BODY_ROTATION - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Central body angular rotation rate.
CHAN_1997 - org.orekit.files.ccsds.definitions.PocMethodType: Chan 1997 method.
CHAN_1997 - org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType: Probability of collision computing method described in :
"Chan,K.
CHAN_2003 - org.orekit.files.ccsds.definitions.PocMethodType: Chan 2003 method.
Chan1997 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod: Compute the probability of collision using the method described in :
"Chan, K.
Chan1997() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997: Empty constructor.
change(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractStateModifier: Change main state.
change(SpacecraftState) - Method in class org.orekit.propagation.AbstractStateModifier: Change main state.
CHANGE_IN_TWO_RECEIVER_ONE_SATELLITE_CARRIER_PHASE - org.orekit.files.sp3.DataUsed: Change in 2-receiver/1-satellite carrier phase.
CHANGE_IN_TWO_RECEIVER_ONE_SATELLITE_CODE_PHASE - org.orekit.files.sp3.DataUsed: Change in 2-receiver/1-satellite code phase.
CHANGE_IN_TWO_RECEIVER_TWO_SATELLITE_CARRIER_PHASE - org.orekit.files.sp3.DataUsed: Change in 2-receiver/2-satellite carrier phase.
CHANGE_IN_TWO_RECEIVER_TWO_SATELLITE_CODE_PHASE - org.orekit.files.sp3.DataUsed: Change in 2-receiver/2-satellite code phase.
CHANGE_IN_UNDIFFERENTIATED_CARRIER_PHASE - org.orekit.files.sp3.DataUsed: Change in undifferenciated carrier phase.
CHANGE_IN_UNDIFFERENTIATED_CODE_PHASE - org.orekit.files.sp3.DataUsed: Change in undifferenciated code phase.
changeCovarianceFrame(FieldOrbit<T>, Frame) - Method in class org.orekit.propagation.FieldStateCovariance: Get the covariance in the output frame.
changeCovarianceFrame(FieldOrbit<T>, LOF) - Method in class org.orekit.propagation.FieldStateCovariance: Get the covariance in a given local orbital frame.
changeCovarianceFrame(Orbit, Frame) - Method in class org.orekit.propagation.StateCovariance: Get the covariance in the output frame.
changeCovarianceFrame(Orbit, LOF) - Method in class org.orekit.propagation.StateCovariance: Get the covariance in a given local orbital frame.
changeCovarianceType(FieldOrbit<T>, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.FieldStateCovariance: Get the covariance matrix in another orbit type.
changeCovarianceType(Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.StateCovariance: Get the covariance matrix in another orbit type.
changeField(Function<T, U>) - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouAlmanac: Create another field version of the instance.
changeField(Function<T, U>) - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Create another field version of the instance.
changeField(Function<T, U>) - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouLegacyNavigationMessage: Create another field version of the instance.
changeField(Function<T, U>) - Method in class org.orekit.propagation.analytical.gnss.data.FieldGalileoAlmanac: Create another field version of the instance.
changeField(Function<T, U>) - Method in class org.orekit.propagation.analytical.gnss.data.FieldGalileoNavigationMessage: Create another field version of the instance.
changeField(Function<T, U>) - Method in class org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements: Create another field version of the instance.
changeField(Function<T, U>) - Method in class org.orekit.propagation.analytical.gnss.data.FieldGPSAlmanac: Create another field version of the instance.
changeField(Function<T, U>) - Method in class org.orekit.propagation.analytical.gnss.data.FieldGPSCivilianNavigationMessage: Create another field version of the instance.
changeField(Function<T, U>) - Method in class org.orekit.propagation.analytical.gnss.data.FieldGPSLegacyNavigationMessage: Create another field version of the instance.
changeField(Function<T, U>) - Method in class org.orekit.propagation.analytical.gnss.data.FieldIRNSSAlmanac: Create another field version of the instance.
changeField(Function<T, U>) - Method in class org.orekit.propagation.analytical.gnss.data.FieldIRNSSNavigationMessage: Create another field version of the instance.
changeField(Function<T, U>) - Method in class org.orekit.propagation.analytical.gnss.data.FieldQZSSAlmanac: Create another field version of the instance.
changeField(Function<T, U>) - Method in class org.orekit.propagation.analytical.gnss.data.FieldQZSSCivilianNavigationMessage: Create another field version of the instance.
changeField(Function<T, U>) - Method in class org.orekit.propagation.analytical.gnss.data.FieldQZSSLegacyNavigationMessage: Create another field version of the instance.
changeFrame(SP3, Frame) - Static method in class org.orekit.files.sp3.SP3: Change the frame of an SP3 file.
changeReferenceFrame(Frame, RealMatrix, AbsoluteDate, Frame) - Static method in class org.orekit.utils.CartesianCovarianceUtils: Convert input position-velocity covariance matrix between reference frames.
ChaoMappingFunction - Class in org.orekit.models.earth.troposphere: Chao mapping function for radio wavelengths.
ChaoMappingFunction() - Constructor for class org.orekit.models.earth.troposphere.ChaoMappingFunction: Builds a new instance.
CHECK_SUM_TERM_LENGTH - Static variable in class org.orekit.files.iirv.terms.CheckSumTerm: The length of the IIRV term within the message.
CHECK_SUM_TERM_PATTERN - Static variable in class org.orekit.files.iirv.terms.CheckSumTerm: Regular expression that ensures the validity of string values for this term.
checkAllowed(double, Object, String, double, double) - Method in class org.orekit.files.ccsds.section.CommentsContainer: Complain if a key is not allowed.
checkDatesConsistency(AbsoluteDate, AbsoluteDate, double) - Static method in class org.orekit.time.TimeStampedPair: Check date consistency.
checkDimension(int, ParameterDriversList, ParameterDriversList, ParameterDriversList) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil: Check dimension.
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.AttitudeEndpoints: Check external frame is properly initialized.
checkFrameAndOrbitTypeConsistency(Frame, OrbitType) - Static method in class org.orekit.propagation.StateCovariance: Check constructor's inputs consistency.
checkIfForward(FieldSpacecraftState<W>, FieldAbsoluteDate<W>) - Static method in class org.orekit.propagation.events.FieldAbstractDetector: Check if propagation is forward or not.
checkIfForward(SpacecraftState, AbsoluteDate) - Static method in class org.orekit.propagation.events.AbstractDetector: Check if propagation is forward or not.
checkInputConsistency(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>) - Static method in class org.orekit.propagation.analytical.Ephemeris: Check input consistency between states, covariances and their associated interpolators.
checkInterpolatorCompatibilityWithSampleSize(FieldTimeInterpolator<? extends FieldTimeStamped<T>, T>, int) - Static method in class org.orekit.time.AbstractFieldTimeInterpolator: Method checking if given interpolator is compatible with given sample size.
checkInterpolatorCompatibilityWithSampleSize(TimeInterpolator<? extends TimeStamped>, int) - Static method in class org.orekit.time.AbstractTimeInterpolator: Method checking if given interpolator is compatible with given sample size.
checkMandatoryEntriesExceptExternalFrame(double, Enum<?>, Enum<?>, Enum<?>) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints: Check is mandatory entries except external frame have been initialized.
checkNotNaN(double, String) - Method in class org.orekit.files.ccsds.section.CommentsContainer: Complain if a field is NaN.
checkNotNegative(int, String) - Method in class org.orekit.files.ccsds.section.CommentsContainer: Complain if a field is negative.
checkNotNull(Object, Enum<?>) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Complain if a field is null.
checkNotNull(Object, String) - Method in class org.orekit.files.ccsds.section.CommentsContainer: Complain if a field is null.
checkOrbitsConsistency(Collection<Orbit>) - Static method in class org.orekit.orbits.AbstractOrbitInterpolator: Check orbits consistency by comparing their gravitational parameters µ.
checkParity(int, int) - Static method in class org.orekit.gnss.rflink.gps.SubFrame: Check parity.
checkSampleAndInterpolatorConsistency(List<SpacecraftState>, boolean, boolean) - Static method in class org.orekit.propagation.SpacecraftStateInterpolator: Check that an interpolator exist for given sample state definition.
checkScreenVolumeConditions() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Check screen volume conditions.
checkStatesAndCovariancesConsistency(List<SpacecraftState>, List<StateCovariance>) - Static method in class org.orekit.propagation.analytical.Ephemeris: Check that given states and covariances are consistent.
checkStatesDefinitionsConsistency(List<SpacecraftState>) - Static method in class org.orekit.propagation.SpacecraftStateInterpolator: Check that all state are either orbit defined or based on absolute position-velocity-acceleration.
checkStep(double) - Method in class org.orekit.propagation.conversion.AbstractFixedStepFieldIntegratorBuilder: Check that given step size is not equal to 0.
CheckSumTerm - Class in org.orekit.files.iirv.terms: Three-character checksum to validate message.
CheckSumTerm(long) - Constructor for class org.orekit.files.iirv.terms.CheckSumTerm: Constructor.
CheckSumTerm(String) - Constructor for class org.orekit.files.iirv.terms.CheckSumTerm: Constructor.
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.
ChronologicalComparator - Class in org.orekit.time: Comparator for TimeStamped instance.
ChronologicalComparator() - Constructor for class org.orekit.time.ChronologicalComparator: Simple constructor.
CIC_INDEX - Static variable in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Index of cosine on inclination in the list returned by GNSSOrbitalElementsDriversProvider.getParametersDrivers().
CIPM2007 - Class in org.orekit.models.earth.weather.water: Official model CIPM-2007 (identical to CIPM-1981/91) from Comité International des Poids et Mesures.
CIPM2007() - Constructor for class org.orekit.models.earth.weather.water.CIPM2007
CIRCULAR - org.orekit.orbits.OrbitType: Type for orbital representation in CircularOrbit and FieldCircularOrbit parameters.
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.
CircularLatitudeArgumentUtility - Class in org.orekit.orbits: Utility methods for converting between different latitude arguments used by CircularOrbit.
CircularOrbit - Class in org.orekit.orbits: This class handles circular orbital parameters.
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit: Creates a new instance with derivatives and with cached position angle same as value inputted.
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit: Creates a new instance.
CircularOrbit(double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit: Creates a new instance without derivatives and with cached position angle same as value inputted.
CircularOrbit(double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit: Creates a new instance.
CircularOrbit(Orbit) - Constructor for class org.orekit.orbits.CircularOrbit: Constructor from any kind of orbital parameters.
CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit: Constructor from Cartesian parameters.
CircularOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CircularOrbit: Constructor from Cartesian parameters.
CIRF_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined: CIRF frame, IERS 1996 conventions, with accurate EOP interpolation.
CIRF_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined: CIRF frame, IERS 1996 conventions, with simple EOP interpolation.
CIRF_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined: CIRF frame, IERS 2003 conventions, with accurate EOP interpolation.
CIRF_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined: CIRF frame, IERS 2003 conventions, with simple EOP interpolation.
CIRF_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined: CIRF frame, IERS 2010 conventions, with accurate EOP interpolation.
CIRF_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined: CIRF frame, IERS 2010 conventions, with simple EOP interpolation.
CIS_INDEX - Static variable in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Index of sine on inclination in the list returned by GNSSOrbitalElementsDriversProvider.getParametersDrivers().
CIVIL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector: Sun elevation at civil dawn/dusk (6° below horizon).
CivilianNavigationMessage<O extends CivilianNavigationMessage<O>> - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a GPS/QZNSS civilian navigation message.
CivilianNavigationMessage(boolean, double, double, int, TimeScales, SatelliteSystem) - Constructor for class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Constructor.
CivilianNavigationMessage(FieldCivilianNavigationMessage<T, A>) - Constructor for class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Constructor from field instance.
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: CK2.
CK4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: CK4.
ClassicalRungeKuttaFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion: Builder for ClassicalRungeKuttaFieldIntegrator.
ClassicalRungeKuttaFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaFieldIntegratorBuilder: Constructor.
ClassicalRungeKuttaFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaFieldIntegratorBuilder: Constructor using a "fielded" step.
ClassicalRungeKuttaIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for ClassicalRungeKuttaIntegrator.
ClassicalRungeKuttaIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder: Build a new instance.
CLASSIFICATION - org.orekit.files.ccsds.ndm.cdm.CdmHeaderKey: User-defined free-text message classification or caveats of this CDM.
CLASSIFICATION - org.orekit.files.ccsds.section.HeaderKey: Classification.
CLASSIFICATION_TYPE - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey: Classifiation type.
ClasspathCrawler - Class in org.orekit.data: Provider for data files stored as resources in the classpath.
ClasspathCrawler(ClassLoader, String...) - Constructor for class org.orekit.data.ClasspathCrawler: Build a data classpath crawler.
ClasspathCrawler(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.DataDictionary: Remove all entries.
clear() - Method in class org.orekit.utils.DoubleArrayDictionary: Remove all entries.
clear() - Method in class org.orekit.utils.FieldArrayDictionary: Remove all entries.
clear() - Method in class org.orekit.utils.FieldDataDictionary: Remove all entries.
clearCelestialBodyCache() - Static method in class org.orekit.bodies.CelestialBodyFactory: Clear all loaded celestial bodies.
clearCelestialBodyCache() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies: Clear all loaded celestial bodies.
clearCelestialBodyCache(String) - Static method in class org.orekit.bodies.CelestialBodyFactory: Clear the specified celestial body from the internal cache.
clearCelestialBodyCache(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies: Clear the specified celestial body from the internal cache.
clearCelestialBodyLoaders() - Static method in class org.orekit.bodies.CelestialBodyFactory: Clear loaders for all celestial bodies.
clearCelestialBodyLoaders() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies: Clear loaders for all celestial bodies.
clearCelestialBodyLoaders(String) - Static method in class org.orekit.bodies.CelestialBodyFactory: Clear loaders for one celestial body.
clearCelestialBodyLoaders(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies: Clear loaders for one celestial body.
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.
clearEphemerisGenerators() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Clear the ephemeris generators.
clearEphemerisGenerators() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Clear the ephemeris generators.
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.
clearImpulseManeuvers() - Method in class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder: Remove all impulse maneuvers.
clearImpulseManeuvers() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Remove all impulse maneuvers.
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.
clipExp(double) - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickModel: A clipped exponential function.
clipExp(T) - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickModel: A clipped exponential function.
CLOCK_ACCELERATION_PREFIX - Static variable in class org.orekit.estimation.measurements.ObservableSatellite: Prefix for clock acceleration parameter driver, the propagator index will be appended to it.
CLOCK_ACCURACY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils: Clock accuracy unit.
CLOCK_ADDITIONAL_STATE - Static variable in class org.orekit.files.sp3.SP3Utils: Additional state name for clock.
CLOCK_BIAS - org.orekit.files.ccsds.ndm.tdm.ObservationType: Data: Clock bias [s].
CLOCK_CORRECTIONS - Static variable in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider: Name of the additional state for satellite clock corrections.
CLOCK_DRIFT - org.orekit.files.ccsds.ndm.tdm.ObservationType: Data: Clock drift [s/s].
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_FILE_UNSUPPORTED_VERSION - org.orekit.errors.OrekitMessages: CLOCK_FILE_UNSUPPORTED_VERSION.
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.
CLOCK_RATE_ACCURACY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils: Clock rate accuracy unit.
CLOCK_RATE_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils: Clock rate unit.
CLOCK_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils: Clock unit.
ClockCorrection - Class in org.orekit.gnss.metric.messages.common: Container for SSR clock correction data.
ClockCorrection(double, double, double) - Constructor for class org.orekit.gnss.metric.messages.common.ClockCorrection: Constructor.
ClockCorrectionsProvider - Class in org.orekit.propagation.analytical.gnss: Provider for clock corrections as additional states.
ClockCorrectionsProvider(GNSSClockElements, double) - 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.files.rinex.clock.RinexClock.ClockDataLine: Constructor.
ClockModel - Interface in org.orekit.time: Offset clock model.
ClockOffset - Class in org.orekit.time: Container for time stamped clock offset.
ClockOffset(AbsoluteDate, double, double, double) - Constructor for class org.orekit.time.ClockOffset: Simple constructor.
ClockOffsetHermiteInterpolator - Class in org.orekit.time: bHermite interpolator of time stamped clock offsets.
ClockOffsetHermiteInterpolator(int) - Constructor for class org.orekit.time.ClockOffsetHermiteInterpolator: Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
ClockOffsetHermiteInterpolator(int, double) - Constructor for class org.orekit.time.ClockOffsetHermiteInterpolator: Constructor.
ClockTimeScale - Class in org.orekit.time: Time scale with clock offset from another time scale.
ClockTimeScale(String, TimeScale, ClockModel) - Constructor for class org.orekit.time.ClockTimeScale: Simple constructor.
clone() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
close() - Method in class org.orekit.data.LineOrientedFilteringReader
close() - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter
close() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter
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.
close() - Method in class org.orekit.files.rinex.observation.RinexObservationWriter
closeTo(RadioWave) - Method in interface org.orekit.gnss.RadioWave: Check if two radio waves are closer than RadioWave.ONE_MILLI_HERTZ.
closeTo(RadioWave, double) - Method in interface org.orekit.gnss.RadioWave: Check if two radio waves are closer than tolerance.
CM_COEFFICIENTS - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Identifier for cMm coefficients.
CMR - org.orekit.gnss.metric.ntrip.DataFormat: CMR.
CMR_PLUS - org.orekit.gnss.metric.ntrip.DataFormat: CMR+.
CN_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [3,3].
CN_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [3,1].
CN_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [3,2].
CNAV - Static variable in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Identifier for message type.
CNDOT_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [6,3].
CNDOT_NDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [6,6].
CNDOT_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [6,1].
CNDOT_RDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [6,4].
CNDOT_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [6,2].
CNDOT_TDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [6,5].
CNES - Static variable in class org.orekit.files.iirv.terms.OriginIdentificationTerm: French Space Agency National Centre for Space Studies (CNES) OriginIdentification.
CNES - Static variable in class org.orekit.files.iirv.terms.RoutingIndicatorTerm: French Space Agency National Centre for Space Studies (CNES) RoutingIndicator.
CNV1 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Identifier for Beidou-3 B1C message type.
CNV2 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Identifier for Beidou-3 B2A message type.
CNV2 - Static variable in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Identifier for message type.
CNV3 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Identifier for Beidou-3 B2B message type.
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.common: Container for code bias data.
CodeBias(int, double) - Constructor for class org.orekit.gnss.metric.messages.common.CodeBias: Constructor.
CODELESS - org.orekit.gnss.SignalCode: Codeless.
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.
COHERENT - org.orekit.files.ccsds.ndm.tdm.RangeMode: Range tones coherent with uplink carrier.
COLLISION_MAX_PC_METHOD - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey: The method that was used to calculate the maximum collision probability.
COLLISION_MAX_PROBABILITY - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey: The maximum collision probability that Object1 and Object2 will collide.
COLLISION_PERCENTILE - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey: An array of 1 to n elements indicating the percentile(s) for which estimates of the collision probability are provided in the COLLISION_PROBABILITY variable.
COLLISION_PROBABILITY - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey: The probability (between 0.0 and 1.0) that Object1 and Object2 will collide.
COLLISION_PROBABILITY_METHOD - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey: The method that was used to calculate the collision probability.
COLUMN_DIM - Static variable in class org.orekit.propagation.AbstractStateCovarianceInterpolator: Default column dimension for position-velocity state covariance.
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(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 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(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.
COMBINED_RANGE_PHASE - org.orekit.gnss.MeasurementType: Combined pseudo-range carrier-phase measurement.
combinedDerivatives(FieldSpacecraftState<T>) - Method in class org.orekit.control.indirect.adjoint.FieldCartesianAdjointDerivativesProvider: Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider: Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointDerivativesProvider: Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay: Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider: Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations: Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations: Compute the derivatives related to the additional state (and optionally main state increments).
CombinedDerivatives - Class in org.orekit.propagation.integration: Container for additional derivatives.
CombinedDerivatives(double[], double[]) - Constructor for class org.orekit.propagation.integration.CombinedDerivatives: Simple constructor.
CombinedObservationData - Class in org.orekit.estimation.measurements.gnss: Combined observation data.
CombinedObservationData(double, double, CombinationType, MeasurementType, List<ObservationData>) - Constructor for class org.orekit.estimation.measurements.gnss.CombinedObservationData: Constructor.
CombinedObservationDataSet - Class in org.orekit.estimation.measurements.gnss: Combined observation data set.
CombinedObservationDataSet(SatelliteSystem, int, AbsoluteDate, double, List<CombinedObservationData>) - Constructor for class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet: Simple constructor.
COMMA_SEP - Static variable in exception org.orekit.errors.UnsupportedParameterException: Comma separator for printing list of supported parameter drivers.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.EulerKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.ODParametersKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovarianceKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.StateVectorKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey: General comment.
COMMENT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.StateVectorKey: Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.tdm.TdmDataKey: Comment entry.
COMMENT - org.orekit.files.ccsds.section.HeaderKey: Header comment.
COMMENT - org.orekit.files.ccsds.section.MetadataKey: Comment entry.
COMMENT - org.orekit.files.rinex.section.RinexLabels: Comments.
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<O extends CommonGnssData<O>> - Class in org.orekit.propagation.analytical.gnss.data: Container for common GNSS data contained in almanac and navigation messages.
CommonGnssData(double, double, int, TimeScales, SatelliteSystem) - Constructor for class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Constructor.
CommonGnssData(FieldCommonGnssData<T, A>) - Constructor for class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Constructor from field instance.
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(OdmCommonMetadata, TimeConverter) - Constructor for class org.orekit.files.ccsds.ndm.odm.CommonMetadataWriter: Simple constructor.
CommonParametersWithDerivatives - Class in org.orekit.estimation.measurements: Common intermediate parameters used to estimate measurements where receiver is a ground station.
CommonParametersWithDerivatives(SpacecraftState, Map<String, Integer>, Gradient, SpacecraftState, TimeStampedFieldPVCoordinates<Gradient>) - Constructor for class org.orekit.estimation.measurements.CommonParametersWithDerivatives: Simple constructor.
CommonParametersWithoutDerivatives - Class in org.orekit.estimation.measurements: Common intermediate parameters used to estimate measurements.
CommonParametersWithoutDerivatives(SpacecraftState, double, SpacecraftState, TimeStampedPVCoordinates) - Constructor for class org.orekit.estimation.measurements.CommonParametersWithoutDerivatives: Simple constructor.
CommonPhysicalProperties - Class in org.orekit.files.ccsds.ndm: Container for common physical properties for both OrbitPhysicalProperties and AdditionalParameters.
CommonPhysicalProperties() - Constructor for class org.orekit.files.ccsds.ndm.CommonPhysicalProperties: 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(FieldTimeStamped<KK>, FieldTimeStamped<KK>) - Method in class org.orekit.time.FieldChronologicalComparator: Compare two time-stamped instances.
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(IIRVVector) - Method in class org.orekit.files.iirv.IIRVVector: Compares two IIRV vectors for equality based on their string representations, include message metadata information.
compareTo(IIRVVectorTerm<?>) - Method in class org.orekit.files.iirv.terms.base.IIRVVectorTerm
compareTo(AbstractSolarActivityDataLoader.LineParameters) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader.LineParameters
compareTo(AbstractSolarActivityDataLoader.LineParameters) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
compareTo(AbstractSolarActivityDataLoader.LineParameters) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters
compareTo(CoefficientsFactory.NSKey) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
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
compareTo(TimeOffset) - Method in class org.orekit.time.TimeOffset: Compare the instance with another one.
COMPASS - org.orekit.files.sp3.SP3FileType: COMPASS only file.
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.
completed() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver: Check if maneuver has been completed.
components(AbsoluteDate) - Method in class org.orekit.files.ccsds.definitions.TimeConverter: Generate calendar components.
compose(AbsoluteDate, KinematicTransform, KinematicTransform) - Static method in interface org.orekit.frames.KinematicTransform: Build a transform by combining two existing ones.
compose(AbsoluteDate, StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform: Build a transform by combining two existing ones.
compose(FieldAbsoluteDate<T>, FieldKinematicTransform<T>, FieldKinematicTransform<T>) - Static method in interface org.orekit.frames.FieldKinematicTransform: Build a transform by combining two existing ones.
compose(FieldAbsoluteDate<T>, FieldStaticTransform<T>, FieldStaticTransform<T>) - Static method in interface org.orekit.frames.FieldStaticTransform: Build a transform by combining two existing ones.
CompositeDataContext - Class in org.orekit.data: A simple implementation of DataContext that composes the constituent factories into a data context.
CompositeDataContext(TimeScales, Frames, CelestialBodies, GravityFields, GeoMagneticFields) - Constructor for class org.orekit.data.CompositeDataContext: Simple constructor.
compositeRotation(FieldStaticTransform<T>, FieldStaticTransform<T>) - Static method in interface org.orekit.frames.FieldStaticTransform: Compute a composite rotation.
compositeRotation(StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform: Compute a composite rotation.
compositeRotationRate(FieldKinematicTransform<T>, FieldKinematicTransform<T>) - Static method in interface org.orekit.frames.FieldKinematicTransform: Compute a composite rotation rate.
compositeRotationRate(KinematicTransform, KinematicTransform) - Static method in interface org.orekit.frames.KinematicTransform: Compute a composite rotation rate.
compositeTranslation(FieldStaticTransform<T>, FieldStaticTransform<T>) - Static method in interface org.orekit.frames.FieldStaticTransform: Compute a composite translation.
compositeTranslation(StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform: Compute a composite translation.
compositeVelocity(FieldKinematicTransform<T>, FieldKinematicTransform<T>) - Static method in interface org.orekit.frames.FieldKinematicTransform: Compute a composite velocity.
compositeVelocity(KinematicTransform, KinematicTransform) - Static method in interface org.orekit.frames.KinematicTransform: Compute a composite velocity.
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.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractAlfriend1999: Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod: Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005: Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997: Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015: Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double, UnivariateIntegrator, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod: Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.
compute(double, double, double, double, double, UnivariateIntegrator, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005: Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.
compute(Cdm, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod: Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, double, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, double, double, UnivariateIntegrator, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod: Compute the probability of collision using an Orekit Conjunction Data Message.
compute(Cdm, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, T, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod: Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, T, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, T, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, T, T, FieldUnivariateIntegrator<T>, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod: Compute the probability of collision using an Orekit Conjunction Data Message.
compute(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod: Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldOrbit<T>, FieldStateCovariance<T>, T, FieldOrbit<T>, FieldStateCovariance<T>, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldOrbit<T>, FieldStateCovariance<T>, T, FieldOrbit<T>, FieldStateCovariance<T>, T, FieldUnivariateIntegrator<T>, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod: Compute the probability of collision using parameters necessary for creating a collision definition instance.
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(Orbit, StateCovariance, double, Orbit, StateCovariance, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(Orbit, StateCovariance, double, Orbit, StateCovariance, double, UnivariateIntegrator, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod: Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(Orbit, StateCovariance, Orbit, StateCovariance, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(Orbit, StateCovariance, Orbit, StateCovariance, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod: Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(Orbit, StateCovariance, Orbit, StateCovariance, double, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldShortTermEncounter2DDefinition<T>) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using given collision definition.
compute(FieldShortTermEncounter2DDefinition<T>, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod: Compute the probability of collision using given collision definition.
compute(FieldShortTermEncounter2DDefinition<T>, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using given collision definition.
compute(FieldShortTermEncounter2DDefinition<T>, FieldUnivariateIntegrator<T>, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod: Compute the probability of collision using given collision definition.
compute(ShortTermEncounter2DDefinition) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using given collision definition.
compute(ShortTermEncounter2DDefinition, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod: Compute the probability of collision using given collision definition.
compute(ShortTermEncounter2DDefinition, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using given collision definition.
compute(ShortTermEncounter2DDefinition, UnivariateIntegrator, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod: Compute the probability of collision using a given collision definition.
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(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractAlfriend1999: Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod: Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005: Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997: Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015: Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T, FieldUnivariateIntegrator<T>, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod: Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.
compute(T, T, T, T, T, FieldUnivariateIntegrator<T>, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005: Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.
computeAccelerationInJ2Frame(FieldVector3D<T>, double, double, T) - Static method in class org.orekit.forces.gravity.J2OnlyPerturbation: Compute acceleration in J2 frame.
computeAccelerationInJ2Frame(Vector3D, double, double, double) - Static method in class org.orekit.forces.gravity.J2OnlyPerturbation: Compute acceleration in J2 frame.
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.
computeAlbedo(AbsoluteDate, double) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Compute Earth albedo.
computeAlbedo(FieldAbsoluteDate<T>, T) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Compute Earth albedo.
computeC2Z(DSSTJ2SquaredClosedFormContext) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel: Get the value of the Zeis constant.
computeC2Z(FieldDSSTJ2SquaredClosedFormContext<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel: Get the value of the Zeis constant.
computeCandidateSolution(SpacecraftState, int) - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting: Form solution container with input initial state.
computeCandidateSolution(SpacecraftState, int) - Method in class org.orekit.control.indirect.shooting.AbstractFixedInitialCartesianSingleShooting: Form solution container with input initial state.
computeChecksum(String) - Static method in class org.orekit.files.iirv.terms.CheckSumTerm: Computes the sum of the decimal equivalent of characters in the line, counting spaces as 0 and negative signs as 1.
computeCombinedCovarianceInEncounterFrame() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the combined covariance expressed in the encounter frame.
computeCombinedCovarianceInEncounterFrame() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the combined covariance expressed in the encounter frame.
computeCombinedCovarianceInReferenceTNW() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Takes both covariance matrices (expressed in their respective RTN local orbital frame) from reference and other collision object with which this instance was created and sum them in the reference collision object TNW local orbital frame.
computeCombinedCovarianceInReferenceTNW() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Takes both covariance matrices (expressed in their respective RTN local orbital frame) from reference and other collision object with which this instance was created and sum them in the reference collision object TNW local orbital frame.
computeCommonParametersWith(SpacecraftState[], boolean) - Method in class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement: Compute common estimation parameters.
computeCommonParametersWithDerivatives(SpacecraftState) - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement: Compute common estimation parameters.
computeCommonParametersWithout(SpacecraftState) - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement: Compute common estimation parameters.
computeCommonParametersWithout(SpacecraftState[], boolean) - Method in class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement: Compute common estimation parameters.
computeCoppolaEncounterDuration() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the Encounter duration (s) evaluated using Coppola's formula described in : "COPPOLA, Vincent, et al.
computeCoppolaEncounterDuration() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the Encounter duration (s) evaluated using Coppola's formula described in : "COPPOLA, Vincent, et al.
computeDeltaPV(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldExtremumApproachDetector: Compute the relative PV between primary and secondary objects.
computeDeltaPV(SpacecraftState) - Method in class org.orekit.propagation.events.ExtremumApproachDetector: Compute the relative PV between primary and secondary objects.
computeDerivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations: Compute differential equations for main state.
computeDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations: Compute differential equations for main state.
computeElementaryFlux(FieldSpacecraftState<T>, FieldVector3D<T>, FieldVector3D<T>, OneAxisEllipsoid, T) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Compute elementary rediffused flux on satellite.
computeElementaryFlux(SpacecraftState, Vector3D, Vector3D, OneAxisEllipsoid, double) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Compute elementary rediffused flux on satellite.
computeEmissivity(AbsoluteDate, double) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Compute Earth emisivity.
computeEmissivity(FieldAbsoluteDate<T>, T) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Compute Earth emisivity.
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(double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear: 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(T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear: Compute the roots for the Hansen coefficients and their derivatives.
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)
computeInnovationVector(EstimatedMeasurement<?>) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil: Compute the unnormalized innovation vector from the given predicted measurement.
computeInnovationVector(EstimatedMeasurement<?>, double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil: Compute the normalized innovation vector from the given predicted measurement.
computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit, StateCovariance>>, Orbit) - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator: Compute the interpolated covariance expressed in the interpolated orbit frame.
computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit, StateCovariance>>, Orbit) - Method in class org.orekit.propagation.StateCovarianceBlender: Compute the interpolated covariance expressed in the interpolated orbit frame.
computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit, StateCovariance>>, Orbit) - Method in class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator: Compute the interpolated covariance expressed in the interpolated orbit frame.
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.
computeKeplerianDurationFromPreviousApoapsis(double, double) - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory: Method computing time elapsed since last apoapsis, assuming Keplerian motion.
computeKeplerianDurationFromPreviousPeriapsis(double, double) - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory: Method computing time elapsed since last periapsis, assuming Keplerian motion.
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.
computeMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeMeanEquinoctialSecondOrderTerms(DSSTJ2SquaredClosedFormContext) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.J2SquaredModel: Compute the J2-squared second-order terms in equinoctial elements.
computeMeanEquinoctialSecondOrderTerms(DSSTJ2SquaredClosedFormContext) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel: Compute the J2-squared second-order terms in equinoctial elements.
computeMeanEquinoctialSecondOrderTerms(FieldDSSTJ2SquaredClosedFormContext<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.J2SquaredModel: Compute the J2-squared second-order terms in equinoctial elements.
computeMeanEquinoctialSecondOrderTerms(FieldDSSTJ2SquaredClosedFormContext<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel: Compute the J2-squared second-order terms in equinoctial elements.
computeMeanOrbit(FieldOrbit<T>, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, double, double, double, double, double, double, double, OsculatingToMeanConverter) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, double, double, double, double, double, double, double, OsculatingToMeanConverter) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, int) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, double, double, double, double, double, double, double, OsculatingToMeanConverter) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, double, double, double, double, double, double, double, OsculatingToMeanConverter) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, double, OsculatingToMeanConverter) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, double, int) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, int) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: 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.
computeMeanState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>, OsculatingToMeanConverter) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Conversion from osculating to mean orbit.
computeMeanState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Conversion from osculating to mean orbit.
computeMeanState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Conversion from osculating to mean orbit.
computeMeanState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>, OsculatingToMeanConverter) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Conversion from osculating to mean orbit.
computeMissDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the miss distance at time of closest approach.
computeMissDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the miss distance at time of closest approach.
computeMODIP(double, double) - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickGalileo: Compute modip for a location.
computeMODIP(double, double) - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickItu: Compute modip for a location.
computeMODIP(double, double) - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickModel: Compute modip for a location.
computeMODIP(T, T) - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickGalileo: Compute modip for a location.
computeMODIP(T, T) - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickItu: Compute modip for a location.
computeMODIP(T, T) - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickModel: Compute modip for a location.
computeOsculatingState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Conversion from mean to osculating orbit.
computeOsculatingState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Conversion from mean to osculating orbit.
computeOtherPositionInCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the other collision object position projected onto the collision plane.
computeOtherPositionInCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the other collision object position projected onto the collision plane.
computeOtherPositionInRotatedCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the other collision object position in the rotated collision plane.
computeOtherPositionInRotatedCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the other collision object position in the rotated collision plane.
computeOtherPositionInRotatedCollisionPlane(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the other collision object position in the rotated collision plane.
computeOtherPositionInRotatedCollisionPlane(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the other collision object position in the rotated collision plane.
computeOtherRelativeToReferencePVInReferenceInertial() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the other collision position and velocity relative to the reference collision object.
computeOtherRelativeToReferencePVInReferenceInertial() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the other collision position and velocity relative to the reference collision object.
computeProjectedAndDiagonalizedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the combined covariance matrix diagonalized and projected onto the collision plane.
computeProjectedAndDiagonalizedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the combined covariance matrix diagonalized and projected onto the collision plane.
computeProjectedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the projected combined covariance matrix onto the collision plane.
computeProjectedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the projected combined covariance matrix onto the collision plane.
computeProjectionMatrix() - Method in interface org.orekit.frames.encounter.EncounterLOF: Get the 2x3 projection matrix that projects values expressed in this encounter local orbital frame to the collision plane.
computeProjectionMatrix(Field<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF: Get the 2x3 projection matrix that projects values expressed in this encounter local orbital frame to the collision plane defined by this same encounter local orbital frame.
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).
computeReferenceInertialToCollisionPlaneProjectionMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the projection matrix from the reference collision object inertial frame to the collision plane.
computeReferenceInertialToCollisionPlaneProjectionMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the projection matrix from the reference collision object inertial frame to the collision plane.
computeSemiMajorAxis() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Compute the semi-major axis from the mean motion of the TLE and the gravitational parameter from TLEConstants.
computeSemiMajorAxis() - Method in class org.orekit.propagation.analytical.tle.TLE: Compute the semi-major axis from the mean motion of the TLE and the gravitational parameter from TLEConstants.
computeSolarFlux(FieldVector3D<T>) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Compute total solar flux impacting Earth.
computeSolarFlux(Vector3D) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Compute total solar flux impacting Earth.
computeSquaredMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeSquaredMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeSquaredMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeSquaredMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeSquaredMahalanobisDistance(double, double, double, double) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the squared Mahalanobis distance.
computeSquaredMahalanobisDistance(FieldVector2D<T>, FieldMatrix<T>) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the squared Mahalanobis distance.
computeSquaredMahalanobisDistance(Vector2D, RealMatrix) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Compute the squared Mahalanobis distance.
computeSquaredMahalanobisDistance(T, T, T, T) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Compute the squared Mahalanobis distance.
computeValue(double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max: Compute the value of the probability of collision.
computeValue(T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max: Compute the value of the probability of collision.
computeValueFromString(String) - Static method in class org.orekit.files.iirv.terms.base.LongValuedIIRVTerm: Parses a string as a long, removing any leading spaces.
computeValueFromString(String, int) - Static method in class org.orekit.files.iirv.terms.base.DoubleValuedIIRVTerm: Compute the double value of the term from a given String.
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(FieldGeodeticPoint<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, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel: This method allows the computation of the zenith hydrostatic and zenith wet delay.
CONE - org.orekit.files.ccsds.ndm.odm.ocm.ShadowModel: Cone model, umbra only.
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.
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.
ConicallyShadowedLightFluxModel - Class in org.orekit.forces.radiation: Class defining a flux model from a single occulted body, casting a shadow on a spherical occulting body.
ConicallyShadowedLightFluxModel(double, double, ExtendedPositionProvider, double) - Constructor for class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel: Constructor with default event detection settings.
ConicallyShadowedLightFluxModel(double, double, ExtendedPositionProvider, double, EventDetectionSettings) - Constructor for class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel: Constructor.
ConicallyShadowedLightFluxModel(double, ExtendedPositionProvider, double) - Constructor for class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel: Constructor with default value for reference flux.
CONJUNCTION_ID - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey: The Originator’s ID that uniquely identifies the conjunction to which the message refers.
CONNECTION_ERROR - org.orekit.errors.OrekitMessages: CONNECTION_ERROR.
CONSIDER_N - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey: Number of consider parameters.
CONSIDER_PARAMS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey: Description of consider parameters.
CONSTANT - org.orekit.files.ccsds.ndm.tdm.RangeMode: Range tones have constant frequency.
constantAfter() - Method in class org.orekit.utils.WaypointPVBuilder: Indicate the resulting PVCoordinatesProvider provide a constant location of the last waypoint after to the last time.
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.
ConstantAzimuthalGradientProvider - Class in org.orekit.models.earth.troposphere: Constant provider for AzimuthalGradientCoefficients and FieldAzimuthalGradientCoefficients.
ConstantAzimuthalGradientProvider(AzimuthalGradientCoefficients) - Constructor for class org.orekit.models.earth.troposphere.ConstantAzimuthalGradientProvider: Simple constructor.
constantBefore() - Method in class org.orekit.utils.WaypointPVBuilder: Indicate the resulting PVCoordinatesProvider provide a constant location of the first waypoint prior to the first time.
ConstantOffsetTimeScale - Class in org.orekit.time: Base class for time scales with constant offset with respect to to TAI.
ConstantOffsetTimeScale(String, TimeOffset) - Constructor for class org.orekit.time.ConstantOffsetTimeScale: Simple constructor.
ConstantPressureTemperatureHumidityProvider - Class in org.orekit.models.earth.weather: Provider for constant weather parameters.
ConstantPressureTemperatureHumidityProvider(PressureTemperatureHumidity) - Constructor for class org.orekit.models.earth.weather.ConstantPressureTemperatureHumidityProvider: 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.
ConstantPVCoordinatesProvider - Class in org.orekit.utils: Provider based on a single point.
ConstantPVCoordinatesProvider(Vector3D, Frame) - Constructor for class org.orekit.utils.ConstantPVCoordinatesProvider: Create the PVCoordinatesProvider from a fixed point in a frame.
ConstantPVCoordinatesProvider(GeodeticPoint, OneAxisEllipsoid) - Constructor for class org.orekit.utils.ConstantPVCoordinatesProvider: Create a the provider from a fixed lat/lon/alt on a central body.
ConstantPVCoordinatesProvider(PVCoordinates, Frame) - Constructor for class org.orekit.utils.ConstantPVCoordinatesProvider: Create the PVCoordinatesProvider from a fixed point in a frame.
Constants - Interface in org.orekit.utils: Set of useful physical constants.
ConstantThrustManeuver - Class in org.orekit.forces.maneuvers: This class implements a simple maneuver with constant thrust.
ConstantThrustManeuver(AttitudeProvider, DateBasedManeuverTriggers, AbstractConstantThrustPropulsionModel) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver: Simple constructor for a constant direction and 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, 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) - 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, double, double, AttitudeProvider, Vector3D, Control3DVectorCostType, 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.
ConstantTroposphericModel - Class in org.orekit.models.earth.troposphere: Defines a constant tropospheric model.
ConstantTroposphericModel(TroposphericDelay) - Constructor for class org.orekit.models.earth.troposphere.ConstantTroposphericModel: Simple constructor.
ConstantValuedIIRVTerm - Class in org.orekit.files.iirv.terms.base: Term in an IIRV Vector representing a constant String value.
ConstantValuedIIRVTerm(String) - Constructor for class org.orekit.files.iirv.terms.base.ConstantValuedIIRVTerm: Constructs a ConstantValuedIIRVTerm instance with a given String value.
ConstantViennaAProvider - Class in org.orekit.models.earth.troposphere: Provider for constant Vienna A coefficients.
ConstantViennaAProvider(ViennaACoefficients) - Constructor for class org.orekit.models.earth.troposphere.ConstantViennaAProvider: Simple constructor.
CONSTELLATION - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey: Name of the constellation this space object belongs to.
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 - 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: Empty constructor.
CONTINUOUS - org.orekit.files.ccsds.definitions.DutyCycleType: Full/continuous thrust.
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.
ContinuousScheduler(MeasurementBuilder<T>, DatesSelector, Predicate<EstimatedMeasurementBase<T>>) - Constructor for class org.orekit.estimation.measurements.generation.ContinuousScheduler: Simple constructor.
Control3DVectorCostType - Enum in org.orekit.forces.maneuvers: Enumerate on types of cost for 3D control vector (thrust as a force or acceleration, including an impulse) at a given time.
ControlSwitchDetector - Class in org.orekit.control.indirect.adjoint.cost: Abstract event detector for singularities in adjoint dynamics.
ControlSwitchDetector(EventDetectionSettings) - Constructor for class org.orekit.control.indirect.adjoint.cost.ControlSwitchDetector: Constructor.
convert() - Method in class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter: Convert an osculating orbit into a mean orbit, in DSST sense.
convert(double) - Method in class org.orekit.utils.units.UnitsConverter: Convert a value.
convert(double[]) - Method in interface org.orekit.data.SimpleTimeStampedTableParser.RowConverter: Convert a row.
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(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(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, 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(FieldPressureTemperatureHumidity<T>, T) - Method in class org.orekit.models.earth.weather.HeightDependentPressureTemperatureHumidityConverter: Convert weather parameters.
convert(PressureTemperatureHumidity, double) - Method in class org.orekit.models.earth.weather.HeightDependentPressureTemperatureHumidityConverter: Convert weather parameters.
convert(Propagator, double, int, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Convert a propagator to another.
convert(Propagator, double, int, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter: Convert a propagator into another one.
convert(Propagator, double, int, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Convert a propagator to another.
convert(Propagator, double, int, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter: Convert a propagator into another one.
CONVERT_COMPATIBLE - org.orekit.files.ccsds.ndm.ParsedUnitsBehavior: Allow compatible units, performing conversion.
convert2DigitsYear(int) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils: Convert a 2 digits year to a complete year.
convertAlpha(PositionAngleType, double, double, double, PositionAngleType) - Static method in class org.orekit.orbits.CircularLatitudeArgumentUtility: Convert argument of latitude.
convertAlpha(PositionAngleType, T, T, T, PositionAngleType) - Static method in class org.orekit.orbits.FieldCircularLatitudeArgumentUtility: Convert argument of latitude.
convertAnomaly(PositionAngleType, double, double, PositionAngleType) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility: Convert anomaly.
convertAnomaly(PositionAngleType, T, T, PositionAngleType) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility: Convert anomaly.
convertFromLofType(LOFType, RealMatrix, Vector3D, Vector3D) - Static method in class org.orekit.utils.CartesianCovarianceUtils: Convert input position-velocity covariance matrix from local frame to reference one.
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.
convertL(PositionAngleType, double, double, double, PositionAngleType) - Static method in class org.orekit.orbits.EquinoctialLongitudeArgumentUtility: Convert argument of longitude.
convertL(PositionAngleType, T, T, T, PositionAngleType) - Static method in class org.orekit.orbits.FieldEquinoctialLongitudeArgumentUtility: Convert argument of longitude.
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.
convertToAveraged(Orbit) - Method in interface org.orekit.propagation.conversion.averaging.converters.OsculatingToAveragedConverter: Convert osculating orbit to averaged orbital state according to underlying theory.
convertToAveraged(Orbit) - Method in class org.orekit.propagation.conversion.averaging.converters.OsculatingToBrouwerLyddaneConverter: Convert osculating orbit to averaged orbital state according to underlying theory.
convertToAveraged(Orbit) - Method in class org.orekit.propagation.conversion.averaging.converters.OsculatingToDSST6X0Converter: Convert osculating orbit to averaged orbital state according to underlying theory.
convertToAveraged(Orbit) - Method in class org.orekit.propagation.conversion.averaging.converters.OsculatingToEcksteinHechlerConverter: Convert osculating orbit to averaged orbital state according to underlying theory.
convertToAveraged(Orbit) - Method in class org.orekit.propagation.conversion.averaging.converters.OsculatingToSGP4Converter: Convert osculating orbit to averaged orbital state according to underlying theory.
convertToFieldOrbit(Field<T>, Orbit) - Method in enum org.orekit.orbits.OrbitType: Convert an orbit to the "Fielded" instance type.
convertToLofType(Vector3D, Vector3D, RealMatrix, LOFType) - Static method in class org.orekit.utils.CartesianCovarianceUtils: Convert input position-velocity covariance matrix from reference frame to local one.
convertToMean(FieldOrbit<T>) - Method in class org.orekit.propagation.conversion.osc2mean.FixedPointConverter: Converts an osculating orbit into a mean orbit.
convertToMean(FieldOrbit<T>) - Method in class org.orekit.propagation.conversion.osc2mean.LeastSquaresConverter: Converts an osculating orbit into a mean orbit.
convertToMean(FieldOrbit<T>) - Method in interface org.orekit.propagation.conversion.osc2mean.OsculatingToMeanConverter: Converts an osculating orbit into a mean orbit.
convertToMean(Orbit) - Method in class org.orekit.propagation.conversion.osc2mean.FixedPointConverter: Converts an osculating orbit into a mean orbit.
convertToMean(Orbit) - Method in class org.orekit.propagation.conversion.osc2mean.LeastSquaresConverter: Converts an osculating orbit into a mean orbit.
convertToMean(Orbit) - Method in interface org.orekit.propagation.conversion.osc2mean.OsculatingToMeanConverter: Converts an osculating orbit into a mean orbit.
convertType(FieldOrbit<T>) - Method in enum org.orekit.orbits.OrbitType: Convert an orbit to the instance type.
convertType(Orbit) - Method in enum org.orekit.orbits.OrbitType: Convert an orbit to the instance type.
COORDINATE_SYSTEM_TERM_LENGTH - Static variable in class org.orekit.files.iirv.terms.CoordinateSystemTerm: The length of the IIRV term within the message.
COORDINATE_SYSTEM_TERM_PATTERN - Static variable in class org.orekit.files.iirv.terms.CoordinateSystemTerm: Regular expression that ensures the validity of string values for this term.
CoordinateSystemTerm - Class in org.orekit.files.iirv.terms: 1-character representing the coordinate system associated with the state variables.
CoordinateSystemTerm(long) - Constructor for class org.orekit.files.iirv.terms.CoordinateSystemTerm: Constructor.
CoordinateSystemTerm(String) - Constructor for class org.orekit.files.iirv.terms.CoordinateSystemTerm: Constructor.
copy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Copy the instance, making sure mandatory fields have been initialized.
copy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Copy the instance, making sure mandatory fields have been initialized.
copyObservationData(ObservationData) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother: Copy an ObservationData object.
copyObservationData(ObservationData) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother: Copy an ObservationData object.
copySelectionSettings(GNSSOrbitalElementsDriversProvider) - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Copy drivers selection settings from another instance.
copyStates() - Method in class org.orekit.propagation.sampling.FieldPropagationStepRecorder: Copy the current saved steps.
copyStates() - Method in class org.orekit.propagation.sampling.PropagationStepRecorder: Copy the current saved steps.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.BeidouGeo: Select the /** 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(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Galileo: Select the /** 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(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Glonass: Select the /** 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(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIF: Select the /** 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.BeidouGeo: 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(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.Galileo: 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(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.Glonass: 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(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIF: 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.
CORRECTION_ABERRATION_DIURNAL - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Diurnal aberration correction entry.
CORRECTION_ABERRATION_YEARLY - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Yearly aberration correction entry.
CORRECTION_ANGLE_1 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Angle 1 correction entry.
CORRECTION_ANGLE_2 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Angle 2 correction entry.
CORRECTION_DOPPLER - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Doppler correction entry.
CORRECTION_MAG - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Magnitude correction entry.
CORRECTION_RANGE - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Range correction entry (beware the unit is Range Units here).
CORRECTION_RCS - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Radar Cross Section correction entry.
CORRECTION_RECEIVE - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Receive correction entry.
CORRECTION_TRANSMIT - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Transmit correction entry.
CorrectionApplied - Enum in org.orekit.files.ccsds.ndm.tdm: Indicator for corrections application.
CORRECTIONS_APPLIED - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Applied correction entry.
CORRUPTED_FILE - org.orekit.errors.OrekitMessages: CORRUPTED_FILE.
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.
CountAndContinue - Class in org.orekit.propagation.events.handlers: Event handler counting event occurrences and always returning Action.CONTINUE.
CountAndContinue() - Constructor for class org.orekit.propagation.events.handlers.CountAndContinue: Constructor with count initialized at zero.
CountAndContinue(int) - Constructor for class org.orekit.propagation.events.handlers.CountAndContinue: Constructor.
countAtDate(AbsoluteDate) - Method in class org.orekit.time.SatelliteClockScale: Compute clock count corresponding to some date.
CountingHandler - Class in org.orekit.propagation.events.handlers: Abstract class for handlers counting event occurrences.
CountingHandler(int, Action) - Constructor for class org.orekit.propagation.events.handlers.CountingHandler: Constructor.
COUNTRY - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey: Name of the country where the space object owner is based.
cov - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey: Covariance time history section.
cov - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey: Covariance time history section.
COV - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey: Covariance time history section.
COV - org.orekit.files.ccsds.ndm.adm.acm.AcmElements: Covariance time history.
COV - org.orekit.files.ccsds.ndm.odm.ocm.OcmDataSubStructureKey: Covariance time history section.
COV - org.orekit.files.ccsds.ndm.odm.ocm.OcmElements: Covariance time history.
COV_BASIS - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey: Basis of this covariance time history data.
COV_BASIS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey: Basis of this covariance time history data.
COV_BASIS_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey: Identification number of the orbit determination or simulation upon which this covariance is based.
COV_BASIS_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey: Identification number of the orbit determination or simulation upon which this covariance is based.
COV_CONFIDENCE - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey: A measure of the confidence in the covariance errors matching reality.
COV_CONFIDENCE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey: Masure of confidence in covariance error matching reality.
COV_CONFIDENCE_METHOD - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey: The method used for the calculation of COV_CONFIDENCE.
COV_FRAME_EPOCH - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey: Epoch of the covariance reference frame.
COV_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey: Covariance identification number.
COV_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey: Covariance identification number.
COV_LINE - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.Acm: Covariance line element for XML messages.
COV_LINE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm: Covariance line element for XML messages.
COV_NEXT_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey: Identification number of next covariance.
COV_ORDERING - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey: Covariance ordering.
COV_PREV_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey: Identification number of previous covariance.
COV_PREV_ID - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey: Identification number of previous covariance.
COV_REF_FRAME - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey: Reference frame of the covariance.
COV_REF_FRAME - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Coordinate system for covariance matrix.
COV_REF_FRAME - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey: Reference frame of the covariance.
COV_SCALE_MAX - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey: Maximum scale factor to apply to achieve realism.
COV_SCALE_MIN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey: Minimum scale factor to apply to achieve realism.
COV_TYPE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey: Covariance element set type.
COV_TYPE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey: Type of attitude error state.
COV_TYPE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey: Covariance element set type.
COV_UNITS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey: SI units for each elements of the covariance.
COVARIANCE_METHOD - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey: Method used to calculate the covariance.
COVARIANCE_MUST_BE_SQUARE - org.orekit.errors.OrekitMessages: COVARIANCE_MUST_BE_SQUARE.
COVARIANCE_SOURCE - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey: The source from which the covariance data used in the report for both Object 1 and Object 2 originates.
covarianceMatrix - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey: Covariance Matrix section.
CovarianceMatrixProvider - Interface in org.orekit.estimation.sequential: Provider for process noise matrices.
CovarianceMethod - Enum in org.orekit.files.ccsds.ndm.cdm: Maneuvrable possibilities used in CCSDS Conjunction Data Messages.
CP - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey: Center of pressure.
CP_REF_FRAME - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey: Reference frame for center of pressure.
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_UNEXPECTED_END_OF_FILE - org.orekit.errors.OrekitMessages: CPF_UNEXPECTED_END_OF_FILE.
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(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: Empty constructor.
CPFParser - Class in org.orekit.files.ilrs: A parser for the CPF orbit file format.
CPFParser() - Constructor for class org.orekit.files.ilrs.CPFParser: Default constructor.
CPFParser(double, int, IERSConventions, TimeScale, Frames) - Constructor for class org.orekit.files.ilrs.CPFParser: Constructor.
CPFWriter - Class in org.orekit.files.ilrs: An CPF Writer class that can take in a general EphemerisFile object and export it as a valid CPF file.
CPFWriter(CPFHeader, TimeScale) - Constructor for class org.orekit.files.ilrs.CPFWriter: Constructor.
CPFWriter(CPFHeader, TimeScale, boolean) - Constructor for class org.orekit.files.ilrs.CPFWriter: Constructor.
CR - org.orekit.files.rinex.clock.RinexClock.ClockDataType: Calibration measurement for a single GPS receiver.
CR_AREA_OVER_MASS - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey: The object’s Cr x A/m used to propagate the state vector and covariance to TCA.
CR_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [1,1].
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.
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<STMEquations>, 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.
CRC_INDEX - Static variable in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Index of cosine on radius in the list returned by GNSSOrbitalElementsDriversProvider.getParametersDrivers().
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_UNEXPECTED_END_OF_FILE - org.orekit.errors.OrekitMessages: CRD_UNEXPECTED_END_OF_FILE.
CRD.AnglesMeasurement - Class in org.orekit.files.ilrs: Pointing angles record.
CRD.Calibration - Class in org.orekit.files.ilrs: Calibration Record.
CRD.CalibrationDetail - Class in org.orekit.files.ilrs: Calibration Detail Record.
CRD.CRDDataBlock - Class in org.orekit.files.ilrs: Data block containing a set of data contain in the CRD file.
CRD.FrRangeMeasurement - Class in org.orekit.files.ilrs: Range record -- Full rate, Sampled Engineering/Quicklook.
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.NptRangeMeasurement - Class in org.orekit.files.ilrs: Range record -- Normal Point.
CRD.RangeMeasurement - Class in org.orekit.files.ilrs: Range record.
CRD.RangeSupplement - Class in org.orekit.files.ilrs: Range Supplement Record.
CRD.SessionStatistics - Class in org.orekit.files.ilrs: Session (Pass) Statistics 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: Constructor.
CRDConfiguration.BaseConfiguration - Class in org.orekit.files.ilrs: Base class for configuration record.
CRDConfiguration.CalibrationTargetConfiguration - Class in org.orekit.files.ilrs: Container for calibration target configuration record.
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: Empty constructor.
CRDHeader.DataType - Enum in org.orekit.files.ilrs: Data type for CRD data.
CRDHeader.RangeType - Enum in org.orekit.files.ilrs: Range type for SLR data.
CRDOT_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [4,3].
CRDOT_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [4,1].
CRDOT_RDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [4,4].
CRDOT_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [4,2].
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(OneAxisEllipsoid, GeodeticPoint) - Static method in class org.orekit.gnss.DOPComputer: Creates a DOP computer for one location.
create(CenterName) - Static method in class org.orekit.files.ccsds.definitions.BodyFacade: Create a body facade from an input center name.
create(CenterName, CelestialBodies) - Static method in class org.orekit.files.ccsds.definitions.BodyFacade: Create a body facade from an input center name.
create(CenterName, DataContext) - Static method in class org.orekit.files.ccsds.definitions.BodyFacade: Create a body facade from an input center name.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.AbstractDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.AlignmentDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.AltitudeDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.AngularSeparationDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.ApsideDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.BetaAngleDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.BooleanDetector
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.CylindricalShadowEclipseDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.DateDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.EclipseDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.ElevationDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.ElevationExtremumDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.ExtremumApproachDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.FieldOfViewDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.FootprintOverlapDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.FunctionalDetector
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.GeographicZoneDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.GroundAtNightDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.HaloXZPlaneCrossingDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.LatitudeRangeCrossingDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.LongitudeRangeCrossingDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.MagneticFieldDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.NegateDetector
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.NodeDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.PositionAngleDetector: Build a new instance.
create(EventDetectionSettings, EventHandler) - Method in class org.orekit.propagation.events.RelativeDistanceDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldApsideDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldBetaAngleDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldBooleanDetector
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldCylindricalShadowEclipseDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldDateDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldElevationDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldElevationExtremumDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldExtremumApproachDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldLatitudeRangeCrossingDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldLongitudeCrossingDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldNegateDetector
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector: Build a new instance.
create(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Method in class org.orekit.propagation.events.FieldRelativeDistanceDetector: Build a new instance.
create(AbsoluteDate, GeodeticPoint, AbsoluteDate, GeodeticPoint, OneAxisEllipsoid) - Method in interface org.orekit.utils.WaypointPVBuilder.InterpolationFactory: Create a PVCoordinatesProvider which interpolates between the provided waypoints.
create(IERSConventions, double, double, DataContext, AbsoluteDate, RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder: Build an instance.
create(IERSConventions, double, double, DataContext, AbsoluteDate, RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.ParserBuilder: Build an instance.
create(IERSConventions, double, double, DataContext, AbsoluteDate, RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.WriterBuilder: Build an 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(double) - Method in interface org.orekit.time.TimeScales: Build an instance corresponding to a Besselian Epoch (BE).
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).
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.
createDataFields(boolean, boolean, RotationOrder, boolean, TimeStampedAngularCoordinates, Formatter) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType: Get the attitude data fields corresponding to the attitude type.
createDefaultDut1FitterLongTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter: Create fitter with default parameters adapted for fitting orientation parameters dUT1 and LOD for long term prediction.
createDefaultDut1FitterShortTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter: Create fitter with default parameters adapted for fitting orientation parameters dUT1 and LOD for short term prediction.
createDefaultNutationFitterLongTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter: Create fitter with default parameters adapted for fitting nutation parameters dx and dy for long term prediction.
createDefaultNutationFitterShortTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter: Create fitter with default parameters adapted for fitting nutation parameters dx and dy for long term prediction.
createDefaultPoleFitterLongTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter: Create fitter with default parameters adapted for fitting pole parameters Xp and Yp for long term prediction.
createDefaultPoleFitterShortTermPrediction() - Static method in class org.orekit.frames.SingleParameterFitter: Create fitter with default parameters adapted for fitting pole parameters Xp and Yp for long term prediction.
createDriver(String) - Static method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Create parameter driver.
createFieldInitialStateWithMassAndAdjoint(double, double[]) - Method in class org.orekit.control.indirect.shooting.AbstractFixedInitialCartesianSingleShooting: Create initial Gradient state with input mass and adjoint vector, the latter being the independent variables.
createFieldState(FieldAbsoluteDate<T>, T[], T, T[]) - Method in class org.orekit.control.indirect.shooting.AbstractFixedInitialCartesianSingleShooting: Create state.
createFilter(ObservationData, ObservationData, ObservationData, SatelliteSystem) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother: Creates an Hatch filter given initial data.
createFilter(ObservationData, ObservationData, SatelliteSystem) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother: Creates an Hatch filter given initial data.
createFinal(GeodeticPoint) - Method in class org.orekit.utils.WaypointPVBuilder: Create the final provider.
createForces(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.propagation.conversion.averaging.DSST6X0OrbitalState: Create collection of fist 6 zonal DSST forces.
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.Ephemeris: Create the harvester suitable for propagator.
createHarvester(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator: 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.
createInitial(GeodeticPoint) - Method in class org.orekit.utils.WaypointPVBuilder: Create the initial provider.
createInitialOrbit() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Build an initial orbit using the current selected parameters.
createInitialStateWithMass(double) - Method in class org.orekit.control.indirect.shooting.AbstractFixedInitialCartesianSingleShooting: Create initial state with input mass.
createJDDate(int, double, TimeScale) - Static method in class org.orekit.time.AbsoluteDate: Build an instance corresponding to a Julian Day date.
createJDDate(int, double, TimeScale, 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.
createJDDate(int, T, TimeScale, 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(double) - Method in interface org.orekit.time.TimeScales: Build an instance corresponding to a Julian Epoch (JE).
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).
createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Create a mapper between raw double components and spacecraft state. /** Simple constructor.
createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Create a mapper between raw double components and spacecraft state. /** Simple constructor.
createMapper(AbsoluteDate, double, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Create a mapper between raw double components and spacecraft state. /** Simple constructor.
createMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Create a mapper between raw double components and spacecraft state. /** Simple constructor.
createMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Create a mapper between raw double components and spacecraft state. /** Simple constructor.
createMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngleType, AttitudeProvider, Frame) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Create a mapper between raw double components and spacecraft state. /** Simple constructor.
createMedian(AbsoluteDate, AbsoluteDate) - Static method in class org.orekit.time.AbsoluteDate: Create an instance as the median data between two existing instances.
createMedian(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Create an instance as the median data between two existing instances.
createMJDDate(int, double, TimeScale) - Static method in class org.orekit.time.AbsoluteDate: Build an instance corresponding to a Modified Julian Day date.
createMJDDate(int, TimeOffset, 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.
CREATION_DATE - org.orekit.files.ccsds.section.HeaderKey: Creation date.
CROSS_SECTIONAL_AREA_TERM_LENGTH - Static variable in class org.orekit.files.iirv.terms.CrossSectionalAreaTerm: The length of the IIRV term within the message.
CROSS_SECTIONAL_AREA_TERM_PATTERN - Static variable in class org.orekit.files.iirv.terms.CrossSectionalAreaTerm: Regular expression that ensures the validity of string values for this term.
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.
CrossSectionalAreaTerm - Class in org.orekit.files.iirv.terms: 5-character average satellite cross-sectional area in square meters with a resolution to the nearest hundredth of a square meter.
CrossSectionalAreaTerm(double) - Constructor for class org.orekit.files.iirv.terms.CrossSectionalAreaTerm: Constructor.
CrossSectionalAreaTerm(String) - Constructor for class org.orekit.files.iirv.terms.CrossSectionalAreaTerm: Constructor.
CRS_INDEX - Static variable in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Index of sine on radius in the list returned by GNSSOrbitalElementsDriversProvider.getParametersDrivers().
CSCALE_FACTOR - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey: The (median) suggested covariance scale factor.
CSCALE_FACTOR_MAX - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey: The maximum suggested covariance scale factor.
CSCALE_FACTOR_MIN - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey: The minimum suggested covariance scale factor.
CSIG3EIGVEC3 - org.orekit.files.ccsds.ndm.cdm.AltCovarianceType: Sigma/Eigenvector Format.
CSIG3EIGVEC3 - org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovarianceKey: The 3x3 positional covariance one-sigma dispersions corresponding to the major, intermediate and minor eigenvalues, followed by the associated eigenvectors.
CSRP_DRG - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [8,7].
CSRP_DRG - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [8,7].
CSRP_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [8,3].
CSRP_NDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [8,6].
CSRP_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [8,1].
CSRP_RDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [8,4].
CSRP_SRP - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [8,9].
CSRP_SRP - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [8,9].
CSRP_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [8,2].
CSRP_TDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [8,5].
CSRP_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [8,1].
CSRP_XDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [8,4].
CSRP_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [8,2].
CSRP_YDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [8,5].
CSRP_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [8,3].
CSRP_ZDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [8,6].
CSS - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment: Coarse Sun Sensor.
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.
CssiSpaceWeatherData(String, CssiSpaceWeatherDataLoader, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Constructor that allows specifying the source of the CSSI space weather file.
CssiSpaceWeatherData(String, CssiSpaceWeatherDataLoader, DataProvidersManager, TimeScale, int, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Constructor that allows specifying the source of the CSSI space weather file and customizable thread safe cache configuration.
CssiSpaceWeatherData(DataSource) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Simple constructor which use the default data context.
CssiSpaceWeatherData(DataSource, CssiSpaceWeatherDataLoader, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Simple constructor.
CssiSpaceWeatherData(DataSource, CssiSpaceWeatherDataLoader, TimeScale, int, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Simple constructor with customizable thread safe cache configuration.
CssiSpaceWeatherData(DataSource, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData: Simple constructor.
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.
CSTC - Static variable in class org.orekit.files.iirv.terms.OriginIdentificationTerm: Air Force Satellite Control Facility (CSTC) OriginIdentification.
CSTC - Static variable in class org.orekit.files.iirv.terms.RoutingIndicatorTerm: Air Force Satellite Control Facility (CSTC) RoutingIndicator.
CSV_FILENAME - Static variable in class org.orekit.frames.FramesFactory: Default regular expression for the csv files (IAU1980 and IAU2000 compatibles).
CT_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [2,1].
CT_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [2,2].
CTDOT_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [5,3].
CTDOT_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [5,1].
CTDOT_RDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [5,4].
CTDOT_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [5,2].
CTDOT_TDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [5,5].
CTHR_DRG - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [9,7].
CTHR_DRG - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [9,7].
CTHR_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [9,3].
CTHR_NDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [9,6].
CTHR_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [9,1].
CTHR_RDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [9,4].
CTHR_SRP - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [9,8].
CTHR_SRP - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [9,8].
CTHR_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [9,2].
CTHR_TDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [9,5].
CTHR_THR - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey: Object covariance matrix [9,9].
CTHR_THR - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [9,9].
CTHR_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [9,1].
CTHR_XDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [9,4].
CTHR_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [9,2].
CTHR_YDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [9,5].
CTHR_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [9,3].
CTHR_ZDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [9,6].
CUC_INDEX - Static variable in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Index of cosine on latitude argument in the list returned by GNSSOrbitalElementsDriversProvider.getParametersDrivers().
currentInterval(FieldSpacecraftState<T>, boolean) - Method in interface org.orekit.propagation.events.intervals.FieldAdaptableInterval: Get the current value of maximal time interval between events handler checks.
currentInterval(SpacecraftState, boolean) - Method in interface org.orekit.propagation.events.intervals.AdaptableInterval: Get the current value of maximal time interval between events handler checks.
CUS_INDEX - Static variable in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Index of sine on latitude argument in the list returned by GNSSOrbitalElementsDriversProvider.getParametersDrivers().
CX_DOT_X - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [4, 1] element.
CX_DOT_X_DOT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [4, 4] element.
CX_DOT_Y - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [4, 2] element.
CX_DOT_Z - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [4, 3] element.
CX_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [1,1].
CX_X - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [1, 1] element.
CXDOT_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [4,1].
CXDOT_XDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [4,4].
CXDOT_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [4,2].
CXDOT_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [4,3].
CY_DOT_X - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [5, 1] element.
CY_DOT_X_DOT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [5, 4] element.
CY_DOT_Y - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [5, 2] element.
CY_DOT_Y_DOT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [5, 5] element.
CY_DOT_Z - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [5, 3] element.
CY_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [2,1].
CY_X - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [2, 1] element.
CY_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [2,2].
CY_Y - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [2, 2] element.
CYCLE - Static variable in class org.orekit.utils.units.Unit: Cycle unit.
cycleSlipDataSet(String, AbsoluteDate, double, GnssSignal) - 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.
CYDOT_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [5,1].
CYDOT_XDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [5,4].
CYDOT_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [5,2].
CYDOT_YDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [5,5].
CYDOT_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [5,3].
CYLINDRICAL - org.orekit.files.ccsds.ndm.odm.ocm.ShadowModel: Cylindrical model.
CylindricallyShadowedLightFluxModel - Class in org.orekit.forces.radiation: Class defining a flux model with a single occulting body, casting a shadow whose shape is a circular cylinder (equivalent to the light source being infinitely distant).
CylindricallyShadowedLightFluxModel(double, ExtendedPositionProvider, double) - Constructor for class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel: Constructor with default event detection settings.
CylindricallyShadowedLightFluxModel(double, ExtendedPositionProvider, double, EventDetectionSettings) - Constructor for class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel: Constructor.
CylindricallyShadowedLightFluxModel(ExtendedPositionProvider, double) - Constructor for class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel: Constructor with default value for reference flux.
CylindricalShadowEclipseDetector - Class in org.orekit.propagation.events: Event detector for eclipses from a single, infinitely-distant light source, occulted by a spherical central body.
CylindricalShadowEclipseDetector(PVCoordinatesProvider, double, EventDetectionSettings, EventHandler) - Constructor for class org.orekit.propagation.events.CylindricalShadowEclipseDetector: Constructor.
CylindricalShadowEclipseDetector(PVCoordinatesProvider, double, EventHandler) - Constructor for class org.orekit.propagation.events.CylindricalShadowEclipseDetector: Constructor with default detection settings.
CZ_DOT_X - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [6, 1] element.
CZ_DOT_X_DOT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [6, 4] element.
CZ_DOT_Y - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [6, 2] element.
CZ_DOT_Y_DOT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [6, 5] element.
CZ_DOT_Z - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [6, 3] element.
CZ_DOT_Z_DOT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [6, 6] element.
CZ_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [3,1].
CZ_X - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [3, 1] element.
CZ_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [3,2].
CZ_Y - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [3, 2] element.
CZ_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [3,3].
CZ_Z - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Covariance matrix [3, 3] element.
CZDOT_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [6,1].
CZDOT_XDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [6,4].
CZDOT_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [6,2].
CZDOT_YDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [6,5].
CZDOT_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [6,3].
CZDOT_ZDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey: Object covariance matrix [6,6].

D

D - org.orekit.gnss.SignalCode: GPS L1(C/A) + (P2-P1) / QZSS L5D / Beidou Data codes.
D0 - org.orekit.gnss.PredefinedObservationType: Doppler for Rinex3.
D1 - org.orekit.gnss.PredefinedObservationType: Doppler GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.
D1 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage: Identifier for message type.
D1A - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E1 A / Beidou B1 B1A for Rinex3.
D1B - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E1 I/NAV OS/CS/SoL / QZSS geo signal for Rinex3.
D1C - org.orekit.gnss.PredefinedObservationType: Doppler GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.
D1D - org.orekit.gnss.PredefinedObservationType: Doppler Beidou B1 Data for Rinex3.
D1E - org.orekit.gnss.PredefinedObservationType: Doppler QZSS L1 C/B for Rinex4.
D1I - org.orekit.gnss.PredefinedObservationType: Doppler Beidou B1 I for Rinex3.
D1L - org.orekit.gnss.PredefinedObservationType: Doppler GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3, Beidou B1A for Rinex3.03.
D1M - org.orekit.gnss.PredefinedObservationType: Doppler GPS L2 M for Rinex3.
D1N - org.orekit.gnss.PredefinedObservationType: Doppler GPS L1 codeless / Beidou B1 codeless for Rinex3.
D1P - org.orekit.gnss.PredefinedObservationType: Doppler GPS L2 P(AS off) / GLONASS G2 P / Beidou B1 Pilot for Rinex3.
D1S - org.orekit.gnss.PredefinedObservationType: Doppler GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3, Beidou B1A for Rinex3.03.
D1W - org.orekit.gnss.PredefinedObservationType: Doppler GPS L1 Z-tracking and similar (AS on) for Rinex3.
D1X - org.orekit.gnss.PredefinedObservationType: Doppler GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) / Beidou B1 Data+Pilot for Rinex3.
D1Y - org.orekit.gnss.PredefinedObservationType: Doppler GPS L1 Y for Rinex3.
D1Z - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3, Beidou B1A for Rinex3.03.
D2 - org.orekit.gnss.PredefinedObservationType: Doppler GPS L2 / GLONASS G2 / Beidou BO2 for Rinex2.
D2 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage: Identifier for message type.
D2C - org.orekit.gnss.PredefinedObservationType: Doppler GPS L2 C/A / GLONASS G2 C/A for Rinex3.
D2D - org.orekit.gnss.PredefinedObservationType: Doppler GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.
D2I - org.orekit.gnss.PredefinedObservationType: Doppler Beidou B1 I for Rinex3.03.
D2L - org.orekit.gnss.PredefinedObservationType: Doppler GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.
D2M - org.orekit.gnss.PredefinedObservationType: Doppler GPS L2 M for Rinex3.
D2N - org.orekit.gnss.PredefinedObservationType: Doppler GPS L2 codeless for Rinex3.
D2P - org.orekit.gnss.PredefinedObservationType: Doppler GPS L2 P(AS off) / GLONASS G2 P for Rinex3.
D2Q - org.orekit.gnss.PredefinedObservationType: Doppler Beidou B1 Q for Rinex3.03.
D2S - org.orekit.gnss.PredefinedObservationType: Doppler GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.
D2W - org.orekit.gnss.PredefinedObservationType: Doppler GPS L2 Z-tracking and similar (AS on) for Rinex3.
D2X - org.orekit.gnss.PredefinedObservationType: Doppler GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3, Beidou B1 I+Q for Rinex3.03.
D2Y - org.orekit.gnss.PredefinedObservationType: Doppler GPS L2 Y for Rinex3.
D3I - org.orekit.gnss.PredefinedObservationType: Doppler GLONASS G3 I for Rinex3.
D3Q - org.orekit.gnss.PredefinedObservationType: Doppler GLONASS G3 Q for Rinex3.
D3X - org.orekit.gnss.PredefinedObservationType: Doppler GLONASS G3 I+Q for Rinex3.
D4A - org.orekit.gnss.PredefinedObservationType: Doppler GLONASS G1a L1OCd for Rinex3.
D4B - org.orekit.gnss.PredefinedObservationType: Doppler GLONASS G1a L1OCp for Rinex3.
D4X - org.orekit.gnss.PredefinedObservationType: Doppler GLONASS G1a L1OCd+L1OCd for Rinex3.
D5 - org.orekit.gnss.PredefinedObservationType: Doppler GPS L5 / Galileo E5a / SBAS L5 for Rinex2.
D5A - org.orekit.gnss.PredefinedObservationType: Doppler IRNSS L5 A for Rinex3.
D5B - org.orekit.gnss.PredefinedObservationType: Doppler IRNSS L5 B for Rinex3.
D5C - org.orekit.gnss.PredefinedObservationType: Doppler IRNSS L5 C for Rinex3.
D5D - org.orekit.gnss.PredefinedObservationType: Doppler QZSS L5 D / Beidou B2a Data for Rinex3.
D5I - org.orekit.gnss.PredefinedObservationType: Doppler GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.
D5P - org.orekit.gnss.PredefinedObservationType: Doppler QZSS L5 P / Beidou B2a Pilot for Rinex3.
D5Q - org.orekit.gnss.PredefinedObservationType: Doppler GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.
D5X - org.orekit.gnss.PredefinedObservationType: Doppler GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C / Beidou B2a Data+Pilot for Rinex3.
D5Z - org.orekit.gnss.PredefinedObservationType: Doppler QZSS L5 D+P for Rinex3.
D6 - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E6 / Beidou B03 for Rinex2.
D6A - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E6 A PRS / GLONASS L2CSI / Beidou B3A for Rinex3.
D6B - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E6 B C/NAV CS / GLONASS L2OCp for Rinex3.
D6C - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E6 C no data for Rinex3.
D6D - org.orekit.gnss.PredefinedObservationType: Doppler Beidou B3A for Rinex3.
D6E - org.orekit.gnss.PredefinedObservationType: Doppler QZSS L6E for Rinex3.
D6I - org.orekit.gnss.PredefinedObservationType: Doppler Beidou B3 I for Rinex3.
D6L - org.orekit.gnss.PredefinedObservationType: Doppler QZSS LEX(6) L for Rinex3.
D6P - org.orekit.gnss.PredefinedObservationType: Doppler Beidou B3A for Rinex3.
D6Q - org.orekit.gnss.PredefinedObservationType: Doppler Beidou B3 Q for Rinex3.
D6S - org.orekit.gnss.PredefinedObservationType: Doppler QZSS LEX(6) S for Rinex3.
D6X - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q / GLONASS G2a L2CSI+L2OCp for Rinex3.
D6Z - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E6 A+B+C / QZSS L6(D+E) / Beidou B3A for Rinex3.
D7 - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E5b / Beidou B02 for Rinex2.
D7D - org.orekit.gnss.PredefinedObservationType: Doppler Beidou B2b Data for Rinex3.
D7I - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.
D7P - org.orekit.gnss.PredefinedObservationType: Doppler Beidou B2b Pilot for Rinex3.
D7Q - org.orekit.gnss.PredefinedObservationType: Doppler Galileo Q no data / Beidou B2 Q for Rinex3.
D7X - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.
D7Z - org.orekit.gnss.PredefinedObservationType: Doppler Beidou B2b Data+Pilot for Rinex3.
D8 - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E5a+b for Rinex2.
D8D - org.orekit.gnss.PredefinedObservationType: Doppler Beidou B2(B2a+B2b) Data for Rinex3.
D8I - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E5(E5a+E5b) I for Rinex3.
D8P - org.orekit.gnss.PredefinedObservationType: Doppler Beidou B2(B2a+B2b) Pilot for Rinex3.
D8Q - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E5(E5a+E5b) Q for Rinex3.
D8X - org.orekit.gnss.PredefinedObservationType: Doppler Galileo E5(E5a+E5b) I+Q / B2(B2a+B2b) Data+Pilot for Rinex3.
D9A - org.orekit.gnss.PredefinedObservationType: Doppler IRNSS S A for Rinex3.
D9B - org.orekit.gnss.PredefinedObservationType: Doppler IRNSS S B for Rinex3.
D9C - org.orekit.gnss.PredefinedObservationType: Doppler IRNSS S C for Rinex3.
D9X - org.orekit.gnss.PredefinedObservationType: Doppler IRNSS S B+C for Rinex3.
DA - org.orekit.gnss.PredefinedObservationType: Doppler GPS L1 C/A / GLONASS G1 C/A for Rinex2.
data - org.orekit.files.ccsds.section.XmlStructureKey: XML data structure.
Data - Interface in org.orekit.files.ccsds.section: This marker interface represents segment data.
DATA - org.orekit.files.ccsds.section.KvnStructureKey: Data structure.
DATA_QUALITY - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: data quality entry.
DATA_ROOT_DIRECTORY_DOES_NOT_EXIST - org.orekit.errors.OrekitMessages: DATA_ROOT_DIRECTORY_DOES_NOT_EXIST.
DATA_SOURCE_TERM_LENGTH - Static variable in class org.orekit.files.iirv.terms.DataSourceTerm: The length of the IIRV term within the message.
DATA_SOURCE_TERM_PATTERN - Static variable in class org.orekit.files.iirv.terms.DataSourceTerm: Regular expression that ensures the validity of string values for this term.
DATA_TYPES - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey: Observation data types used.
DATA_TYPES - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Lit of data types in the data section.
dataContext(DataContext) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder: Sets the data context used by the propagator.
DataContext - Interface in org.orekit.data: Provides auxiliary data for portions of the application.
DataDictionary - Class in org.orekit.utils: String → Object mapping, for small number of keys.
DataDictionary() - Constructor for class org.orekit.utils.DataDictionary: Constructor with default initial capacity.
DataDictionary(int) - Constructor for class org.orekit.utils.DataDictionary: Constructor with specified capacity.
DataDictionary(DataDictionary) - Constructor for class org.orekit.utils.DataDictionary: Constructor from another dictionary.
DataDictionary.Entry - Class in org.orekit.utils: Entry in a dictionary.
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(File) - Constructor for class org.orekit.data.DataSource: Build an instance from a file on the local file system.
DataSource(String) - Constructor for class org.orekit.data.DataSource: Build an instance from file name only.
DataSource(String, DataSource.ReaderOpener) - Constructor for class org.orekit.data.DataSource: Complete constructor.
DataSource(String, DataSource.StreamOpener) - Constructor for class org.orekit.data.DataSource: Complete constructor.
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.
DataSourceTerm - Class in org.orekit.files.iirv.terms: Source of the data message.
DataSourceTerm(long) - Constructor for class org.orekit.files.iirv.terms.DataSourceTerm: Constructor.
DataSourceTerm(String) - Constructor for class org.orekit.files.iirv.terms.DataSourceTerm: Constructor.
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.
DATATION_ACCURACY - Static variable in interface org.orekit.propagation.events.EventDetectorsProvider: Accuracy of switching events dates (s).
DataType - Enum in org.orekit.gnss.metric.parser: Enum containing all low level data types that can be parsed to build a message.
DataUsed - Enum in org.orekit.files.sp3: Enumerate for data used.
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.models.earth.troposphere.TimeSpanEstimatedModel: 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.models.earth.troposphere.TimeSpanEstimatedModel: Prefix for dates before in the tropospheric parameter drivers' name.
DATE_FORMAT - Static variable in interface org.orekit.utils.Formatter: String format used for dates.
dateAtCount(double) - Method in class org.orekit.time.SatelliteClockScale: Compute date corresponding to some clock count.
DateBasedManeuverTriggers - Class in org.orekit.forces.maneuvers.trigger: Maneuver triggers based on a start and end date.
DateBasedManeuverTriggers(String, AbsoluteDate, double) - Constructor for class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers: Simple constructor.
DateBasedManeuverTriggers(String, AbsoluteDate, double, EventDetectionSettings) - Constructor for class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers: Simple constructor.
DateBasedManeuverTriggers(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) - Constructor for class org.orekit.time.DateComponents: Build a date from its offset with respect to a DateComponents.J2000_EPOCH.
DateComponents(int, int) - Constructor for class org.orekit.time.DateComponents: Build a date from a year and day number.
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(DateComponents, int) - Constructor for class org.orekit.time.DateComponents: Build a date from its offset with respect to a reference epoch.
DateDetectionAdaptableIntervalFactory - Class in org.orekit.propagation.events.intervals: Factory for adaptable interval tuned for date(s) detection.
DateDetector - Class in org.orekit.propagation.events: Finder for date events.
DateDetector(double, AbsoluteDate) - Constructor for class org.orekit.propagation.events.DateDetector: Build a new instance from a single time.
DateDetector(double, TimeStamped...) - Constructor for class org.orekit.propagation.events.DateDetector: Build a new instance.
DateDetector(EventDetectionSettings, EventHandler, double, TimeStamped...) - Constructor for class org.orekit.propagation.events.DateDetector: Protected constructor with full parameters.
DateDetector(AbsoluteDate) - Constructor for class org.orekit.propagation.events.DateDetector: Build a new instance from a single time.
DateDetector(TimeStamped...) - 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.
DATES_MISMATCH - org.orekit.errors.OrekitMessages: DATES_MISMATCH.
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(int, int, int) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from raw level components.
DateTimeComponents(int, int, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from raw level components.
DateTimeComponents(int, int, int, int, int, TimeOffset) - 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(int, Month, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from raw level components.
DateTimeComponents(int, Month, int, int, int, TimeOffset) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from raw level components.
DateTimeComponents(DateComponents, TimeComponents) - Constructor for class org.orekit.time.DateTimeComponents: Build a new instance from its components.
DateTimeComponents(DateTimeComponents, double) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from a seconds offset with respect to another one.
DateTimeComponents(DateTimeComponents, long, TimeUnit) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from a seconds offset with respect to another one.
DateTimeComponents(DateTimeComponents, TimeOffset) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from a seconds offset with respect to another one.
dateToCalendarString(TimeConverter, AbsoluteDate) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator: Convert a date to calendar string value with high precision.
dateToCalendarString(TimeConverter, AbsoluteDate) - Method in interface org.orekit.files.ccsds.utils.generation.Generator: Convert a date to calendar 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(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.
dateToString(TimeConverter, AbsoluteDate) - 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.
DAY - Static variable in class org.orekit.time.TimeOffset: Split time representing 1 day.
DAY - Static variable in class org.orekit.utils.units.Unit: Day unit.
DAY_OF_YEAR_LENGTH - Static variable in class org.orekit.files.iirv.terms.DayOfYearTerm: The length of the IIRV term within the message.
DAY_OF_YEAR_PATTERN - Static variable in class org.orekit.files.iirv.terms.DayOfYearTerm: Regular expression that ensures the validity of string values for this term.
DAY_WITH_POSITIVE_LEAP - Static variable in class org.orekit.time.TimeOffset: Split time representing 1 day that includes an additional leap second.
DayOfYearTerm - Class in org.orekit.files.iirv.terms: 3-character integer representing the day of the year.
DayOfYearTerm(long) - Constructor for class org.orekit.files.iirv.terms.DayOfYearTerm: Constructor.
DayOfYearTerm(String) - Constructor for class org.orekit.files.iirv.terms.DayOfYearTerm: Constructor.
DayOfYearTerm(AbsoluteDate, UTCScale) - Constructor for class org.orekit.files.iirv.terms.DayOfYearTerm: Constructs a DayOfYearTerm object from an AbsoluteDate object.
DAYS_SINCE_FIRST_OBS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey: Time elapsed between first accepted observation on epoch.
DAYS_SINCE_LAST_OBS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey: Time elapsed between last accepted observation on epoch.
DAYS_TO_SECONDS - Static variable in class org.orekit.utils.units.UnitsConverter: Days to seconds converter.
DB - org.orekit.gnss.PredefinedObservationType: Doppler GPS L1C for Rinex2.
DC - org.orekit.gnss.PredefinedObservationType: Doppler GPS L2C for Rinex2.
DC_BODY_FRAME - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Spacecraft body frame in which OrbitManeuverHistoryMetadataKey.DC_BODY_TRIGGER is specified.
DC_BODY_TRIGGER - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Direction in body frame for triggering duty cycle.
DC_EXEC_START - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Start time of initial duty cycle-based maneuver execution.
DC_EXEC_STOP - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: End time of final duty cycle-based maneuver execution.
DC_MAX_CYCLES - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Maximum number of "ON" duty cycles.
DC_MIN_CYCLES - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Minimum number of "ON" duty cycles.
DC_PA_START_ANGLE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Phase angle of pulse start.
DC_PA_STOP_ANGLE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Phase angle of pulse stop.
DC_REF_DIR - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Reference direction for triggering duty cycle.
DC_REF_TIME - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Duty cycle thrust reference time.
DC_TIME_PULSE_DURATION - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Duty cycle pulse "ON" duration.
DC_TIME_PULSE_PERIOD - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Duty cycle elapsed time between start of a pulse and start of next pulse.
DC_TYPE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Type of duty cycle.
DC_WIN_CLOSE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Start time of duty cycle-based maneuver window.
DC_WIN_OPEN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey: Start time of duty cycle-based maneuver window.
DCM - org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType: Direction cosine matrix.
DCP_SENSITIVITY_VECTOR_POSITION - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey: The Drag Consider Parameter (DCP) sensitivity vector (position errors at TCA).
DCP_SENSITIVITY_VECTOR_VELOCITY - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey: The Drag Consider Parameter (DCP) sensitivity vector (velocity errors at TCA).
DD - org.orekit.gnss.PredefinedObservationType: Doppler GLONASS G2 for Rinex2.
DEBRIS - org.orekit.files.ccsds.ndm.odm.ocm.ObjectType: Debris.
DECAYED - org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus: Decayed object.
DECEMBER - org.orekit.time.Month: December.
decode(EncodedMessage) - Method in enum org.orekit.gnss.metric.parser.DataType: Decode a piece of data extracted from an encoded message.
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.
decomposer(MatrixDecomposer) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder: Configure the matrix decomposer.
decomposer(MatrixDecomposer) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder: Configure the matrix decomposer.
decorate(ObservedMeasurement<?>, AbsoluteDate) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil: Decorate an observed measurement.
decorateUnscented(ObservedMeasurement<?>, AbsoluteDate) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil: Decorate an observed measurement for an Unscented Kalman Filter.
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 - org.orekit.files.ccsds.ndm.cdm.CovarianceMethod: Non-calculated default value was used.
DEFAULT - org.orekit.frames.encounter.EncounterLOFType: Default encounter local orbital frame based on Figure 1.3 from Romain Serra's thesis.
DEFAULT - Static variable in class org.orekit.files.iirv.terms.MessageSourceTerm: Default value for the message source is "0".
DEFAULT - Static variable in class org.orekit.files.iirv.terms.MessageTypeTerm: Default value: "03" (operations data message).
DEFAULT - Static variable in class org.orekit.files.iirv.terms.VehicleIdCodeTerm: Default VIC set to 1.
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_ABSOLUTE_MASS_TOLERANCE - Static variable in interface org.orekit.propagation.CartesianToleranceProvider: Default absolute tolerance for mass integration.
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_RATE_VALUE - Static variable in class org.orekit.files.sp3.SP3Utils: Bad or absent clock rate values are to be set to 999999.999999.
DEFAULT_CLOCK_VALUE - Static variable in class org.orekit.files.sp3.SP3Utils: 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_DAMPING - Static variable in class org.orekit.propagation.conversion.osc2mean.FixedPointConverter: Default damping ratio.
DEFAULT_DATE_EQUALITY_THRESHOLD - Static variable in class org.orekit.time.FieldTimeStampedPair: Default date equality threshold of 1 ns.
DEFAULT_DATE_EQUALITY_THRESHOLD - Static variable in class org.orekit.time.TimeStampedPair: Default date equality threshold of 1 ns.
DEFAULT_DC_TYPE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Default duty cycle type.
DEFAULT_DE_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader: Default supported files name pattern for JPL DE files.
DEFAULT_ELEVATION_SWITCH_INF - Static variable in class org.orekit.propagation.events.intervals.ElevationDetectionAdaptableIntervalFactory: Default elevation above which interval should be switched to fine interval (-5°).
DEFAULT_ELEVATION_SWITCH_SUP - Static variable in class org.orekit.propagation.events.intervals.ElevationDetectionAdaptableIntervalFactory: Default elevation below which interval should be switched to fine interval (+15°).
DEFAULT_EPSILON - Static variable in class org.orekit.propagation.conversion.averaging.converters.FixedPointOsculatingToAveragedConverter: Default convergence threshold.
DEFAULT_EXTRAPOLATION_THRESHOLD_SEC - Static variable in class org.orekit.time.AbstractFieldTimeInterpolator: Default extrapolation time threshold: 1ms.
DEFAULT_EXTRAPOLATION_THRESHOLD_SEC - Static variable in class org.orekit.time.AbstractTimeInterpolator: 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_DEGREE - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Default interpolation degree.
DEFAULT_INTERPOLATION_DEGREE - Static variable in class org.orekit.frames.EOPHistory: Default interpolation degree.
DEFAULT_INTERPOLATION_METHOD - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Default interpolation method.
DEFAULT_INTERPOLATION_METHOD - Static variable in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris: Default interpolation sample size if it is not specified.
DEFAULT_INTERPOLATION_POINTS - Static variable in class org.orekit.time.AbstractFieldTimeInterpolator: Default number of interpolation points.
DEFAULT_INTERPOLATION_POINTS - Static variable in class org.orekit.time.AbstractTimeInterpolator: Default number of interpolation points.
DEFAULT_INTERPOLATION_SAMPLE - Static variable in class org.orekit.files.iirv.IIRVParser: Default number of sample for interpolating data (See: reference documents).
DEFAULT_INTERPOLATION_SAMPLE - Static variable in class org.orekit.files.ilrs.CPFParser: Default number of sample for interpolating data (See: reference documents).
DEFAULT_INTERPOLATION_SAMPLES - Static variable in class org.orekit.files.sp3.SP3Parser: Default number of samples to use when interpolating SP3 coordinates.
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.CanonicalSaastamoinenModel: Default lowest acceptable elevation angle [rad].
DEFAULT_LOW_ELEVATION_THRESHOLD - Static variable in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel: 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_MASS - Static variable in class org.orekit.propagation.SpacecraftState: Default mass.
DEFAULT_MAX_CHECK - Static variable in class org.orekit.propagation.events.AbstractDetector: Default maximum checking interval (s).
DEFAULT_MAX_CHECK - Static variable in class org.orekit.propagation.events.DateDetector: Default value for max check.
DEFAULT_MAX_CHECK - Static variable in class org.orekit.propagation.events.EventDetectionSettings: Default maximum checking interval (s).
DEFAULT_MAX_CHECK - Static variable in class org.orekit.propagation.events.FieldAbstractDetector: Default maximum checking interval (s).
DEFAULT_MAX_CHECK - Static variable in class org.orekit.propagation.events.FieldDateDetector: Default value for max check.
DEFAULT_MAX_CHECK - Static variable in class org.orekit.propagation.events.FieldEventDetectionSettings: Default maximum checking interval (s).
DEFAULT_MAX_CHECK - Static variable in class org.orekit.propagation.events.intervals.DateDetectionAdaptableIntervalFactory: Default value for max check.
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.EventDetectionSettings: Default maximum number of iterations in the event time search.
DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.FieldAbstractDetector: Default maximum number of iterations in the event time search.
DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.FieldEventDetectionSettings: Default maximum number of iterations in the event time search.
DEFAULT_MAX_ITERATIONS - Static variable in class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm: Default value for maximum number of iterations.
DEFAULT_MAX_ITERATIONS - Static variable in class org.orekit.propagation.conversion.averaging.converters.FixedPointOsculatingToAveragedConverter: Default maximum number of iterations.
DEFAULT_MAX_ITERATIONS - Static variable in class org.orekit.propagation.conversion.osc2mean.FixedPointConverter: Default maximum number of iterations.
DEFAULT_MAX_ITERATIONS - Static variable in class org.orekit.propagation.conversion.osc2mean.LeastSquaresConverter: Default maximum number of iterations.
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_MIN_GAP - Static variable in class org.orekit.propagation.events.DateDetector: Default value for minimum gap between added dates.
DEFAULT_MIN_GAP - Static variable in class org.orekit.propagation.events.FieldDateDetector: Default value for minimum gap between added dates.
DEFAULT_NAME - Static variable in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers: Default name for trigger.
DEFAULT_ORBIT_TYPE - Static variable in class org.orekit.propagation.numerical.NumericalPropagator: Default orbit type.
DEFAULT_ORIGINATOR - Static variable in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter: Default value for HeaderKey.ORIGINATOR.
DEFAULT_ORIGINATOR - Static variable in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter: Default value for HeaderKey.ORIGINATOR.
DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.OceanTides: Default number of points tides field sampling.
DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.SolidTides: Default number of points tides field sampling.
DEFAULT_PORT - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient: Default port for ntrip communication.
DEFAULT_POSITION_ANGLE - Static variable in class org.orekit.propagation.AbstractStateCovarianceInterpolator: Default position angle for covariance expressed in Cartesian elements.
DEFAULT_POSITION_ANGLE_TYPE - Static variable in class org.orekit.propagation.numerical.NumericalPropagator: Default position angle type.
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_NAMES - Static variable in class org.orekit.files.rinex.observation.RinexObservationParser: Default name pattern for rinex 2 observation files.
DEFAULT_RINEX_3_NAMES - Static variable in class org.orekit.files.rinex.observation.RinexObservationParser: Default name pattern for rinex 3 observation files.
DEFAULT_SCALING_THRESHOLD - Static variable in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015: Default scaling threshold to use when sum becomes large.
DEFAULT_SCLK_OFFSET_AT_EPOCH - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Default value for SCLK_OFFSET_AT_EPOCH.
DEFAULT_SCLK_SEC_PER_SI_SEC - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Default value for SCLK_SEC_PER_SI_SEC.
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.time.AGILeapSecondFilesLoader: Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.time.TAIUTCDatFilesLoader: Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES_DTC - Static variable in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData: Default regular expression for supported names that works with test and published files for the DTCFILE file.
DEFAULT_SUPPORTED_NAMES_SOLFSMY - Static variable in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData: Default regular expression for supported names that works with test and published files for the SOLFSMY file.
DEFAULT_TCA_DIFFERENCE_TOLERANCE - Static variable in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod: Default time of closest approach difference tolerance.
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.conversion.osc2mean.FixedPointConverter: Default convergence threshold.
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.conversion.osc2mean.LeastSquaresConverter: Default convergence threshold.
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.DateDetector: Default value for convergence threshold.
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.EventDetectionSettings: Default convergence threshold (s).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.FieldAbstractDetector: Default convergence threshold (s).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.FieldDateDetector: Default value for convergence threshold.
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.FieldEventDetectionSettings: Default convergence threshold (s).
DEFAULT_TIMEOUT - Static variable in class org.orekit.gnss.metric.ntrip.NtripClient: Default timeout for connections and reads (ms).
DEFAULT_TOLERANCE_MASS_ADJOINT - Static variable in class org.orekit.control.indirect.shooting.AbstractIndirectShooting: Default value for convergence tolerance on mass adjoint variable.
DEFAULT_V00_PATTERN - Static variable in class org.orekit.files.sp3.NsgfV00Filter: Default regular expression for NSGF V00 files.
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.
DEFAULT_ZERO_THRESHOLD - Static variable in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Threshold below which values are considered equal to zero.
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: Empty constructor.
DefaultEncounterLOF - Class in org.orekit.frames.encounter: Default encounter local orbital frame.
DefaultEncounterLOF(FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.encounter.DefaultEncounterLOF: Field constructor.
DefaultEncounterLOF(PVCoordinates) - Constructor for class org.orekit.frames.encounter.DefaultEncounterLOF: Constructor.
defaultTypeBuilder(SatelliteSystem, String) - Static method in class org.orekit.files.sinex.SinexBiasParser: Default type builder.
DEG_PER_S - Static variable in class org.orekit.files.ccsds.definitions.Units: Degree per second unit.
DEG_PER_S_1_2 - Static variable in class org.orekit.files.ccsds.definitions.Units: Degree per second^1/2 unit.
DEG_PER_S_3_2 - Static variable in class org.orekit.files.ccsds.definitions.Units: Degree per second^3/2 unit.
DEGRADED - org.orekit.files.ccsds.ndm.tdm.DataQuality: Data exhibits quality issues.
DEGREE - Static variable in class org.orekit.utils.units.Unit: Degree unit.
DEGREES - org.orekit.data.PolynomialParser.Unit: Degrees angles.
DELAUNAY - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType: Delaunay elements (L, G, H, l, g, h).
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.
DELAUNAYMOD - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType: Modified Delaunay elements (Lm, Gm, Hm, lm, gm, hm).
DELTA - org.orekit.orbits.WalkerConstellation.Pattern: Delta pattern: ascending nodes distributed over 360°.
DELTA_MASS - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Mass change.
DELTA_R_FILE_NAME - Static variable in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel: Default file name for δR correction term table.
deltaRef(AbsoluteDate) - Method in class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature: Get duration since reference date.
deltaRef(AbsoluteDate) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2: Get duration since reference date.
deltaRef(AbsoluteDate) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2w: Get duration since reference date.
deltaRef(AbsoluteDate) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature3: Get duration since reference date.
deltaRef(FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature: Get duration since reference date.
deltaRef(FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2: Get duration since reference date.
deltaRef(FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2w: Get duration since reference date.
deltaRef(FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature3: Get duration since reference date.
DENSITY_FORECAST_UNCERTAINTY - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey: The atmospheric density forecast error.
dependsOnAttitudeRate() - Method in class org.orekit.forces.drag.DragForce: Check if force model depends on attitude's rotation rate or acceleration at a given, fixed date.
dependsOnAttitudeRate() - Method in interface org.orekit.forces.drag.DragSensitive: Check if model depends on attitude's rotation rate or acceleration at a given, fixed date.
dependsOnAttitudeRate() - Method in interface org.orekit.forces.ForceModel: Check if force model depends on attitude's rotation rate or acceleration at a given, fixed date.
dependsOnAttitudeRate() - Method in interface org.orekit.forces.ForceModelModifier: Check if force model depends on attitude's rotation rate or acceleration at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.drag.AbstractDragForceModel: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.empirical.AbstractParametricAcceleration: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in interface org.orekit.forces.ForceModel: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in interface org.orekit.forces.ForceModelModifier: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.AbstractBodyAttraction: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.DeSitterRelativity: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.J2OnlyPerturbation: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.LenseThirringRelativity: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.NewtonianAttraction: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.Relativity: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.inertia.InertialForces: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.maneuvers.Maneuver: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in interface org.orekit.forces.radiation.RadiationForceModel: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.RadiationPressureModel: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Check if force model depends on position only at a given, fixed date.
dependsOnPositionOnly() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel: Check if force model depends on position only at a given, fixed date.
DEPLOY_DIR_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: One σ angular off-nominal deployment vector direction.
DEPLOY_DV_CDA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.
DEPLOY_DV_RATIO - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Ratio of child-to-host ΔV vectors.
DEPLOY_DV_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: One σ percent error on deployment ΔV magnitude.
DEPLOY_DV_X - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Velocity increment of deployed "child" object along X axis.
DEPLOY_DV_Y - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Velocity increment of deployed "child" object along Y axis.
DEPLOY_DV_Z - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Velocity increment of deployed "child" object along Z axis.
DEPLOY_ID - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Identifier of resulting "child" object deployed from this host.
DEPLOY_MASS - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Decrement in host mass as a result of deployment (shall be ≤ 0).
derivative(double) - Method in class org.orekit.data.PolynomialNutation: Evaluate the time derivative of the polynomial.
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(T) - Method in class org.orekit.data.PolynomialNutation: Evaluate the time derivative of the polynomial.
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: Empty constructor.
DetectorModifier - Interface in org.orekit.propagation.events: Base class for modifying an existing detector.
DETERMINED_OD - org.orekit.files.ccsds.ndm.odm.ocm.ManBasis: Past maneuver reconstructed from orbit determination.
DETERMINED_TLM - org.orekit.files.ccsds.ndm.odm.ocm.ManBasis: Past maneuver reconstructed from telemetry.
DF002 - org.orekit.gnss.metric.parser.RtcmDataField: RTCM Message number.
DF009 - org.orekit.gnss.metric.parser.RtcmDataField: GPS Satellite ID.
DF038 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS Satellite ID.
DF040 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS Satellite Frequency Channel Number.
DF068 - org.orekit.gnss.metric.parser.RtcmDataField: GNSS satellite ID.
DF071 - org.orekit.gnss.metric.parser.RtcmDataField: GPS IODE (Issue Of Data, Ephemeris).
DF076 - org.orekit.gnss.metric.parser.RtcmDataField: GPS Week number.
DF077 - org.orekit.gnss.metric.parser.RtcmDataField: GPS SV Accuracy.
DF078 - org.orekit.gnss.metric.parser.RtcmDataField: GPS CODE ON L2.
DF079 - org.orekit.gnss.metric.parser.RtcmDataField: GPS Rate of Inclination Angle.
DF081 - org.orekit.gnss.metric.parser.RtcmDataField: GPS toc.
DF082 - org.orekit.gnss.metric.parser.RtcmDataField: GPS a_f2.
DF083 - org.orekit.gnss.metric.parser.RtcmDataField: GPS a_f1.
DF084 - org.orekit.gnss.metric.parser.RtcmDataField: GPS a_f0.
DF085 - org.orekit.gnss.metric.parser.RtcmDataField: GPS IODC (Issue Of Data, Clock).
DF086 - org.orekit.gnss.metric.parser.RtcmDataField: GPS C_rs.
DF087 - org.orekit.gnss.metric.parser.RtcmDataField: GPS Δn (DELTA n).
DF088 - org.orekit.gnss.metric.parser.RtcmDataField: GPS M₀.
DF089 - org.orekit.gnss.metric.parser.RtcmDataField: GPS C_uc.
DF090 - org.orekit.gnss.metric.parser.RtcmDataField: GPS Eccentricity (e).
DF091 - org.orekit.gnss.metric.parser.RtcmDataField: GPS C_us.
DF092 - org.orekit.gnss.metric.parser.RtcmDataField: GPS A^1/2.
DF093 - org.orekit.gnss.metric.parser.RtcmDataField: GPS t_oe.
DF094 - org.orekit.gnss.metric.parser.RtcmDataField: GPS C_ic.
DF095 - org.orekit.gnss.metric.parser.RtcmDataField: GPS Ω₀ (OMEGA)₀.
DF096 - org.orekit.gnss.metric.parser.RtcmDataField: GPS C_is.
DF097 - org.orekit.gnss.metric.parser.RtcmDataField: GPS i₀.
DF098 - org.orekit.gnss.metric.parser.RtcmDataField: GPS C_rc.
DF099 - org.orekit.gnss.metric.parser.RtcmDataField: GPS ω (Argument of Perigee).
DF100 - org.orekit.gnss.metric.parser.RtcmDataField: GPS OMEGADOT (Rate of Right Ascension).
DF101 - org.orekit.gnss.metric.parser.RtcmDataField: GPS t_GD.
DF102 - org.orekit.gnss.metric.parser.RtcmDataField: GPS SV HEALTH.
DF103 - org.orekit.gnss.metric.parser.RtcmDataField: GPS L2 P data flag.
DF104 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS almanac health (C_n word).
DF105 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS almanac health availability indicator.
DF106 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS P1.
DF107 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS t_k (s).
DF108 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS MSB of B_n word.
DF109 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS P2 Flag.
DF110 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS t_b.
DF111 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS x_n (t_b), first derivative.
DF112 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS x_n (t_b).
DF113 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS x_n (t_b), second derivative.
DF114 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS y_n (t_b), first derivative.
DF115 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS y_n (t_b).
DF116 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS y_n (t_b), second derivative.
DF117 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS z_n (t_b), first derivative.
DF118 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS z_n (t_b).
DF119 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS z_n (t_b), second derivative.
DF120 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS P3 Flag.
DF121 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS γ_n (t_b).
DF122 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M P.
DF123 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M l_n (third string).
DF124 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS τ_n (t_b).
DF125 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS Δτ_n.
DF126 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS E_n.
DF127 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M P4.
DF128 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M F_T.
DF129 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M N_T.
DF130 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M M.
DF131 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS The Availability of Additional Data.
DF132 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS N^A.
DF133 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS τ_c.
DF134 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M N₄.
DF135 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS τ_GPS.
DF136 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS-M l_n (fifth string).
DF137 - org.orekit.gnss.metric.parser.RtcmDataField: GPS Fit Interval.
DF252 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo Satellite ID.
DF289 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo Week Number (WN).
DF290 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo IODnav.
DF291 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo SV SISA.
DF292 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo IDOT.
DF293 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo t_oc.
DF294 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo a_f2.
DF295 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo a_f1.
DF296 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo a_f0.
DF297 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo C_rs.
DF298 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo Δn.
DF299 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo M₀.
DF300 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo C_uc.
DF301 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo e.
DF302 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo C_us.
DF303 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo A^1/2.
DF304 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo t_oe.
DF305 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo C_ic.
DF306 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo Ω₀.
DF307 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo C_is.
DF308 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo i₀.
DF309 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo C_rc.
DF310 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo ω.
DF311 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo OMEGADOT (Rate of Right Ascension).
DF312 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo BGD (E1/E5a).
DF313 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo BGD (E5b/E1).
DF314 - org.orekit.gnss.metric.parser.RtcmDataField: E5a SIGNAL Health Status.
DF315 - org.orekit.gnss.metric.parser.RtcmDataField: E5a Data Validity Status.
DF316 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo SOL NAV Signal Health Status (SOLHS).
DF317 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo SOL NAV Data Validity Status (SOLDVS).
DF365 - org.orekit.gnss.metric.parser.RtcmDataField: Delta Orbit Radial (m).
DF366 - org.orekit.gnss.metric.parser.RtcmDataField: Delta Along-Track (m).
DF367 - org.orekit.gnss.metric.parser.RtcmDataField: Delta Cross-Track (m).
DF368 - org.orekit.gnss.metric.parser.RtcmDataField: Dot Delta Radial (m/s).
DF369 - org.orekit.gnss.metric.parser.RtcmDataField: Dot Delta Along-Track (m/s).
DF370 - org.orekit.gnss.metric.parser.RtcmDataField: Dot Delta Cross-Track (m/s).
DF375 - org.orekit.gnss.metric.parser.RtcmDataField: Satellite Reference Datum.
DF376 - org.orekit.gnss.metric.parser.RtcmDataField: Delta Clock C0.
DF377 - org.orekit.gnss.metric.parser.RtcmDataField: Delta Clock C1.
DF378 - org.orekit.gnss.metric.parser.RtcmDataField: Delta Clock C2.
DF384 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS Satellite ID.
DF385 - org.orekit.gnss.metric.parser.RtcmDataField: GPS Epoch Time 1s.
DF386 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS Epoch Time 1s.
DF387 - org.orekit.gnss.metric.parser.RtcmDataField: No. of Satellites.
DF388 - org.orekit.gnss.metric.parser.RtcmDataField: Multiple Message Indicator.
DF391 - org.orekit.gnss.metric.parser.RtcmDataField: SSR Update Interval.
DF392 - org.orekit.gnss.metric.parser.RtcmDataField: GLONASS Issue Of Date (IOD).
DF413 - org.orekit.gnss.metric.parser.RtcmDataField: IOD SSR.
DF414 - org.orekit.gnss.metric.parser.RtcmDataField: SSR Provider ID.
DF415 - org.orekit.gnss.metric.parser.RtcmDataField: SSR Solution ID.
DF429 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS Satellite ID.
DF430 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS t_oc.
DF431 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS a_f2.
DF432 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS a_f1.
DF433 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS a_f0.
DF434 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS IODE.
DF435 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS C_rs.
DF436 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS Δn.
DF437 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS M₀.
DF438 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS C_uc.
DF439 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS e.
DF440 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS C_us.
DF441 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS A^1/2.
DF442 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS t_oe.
DF443 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS C_ic.
DF444 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS Ω₀.
DF445 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS C_is.
DF446 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS i₀.
DF447 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS C_rc.
DF448 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS ω.
DF449 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS OMEGADOT (Rate of Right Ascension).
DF450 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS iDOT.
DF451 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS Codes on L2 Channel.
DF452 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS Week Number.
DF453 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS URA Number.
DF454 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS SV health.
DF455 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS t_GD.
DF456 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS IODC.
DF457 - org.orekit.gnss.metric.parser.RtcmDataField: QZSS Fit Interval.
DF458 - org.orekit.gnss.metric.parser.RtcmDataField: Galileo Epoch Time 1s.
DF488 - org.orekit.gnss.metric.parser.RtcmDataField: BDS Satellite ID.
DF489 - org.orekit.gnss.metric.parser.RtcmDataField: BDS Week Number.
DF490 - org.orekit.gnss.metric.parser.RtcmDataField: BDS SV URA Index.
DF491 - org.orekit.gnss.metric.parser.RtcmDataField: BDS IDOT.
DF492 - org.orekit.gnss.metric.parser.RtcmDataField: BDS AODE.
DF493 - org.orekit.gnss.metric.parser.RtcmDataField: BDS t_oc.
DF494 - org.orekit.gnss.metric.parser.RtcmDataField: BDS a_f2.
DF495 - org.orekit.gnss.metric.parser.RtcmDataField: BDS a_f1.
DF496 - org.orekit.gnss.metric.parser.RtcmDataField: BDS a_f0.
DF497 - org.orekit.gnss.metric.parser.RtcmDataField: BDS AODC.
DF498 - org.orekit.gnss.metric.parser.RtcmDataField: BDS C_rs.
DF499 - org.orekit.gnss.metric.parser.RtcmDataField: BDS Δn.
DF500 - org.orekit.gnss.metric.parser.RtcmDataField: BDS M₀.
DF501 - org.orekit.gnss.metric.parser.RtcmDataField: BDS C_uc.
DF502 - org.orekit.gnss.metric.parser.RtcmDataField: BDS e.
DF503 - org.orekit.gnss.metric.parser.RtcmDataField: BDS C_us.
DF504 - org.orekit.gnss.metric.parser.RtcmDataField: BDS a^1/2.
DF505 - org.orekit.gnss.metric.parser.RtcmDataField: BDS t_oe.
DF506 - org.orekit.gnss.metric.parser.RtcmDataField: BDS C_ic.
DF507 - org.orekit.gnss.metric.parser.RtcmDataField: BDS Ω₀.
DF508 - org.orekit.gnss.metric.parser.RtcmDataField: BDS C_is.
DF509 - org.orekit.gnss.metric.parser.RtcmDataField: BDS i₀.
DF510 - org.orekit.gnss.metric.parser.RtcmDataField: BDS C_rc.
DF511 - org.orekit.gnss.metric.parser.RtcmDataField: BDS ω.
DF512 - org.orekit.gnss.metric.parser.RtcmDataField: BDS OMEGADOT (Rate of Right Ascension).
DF513 - org.orekit.gnss.metric.parser.RtcmDataField: BDS t_GD1.
DF514 - org.orekit.gnss.metric.parser.RtcmDataField: BDS t_GD2.
DF515 - org.orekit.gnss.metric.parser.RtcmDataField: BDS SV Health.
DIFFERENT_STATE_DEFINITION - org.orekit.errors.OrekitMessages: DIFFERENT_STATE_DEFINITION.
DIFFERENT_TIME_OF_CLOSEST_APPROACH - org.orekit.errors.OrekitMessages: DIFFERENT_TIME_OF_CLOSEST_APPROACH.
DifferentialSignalBias - Class in org.orekit.files.sinex: Container for differential signal bias for a single link endpoint (either emitter or receiver).
DifferentialSignalBias() - Constructor for class org.orekit.files.sinex.DifferentialSignalBias: Simple constructor.
differentiate(ParameterFunction, int, double) - Static method in class org.orekit.utils.Differentiation: Differentiate a scalar function using finite differences.
differentiate(StateFunction, int, AttitudeProvider, OrbitType, PositionAngleType, 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.
DIGEST - org.orekit.gnss.metric.ntrip.Authentication: Digest.
DIMENSION_INCONSISTENT_WITH_PARAMETERS - org.orekit.errors.OrekitMessages: DIMENSION_INCONSISTENT_WITH_PARAMETERS.
Dipole - Class in org.orekit.estimation.measurements.gnss: Dipole configuration for satellite-to-ground and inter-satellites wind-up effects.
Dipole(Vector3D, Vector3D) - Constructor for class org.orekit.estimation.measurements.gnss.Dipole: Simple constructor.
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.
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 class org.orekit.models.earth.displacement.PostSeismicDeformation: 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.TectonicsDisplacement: 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.
displacement(AbsoluteDate, GeodeticPoint) - Method in class org.orekit.models.earth.displacement.PsdCorrection: Compute displacement.
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(int) - Method in class org.orekit.time.TimeOffset: Divide the instance by a positive constant.
divide(String, Unit) - Method in class org.orekit.utils.units.Unit: Create quotient of units.
DOCKED_WITH - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Other space objects this object is docked to.
doesCount(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldCountAndContinue: Method returning true if and only if the count needs to be incremented.
doesCount(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldCountingHandler: Method returning true if and only if the count needs to be incremented.
doesCount(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.CountAndContinue: Method returning true if and only if the count needs to be incremented.
doesCount(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.CountingHandler: Method returning true if and only if the count needs to be incremented.
doEvent(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventState: Notify the user's listener of the event.
doEvent(SpacecraftState) - Method in class org.orekit.propagation.events.EventState: Notify the user's listener of the event.
DOI - org.orekit.files.rinex.section.RinexLabels: DOI.
doModify(EstimationModifier<T>, EstimatedMeasurementBase<T>) - 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.
DOPPLER - org.orekit.gnss.MeasurementType: Doppler measurement.
DOPPLER_COUNT - org.orekit.files.ccsds.ndm.tdm.ObservationType: Data: Doppler counts [n/a].
DOPPLER_COUNT_BIAS - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Bias that was added to Doppler count in the data section.
DOPPLER_COUNT_ROLLOVER - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Indicator for occurred rollover in Doppler count.
DOPPLER_COUNT_SCALE - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Scaled by which Doppler count was multiplied in the data section.
DOPPLER_INSTANTANEOUS - org.orekit.files.ccsds.ndm.tdm.ObservationType: Data: Doppler instantaneous [km/s].
DOPPLER_INTEGRATED - org.orekit.files.ccsds.ndm.tdm.ObservationType: Data: Doppler integrated [km/s].
DOR - org.orekit.files.ccsds.ndm.tdm.ObservationType: Data: DOR [s].
DormandPrince54FieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion: Builder for DormandPrince54FieldIntegrator.
DormandPrince54FieldIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince54FieldIntegratorBuilder: Build a new instance using default integration tolerances.
DormandPrince54FieldIntegratorBuilder(double, double, ToleranceProvider) - Constructor for class org.orekit.propagation.conversion.DormandPrince54FieldIntegratorBuilder: Build a new instance.
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 using default integration tolerances.
DormandPrince54IntegratorBuilder(double, double, ToleranceProvider) - Constructor for class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder: Build a new instance.
DormandPrince853FieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion: Builder for DormandPrince853FieldIntegrator.
DormandPrince853FieldIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince853FieldIntegratorBuilder: Build a new instance using default integration tolerances.
DormandPrince853FieldIntegratorBuilder(double, double, ToleranceProvider) - Constructor for class org.orekit.propagation.conversion.DormandPrince853FieldIntegratorBuilder: 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 using default integration tolerances.
DormandPrince853IntegratorBuilder(double, double, ToleranceProvider) - 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(Map<String, double[]>) - Constructor for class org.orekit.utils.DoubleArrayDictionary: Constructor from a map.
DoubleArrayDictionary(DoubleArrayDictionary) - Constructor for class org.orekit.utils.DoubleArrayDictionary: Constructor from another dictionary.
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. rectangular shape).
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. rectangular shape).
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.
DoubleValuedIIRVTerm - Class in org.orekit.files.iirv.terms.base: Term in an IIRV Vector representing a double value.
DoubleValuedIIRVTerm(String, double, int, int, boolean) - Constructor for class org.orekit.files.iirv.terms.base.DoubleValuedIIRVTerm: Constructs an IIRV Vector Term represented by a double.
DoubleValuedIIRVTerm(String, String, int, int, boolean) - Constructor for class org.orekit.files.iirv.terms.base.DoubleValuedIIRVTerm: Constructs an IIRV Vector Term represented by a double from a given String.
DR - org.orekit.files.rinex.clock.RinexClock.ClockDataType: Discontinuity measurements for a single GPS receiver.
DRAG_AREA - org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey: Drag area.
DRAG_COEFF - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey: Drag coefficient.
DRAG_COEFF - org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey: Drag coefficient.
DRAG_COEFF_NOM - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Nominal drag coefficient.
DRAG_COEFFICIENT - Static variable in interface org.orekit.forces.drag.DragSensitive: Parameter name for drag coefficient.
DRAG_COEFFICIENT_TERM_LENGTH - Static variable in class org.orekit.files.iirv.terms.DragCoefficientTerm: The length of the IIRV term within the message.
DRAG_COEFFICIENT_TERM_PATTERN - Static variable in class org.orekit.files.iirv.terms.DragCoefficientTerm: Regular expression that ensures the validity of string values for this term.
DRAG_CONST_AREA - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
DRAG_UNCERTAINTY - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Drag coefficient 1σ uncertainty.
dragAcceleration(FieldSpacecraftState<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Compute the acceleration due to drag.
dragAcceleration(FieldSpacecraftState<T>, T, FieldVector3D<T>, T[]) - Method in interface org.orekit.forces.drag.DragSensitive: Compute the acceleration due to drag.
dragAcceleration(FieldSpacecraftState<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.drag.IsotropicDrag: Compute the acceleration due to drag.
dragAcceleration(SpacecraftState, double, Vector3D, double[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Compute the acceleration due to drag.
dragAcceleration(SpacecraftState, double, Vector3D, double[]) - Method in interface org.orekit.forces.drag.DragSensitive: Compute the acceleration due to drag.
dragAcceleration(SpacecraftState, double, Vector3D, double[]) - Method in class org.orekit.forces.drag.IsotropicDrag: Compute the acceleration due to drag.
DragCoefficientTerm - Class in org.orekit.files.iirv.terms: 4-character dimensionless drag coefficient.
DragCoefficientTerm(double) - Constructor for class org.orekit.files.iirv.terms.DragCoefficientTerm: Constructor.
DragCoefficientTerm(String) - Constructor for class org.orekit.files.iirv.terms.DragCoefficientTerm: Constructor.
DragForce - Class in org.orekit.forces.drag: Atmospheric drag force model.
DragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.DragForce: Constructor with default flag for finite differences.
DragForce(Atmosphere, DragSensitive, boolean) - 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_RATE_SHIFT_DEG_PER_DAY - Static variable in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements: Longitude drift rate.
DRIFT_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation: Suffix for ground clock drift parameters name.
DRY_MASS - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey: Mass without propellant.
DRY_MASS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Mass without propellant.
DSS - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment: Digital Sun Sensor.
DSST_ECC_NO_NUMERICAL_AVERAGING_METHOD - org.orekit.errors.OrekitMessages: DSST_ECC_NO_NUMERICAL_AVERAGING_METHOD.
DSST_NEWCOMB_OPERATORS_COMPUTATION - org.orekit.errors.OrekitMessages: DSST_NEWCOMB_OPERATORS_COMPUTATION.
DSST_SPR_SHADOW_INCONSISTENT - org.orekit.errors.OrekitMessages: DSST_SPR_SHADOW_INCONSISTENT.
DSST_THEORY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata: Constant for DSST mean elements theory.
DSST_VMNS_COEFFICIENT_ERROR_MS - org.orekit.errors.OrekitMessages: DSST_VMNS_COEFFICIENT_ERROR_MS.
DSST6X0OrbitalState - Class in org.orekit.propagation.conversion.averaging: Class representing an averaged orbital state as in the DSST theory using only the first 6 zonal harmonics as perturbations.
DSST6X0OrbitalState(AbsoluteDate, AveragedEquinoctialWithMeanAngle, Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.averaging.DSST6X0OrbitalState: Constructor.
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(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver, 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.
DSSTGravityContext - Class in org.orekit.propagation.semianalytical.dsst.forces: This class is a container for the common parameters used in DSSTTesseral and DSSTZonal.
DSSTHarvester - Class in org.orekit.propagation.semianalytical.dsst: Harvester between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
DSSTJ2SquaredClosedForm - Class in org.orekit.propagation.semianalytical.dsst.forces: Second order J2-squared force model.
DSSTJ2SquaredClosedForm(J2SquaredModel, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm: Constructor.
DSSTJ2SquaredClosedFormContext - Class in org.orekit.propagation.semianalytical.dsst.forces: This class is a container for the common parameters used in DSSTJ2SquaredClosedForm.
DSSTJ2SquaredClosedFormContext(AuxiliaryElements, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext: Simple 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.
DSSTPropagator - Class in org.orekit.propagation.semianalytical.dsst: This class propagates orbits using the DSST theory.
DSSTPropagator(ODEIntegrator) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Create a new instance of DSSTPropagator.
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.
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, double, double, ExtendedPositionProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Constructor with customizable reference values but spherical spacecraft.
DSSTSolarRadiationPressure(double, double, ExtendedPositionProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Simple constructor with default reference values and spherical spacecraft.
DSSTSolarRadiationPressure(double, double, ExtendedPositionProvider, OneAxisEllipsoid, RadiationSensitive, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Complete constructor.
DSSTSolarRadiationPressure(ExtendedPositionProvider, OneAxisEllipsoid, RadiationSensitive, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Simple constructor with default reference values, but custom spacecraft.
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.
DSSTTheory - Class in org.orekit.propagation.conversion.osc2mean: DSST theory for osculating to mean orbit conversion.
DSSTTheory(Collection<DSSTForceModel>) - Constructor for class org.orekit.propagation.conversion.osc2mean.DSSTTheory: Constructor with default values.
DSSTTheory(Collection<DSSTForceModel>, AttitudeProvider, double) - Constructor for class org.orekit.propagation.conversion.osc2mean.DSSTTheory: Full constructor.
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.
DSSTThirdBodyDynamicContext - Class in org.orekit.propagation.semianalytical.dsst.forces: This class is a container for the common parameters used in DSSTThirdBody.
DSSTThirdBodyDynamicContext(AuxiliaryElements, CelestialBody, double[]) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext: Constructor.
DSSTThirdBodyStaticContext - Class in org.orekit.propagation.semianalytical.dsst.forces: This class is a container for the common parameters used in DSSTThirdBody.
DSSTThirdBodyStaticContext(AuxiliaryElements, double, double, double[]) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyStaticContext: Constructor.
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 bodyFixedFrame = orbit frame, and default reference values.
DSSTZonal(UnnormalizedSphericalHarmonicsProvider, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Constructor with bodyFixedFrame = orbit frame.
DSSTZonal(Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Constructor with default reference values.
DSSTZonal(Frame, UnnormalizedSphericalHarmonicsProvider, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Constructor.
DSSTZonalContext - Class in org.orekit.propagation.semianalytical.dsst.forces: This class is a container for the common parameters used in DSSTZonal.
DT - org.orekit.models.earth.weather.SeasonalModelType: Temperature gradient model.
DtcDataLoader - Class in org.orekit.models.earth.atmosphere.data: This class reads solar activity data from DTCFILE files for the class JB2008SpaceEnvironmentData.
DtcDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.DtcDataLoader: Constructor.
DtcDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data: Container class for Solar activity indexes.
DTM2000 - Class in org.orekit.models.earth.atmosphere: This atmosphere model is the realization of the DTM-2000 model.
DTM2000(DTM2000InputParameters, ExtendedPositionProvider, BodyShape) - Constructor for class org.orekit.models.earth.atmosphere.DTM2000: Simple constructor for independent computation.
DTM2000(DTM2000InputParameters, ExtendedPositionProvider, 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.
DUAL_CONE - org.orekit.files.ccsds.ndm.odm.ocm.ShadowModel: Cone model, penumbra and umbra.
DualFrequencyHatchFilter - Class in org.orekit.estimation.measurements.filtering: Hatch Filter using Carrier-Phase measurements taken at two different frequencies, to form a Divergence-Free phase combination.
DualFrequencyHatchFilter(ObservationData, ObservationData, ObservationData, double, double, double, int) - Constructor for class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter: Constructor for the Dual Frequency Hatch Filter.
DualFrequencySmoother - Class in org.orekit.estimation.measurements.filtering: Handler to perform pseudo-range smoothing using Divergence-Free phase combinations.
DualFrequencySmoother(double, int) - Constructor for class org.orekit.estimation.measurements.filtering.DualFrequencySmoother: Simple constructor.
DUMMY - Static variable in class org.orekit.files.sp3.SP3Coordinate: Dummy coordinate with all fields set to 0.0.
DummyMappingFunction - Class in org.orekit.models.earth.troposphere: Dummy mapping function.
DummyMappingFunction() - Constructor for class org.orekit.models.earth.troposphere.DummyMappingFunction: Builds a new instance.
DUPLICATED_GRAVITY_FIELD_COEFFICIENT_IN_FILE - org.orekit.errors.OrekitMessages: DUPLICATED_GRAVITY_FIELD_COEFFICIENT_IN_FILE.
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(AbsoluteDate) - Method in class org.orekit.time.FieldAbsoluteDate: Compute the physically elapsed duration between two instants.
durationFrom(AbsoluteDate, TimeUnit) - Method in class org.orekit.time.AbsoluteDate: Compute the physically elapsed duration between two instants.
durationFrom(AbsoluteDate, TimeUnit) - Method in class org.orekit.time.FieldAbsoluteDate: 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(FieldAbsoluteDate<T>, TimeUnit) - Method in class org.orekit.time.FieldAbsoluteDate: Compute the physically elapsed duration between two instants.
durationFrom(FieldTimeStamped<T>) - Method in interface org.orekit.time.FieldTimeStamped: Compute the physically elapsed duration between two instants.
durationFrom(TimeStamped) - Method in interface org.orekit.time.TimeStamped: 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.
DV_BOL - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Total ΔV capability at beginning of life.
DV_DIR_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: One σ angular off-nominal ΔV direction.
DV_MAG_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: One σ percent error on ΔV magnitude.
DV_REMAINING - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey: Total ΔV remaining for spacecraft.
DV_X - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Velocity increment along X axis.
DV_Y - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Velocity increment along Y axis.
DV_Z - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType: Velocity increment along Z axis.
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.
E - org.orekit.gnss.SignalCode: QZSS L6E and L6 (D+E) codes.
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.
E01 - org.orekit.gnss.PredefinedGnssSignal: Galileo, "E1" (1575.42 MHz).
E05 - org.orekit.gnss.PredefinedGnssSignal: Galileo E5a (1176.45 MHz).
E06 - org.orekit.gnss.PredefinedGnssSignal: Galileo E6 (1278.75 MHz).
E07 - org.orekit.gnss.PredefinedGnssSignal: Galileo E5b (1207.14 MHz).
E08 - org.orekit.gnss.PredefinedGnssSignal: Galileo E5 (E5a + E5b) (1191.795MHz).
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.
EARTH - org.orekit.attitudes.PredefinedTarget: Earth direction (assumes the frame is Earth centered).
EARTH - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType: Constant for the Earth.
EARTH - org.orekit.files.ccsds.definitions.CenterName: Earth body.
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 - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType: Constant for the Earth-Moon barycenter.
EARTH_MOON - org.orekit.files.ccsds.definitions.CenterName: Earth-Moon barycenter bodies pair.
EARTH_MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Earth-Moon barycenter.
EARTH_RADII - Static variable in class org.orekit.utils.units.Unit: Earth Radii used as Bstar unit in CCSDS OMM.
EARTH_RADIUS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants: Earth radius in km.
EARTH_TIDES - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey: Is solid Earth and ocean tides used for the OD of the object ?
EarthOrientationParameterMessage - Class in org.orekit.files.rinex.navigation: Container for data contained in a Earth Orientation Parameter navigation message.
EarthOrientationParameterMessage(SatelliteSystem, int, String) - Constructor for class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage: Simple constructor.
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.
EAST - org.orekit.attitudes.PredefinedTarget: East direction.
EAST - org.orekit.models.earth.displacement.PsdCorrection.Axis: East axis.
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.
ECCENTRIC - org.orekit.orbits.PositionAngleType: Eccentric angle.
ECCENTRICITY - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey: Orbit eccentricity.
ECCENTRICITY - Static variable in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Name for eccentricity parameter.
eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.CircularLatitudeArgumentUtility: Computes the mean latitude argument from the eccentric latitude argument.
eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.EquinoctialLongitudeArgumentUtility: Computes the mean longitude argument from the eccentric longitude argument.
eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldCircularLatitudeArgumentUtility: Computes the mean latitude argument from the eccentric latitude argument.
eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialLongitudeArgumentUtility: Computes the mean longitude argument from the eccentric longitude argument.
eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.CircularLatitudeArgumentUtility: Computes the true latitude argument from the eccentric latitude argument.
eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.EquinoctialLongitudeArgumentUtility: Computes the true longitude argument from the eccentric longitude argument.
eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldCircularLatitudeArgumentUtility: Computes the true latitude argument from the eccentric latitude argument.
eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialLongitudeArgumentUtility: Computes the true longitude argument from the eccentric longitude argument.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.FieldGnssPropagatorBuilder: Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
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.FieldGnssPropagatorBuilder: Sets the Earth Centered Inertial frame used for propagation.
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.
EcksteinHechlerOrbitalState - Class in org.orekit.propagation.conversion.averaging: Class representing an averaged orbital state as in the Eckstein-Hechler theory.
EcksteinHechlerOrbitalState(AbsoluteDate, AveragedCircularWithMeanAngle, Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.averaging.EcksteinHechlerOrbitalState: Constructor.
EcksteinHechlerPropagator - Class in org.orekit.propagation.analytical: This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.
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, 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, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, mass 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, 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, AttitudeProvider, double, double, double, double, double, double, double, double, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double, PropagationType, double, int) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double, PropagationType, OsculatingToMeanConverter) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, attitude provider, mass 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, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Private helper constructor.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Private helper constructor.
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, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, attitude provider and potential provider.
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit and potential provider.
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit and potential provider.
EcksteinHechlerPropagatorBuilder - Class in org.orekit.propagation.conversion: Builder for Eckstein-Hechler propagator.
EcksteinHechlerPropagatorBuilder(Orbit, double, double, TideSystem, double, double, double, double, double, OrbitType, PositionAngleType, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder: Build a new instance.
EcksteinHechlerPropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngleType, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder: Build a new instance.
EcksteinHechlerPropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngleType, double, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder: Build a new instance.
EcksteinHechlerTheory - Class in org.orekit.propagation.conversion.osc2mean: Eckstein-Hechler theory for osculating to mean orbit conversion.
EcksteinHechlerTheory(double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.osc2mean.EcksteinHechlerTheory: Constructor.
EcksteinHechlerTheory(UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.osc2mean.EcksteinHechlerTheory: Constructor.
EclipseDetector - Class in org.orekit.propagation.events: Finder for satellite eclipse related events.
EclipseDetector(EventDetectionSettings, EventHandler, OccultationEngine, double, boolean) - Constructor for class org.orekit.propagation.events.EclipseDetector: Protected constructor with full parameters.
EclipseDetector(ExtendedPositionProvider, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.EclipseDetector: Build a new eclipse detector.
EclipseDetector(OccultationEngine) - Constructor for class org.orekit.propagation.events.EclipseDetector: Build a new eclipse detector.
ECLIPTIC_CONVENTIONS_1996 - org.orekit.frames.Predefined: Ecliptic framen IERS 1996 conventions.
ECLIPTIC_CONVENTIONS_2003 - org.orekit.frames.Predefined: Ecliptic framen IERS 2003 conventions.
ECLIPTIC_CONVENTIONS_2010 - org.orekit.frames.Predefined: Ecliptic framen IERS 2010 conventions.
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.
ECOM_COEFFICIENT - Static variable in class org.orekit.forces.radiation.ECOM2: Parameter name for ECOM model coefficients enabling Jacobian processing.
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, ExtendedPositionProvider, double) - Constructor for class org.orekit.forces.radiation.ECOM2: Constructor.
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.
EGM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for EGM files.
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.
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.
EGNOS - org.orekit.files.rinex.navigation.SbasId: European Geostationary Navigation Overlay Service.
EGO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory: Extended Geostationary Orbit, 37948 < a < 46380 km, e < 0.25, i < 25°.
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.
EIGVAL3EIGVEC3 - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType: 12 elements eigenvalue/eigenvectors (EigMaj, EigMed, EigMin, EigVecMaj, EigVecMed, EigVecMin).
EKF - org.orekit.files.ccsds.definitions.AdMethodType: Extended Kalman Filter.
EKF - org.orekit.files.ccsds.definitions.OdMethodType: Extended Kalman Filter.
electronDensity(DateTimeComponents, double, double, double, double) - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickModel: Computes the electron density at a given height.
electronDensity(DateTimeComponents, T, T, T, T) - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickModel: Computes the electron density at a given height.
ELEMENT_SET_NO - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey: Element set number for this satellite.
ElevationDetectionAdaptableIntervalFactory - Class in org.orekit.propagation.events.intervals: Factory class for AdaptableInterval suitable for elevation detection on eccentric orbits.
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(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.
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(EventDetectionSettings, EventHandler, double, ElevationMask, AtmosphericRefractionModel, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector: Protected constructor with full parameters.
ElevationDetector(AdaptableInterval, 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(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector: Build a detector.
ElevationExtremumDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector: Build a new detector.
ElevationExtremumDetector(EventDetectionSettings, EventHandler, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector: Protected constructor with full parameters.
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.
ELLIPSOID - org.orekit.files.ccsds.ndm.cdm.ScreenVolumeShape: Ellipsoid.
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(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility: Computes the elliptic mean anomaly from the elliptic eccentric anomaly.
ellipticEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility: Computes the elliptic mean anomaly from the elliptic eccentric anomaly.
ellipticEccentricToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility: Computes the elliptic true anomaly from the elliptic eccentric anomaly.
ellipticEccentricToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility: Computes the elliptic true anomaly from the elliptic eccentric anomaly.
ellipticMeanToEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility: Computes the elliptic eccentric anomaly from the elliptic mean anomaly.
ellipticMeanToEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility: Computes the elliptic eccentric anomaly from the elliptic mean anomaly.
ellipticMeanToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility: Computes the elliptic true anomaly from the elliptic mean anomaly.
ellipticMeanToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility: Computes the elliptic true anomaly from the elliptic mean anomaly.
ellipticTrueToEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility: Computes the elliptic eccentric anomaly from the elliptic true anomaly.
ellipticTrueToEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility: Computes the elliptic eccentric anomaly from the elliptic true anomaly.
ellipticTrueToMean(double, double) - Static method in class org.orekit.orbits.KeplerianAnomalyUtility: Computes the elliptic mean anomaly from the elliptic true anomaly.
ellipticTrueToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianAnomalyUtility: Computes the elliptic mean anomaly from the elliptic true anomaly.
EME2000 - org.orekit.files.ccsds.definitions.CelestialBodyFrame: Earth Mean Equator and Equinox of J2000.
EME2000 - org.orekit.frames.Predefined: EME2000 frame.
emitterToInert(EstimatedMeasurementBase<InterSatellitesPhase>) - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesWindUp: Compute rotation from emitter to inertial frame.
emitterToInert(EstimatedMeasurementBase<Phase>) - Method in class org.orekit.estimation.measurements.gnss.WindUp: Compute rotation from emitter to inertial frame.
emitterToInert(EstimatedMeasurementBase<T>) - Method in class org.orekit.estimation.measurements.gnss.AbstractWindUp: Compute rotation from emitter to inertial frame.
EMPTY - org.orekit.gnss.metric.ntrip.NavigationSystem: No navigation system for this stream.
emptyCache() - Static method in class org.orekit.utils.ImmutableFieldTimeStampedCache: Get an empty immutable cache.
emptyCache() - Static method in class org.orekit.utils.ImmutableTimeStampedCache: Get an empty immutable cache, cast to the correct type.
EnablingPredicate - 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.
EncounterLOF - Interface in org.orekit.frames.encounter: Interface for encounter local orbital frame.
EncounterLOFType - Enum in org.orekit.frames.encounter: Enum for encounter local orbital frame.
END - org.orekit.files.ccsds.ndm.tdm.IntegrationReference: Time tag at integration interval end.
END - org.orekit.files.rinex.section.RinexLabels: End of header.
END_OF_ENCODED_MESSAGE - org.orekit.errors.OrekitMessages: END_OF_ENCODED_MESSAGE.
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.
ensureCompatible(String, List<Unit>, boolean, List<Unit>) - Static method in class org.orekit.utils.units.Unit: Ensure some units are compatible with reference units.
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.
enterSection(Generator) - Method in class org.orekit.files.ccsds.section.AbstractWriter: Enter the section.
ENTRY - org.orekit.files.ccsds.utils.lexical.TokenType: Entry content token.
EOP_SOURCE - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey: Source and version of Earth Orientation Parameters.
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, double, double, ITRFVersion, AbsoluteDate) - Constructor for class org.orekit.frames.EOPEntry: Simple constructor.
EOPFittedModel - Class in org.orekit.frames: Container for fitted model for Earth Orientation Parameters.
EOPFittedModel(SecularAndHarmonic, SecularAndHarmonic, SecularAndHarmonic, SecularAndHarmonic, SecularAndHarmonic) - Constructor for class org.orekit.frames.EOPFittedModel: Simple constructor.
EOPFitter - Class in org.orekit.frames: Earth Orientation Parameters fitter for EOP prediction.
EOPFitter(SingleParameterFitter, SingleParameterFitter, SingleParameterFitter, SingleParameterFitter, SingleParameterFitter) - Constructor for class org.orekit.frames.EOPFitter: 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, int, Collection<? extends EOPEntry>, boolean) - Constructor for class org.orekit.frames.EOPHistory: Simple constructor.
EOPHistory(IERSConventions, int, 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: Legacy constructor with tabulated states and default Hermite interpolation.
Ephemeris(List<SpacecraftState>, TimeInterpolator<SpacecraftState>) - Constructor for class org.orekit.propagation.analytical.Ephemeris: Constructor with tabulated states.
Ephemeris(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>) - Constructor for class org.orekit.propagation.analytical.Ephemeris: Constructor with tabulated states and associated covariances.
Ephemeris(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.Ephemeris: Constructor with tabulated states and associated covariances.
Ephemeris(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.Ephemeris: Constructor with tabulated states.
EPHEMERIS_NAME - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey: Unique name of the external ephemeris file used for the object or NONE.
EPHEMERIS_NAME_1 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: External ephemeris file for the participant 1.
EPHEMERIS_NAME_2 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: External ephemeris file for the participant 2.
EPHEMERIS_NAME_3 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: External ephemeris file for the participant 3.
EPHEMERIS_NAME_4 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: External ephemeris file for the participant 4.
EPHEMERIS_NAME_5 - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: External ephemeris file for the participant 5.
EPHEMERIS_TYPE - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey: Ephemeris Type, only required if MEAN_ELEMENT_THEORY = SGP/SGP4.
EPHEMERIS_TYPE_PPT3 - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Constant for EPHEMERIS_TYPE PPT3.
EPHEMERIS_TYPE_SGP - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Constant for EPHEMERIS_TYPE SGP.
EPHEMERIS_TYPE_SGP4 - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Constant for EPHEMERIS_TYPE SGP4.
EPHEMERIS_TYPE_SGP4_XP - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Constant for EPHEMERIS_TYPE SGP4-XP.
EPHEMERIS_TYPE_SPECIAL_PERTURBATIONS - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Constant for EPHEMERIS_TYPE Special Perturbations.
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.
EphemerisOcmWriter - Class in org.orekit.files.ccsds.ndm.odm.ocm: An EphemerisFileWriter generating OCM files.
EphemerisOcmWriter(OcmWriter, OdmHeader, OcmMetadata, TrajectoryStateHistoryMetadata, FileFormat, String, double, int) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.EphemerisOcmWriter: Constructor used to create a new OCM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
EphemerisOcmWriter(OcmWriter, OdmHeader, OcmMetadata, TrajectoryStateHistoryMetadata, FileFormat, String, double, int, Formatter) - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.EphemerisOcmWriter: Constructor used to create a new OCM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
EphemerisOemWriter - Class in org.orekit.files.ccsds.ndm.odm.oem: An EphemerisFileWriter generating OEM files.
EphemerisOemWriter(OemWriter, OdmHeader, OemMetadata, FileFormat, String, double, int) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.EphemerisOemWriter: 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.
EphemerisOemWriter(OemWriter, OdmHeader, OemMetadata, FileFormat, String, double, int, Formatter) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.EphemerisOemWriter: 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.
EphemerisPropagatorBuilder - Class in org.orekit.propagation.conversion: Builder for Ephemeris propagator.
EphemerisPropagatorBuilder(List<SpacecraftState>, int, double, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.EphemerisPropagatorBuilder: Constructor.
EphemerisPropagatorBuilder(List<SpacecraftState>, TimeInterpolator<SpacecraftState>) - Constructor for class org.orekit.propagation.conversion.EphemerisPropagatorBuilder: Constructor using the default attitude provider.
EphemerisPropagatorBuilder(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>) - Constructor for class org.orekit.propagation.conversion.EphemerisPropagatorBuilder: Constructor with covariances and default attitude provider.
EphemerisPropagatorBuilder(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.EphemerisPropagatorBuilder: Constructor.
EphemerisPropagatorBuilder(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.EphemerisPropagatorBuilder: Constructor.
EphemerisSegmentPropagator<C extends TimeStampedPVCoordinates> - Class in org.orekit.files.general: A Propagator based on a EphemerisFile.EphemerisSegment.
EphemerisSegmentPropagator(EphemerisFile.EphemerisSegment<C>, AttitudeProvider) - Constructor for class org.orekit.files.general.EphemerisSegmentPropagator: Create a Propagator from an ephemeris segment.
EPOCH - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Entry epoch.
EPOCH - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey: Epoch entry (only for ADM V1).
EPOCH - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey: Epoch entry (only for OEM files).
EPOCH - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey: Epoch of Keplerian elements.
EPOCH - org.orekit.files.ccsds.ndm.odm.StateVectorKey: Epoch of state vector and optional Keplerian elements.
EPOCH - org.orekit.files.ccsds.ndm.tdm.TdmDataKey: Epoch entry.
EPOCH_TZERO - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey: Default epoch to which all relative times are referenced in data blocks, unless overridden by block-specific AcmMetadataKey.EPOCH_TZERO values.
EPOCH_TZERO - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey: Default epoch to which all relative times are referenced in data blocks, unless overridden by block-specific OcmMetadataKey.EPOCH_TZERO values.
EpochDerivativesEquations - Class in org.orekit.propagation.numerical: Computes derivatives of the acceleration, including ThirdBodyAttraction.
EpochDerivativesEquations(String, NumericalPropagator) - Constructor for class org.orekit.propagation.numerical.EpochDerivativesEquations: Simple constructor.
EPSILON_DEFAULT - Static variable in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Default convergence threshold for mean parameters conversion.
EPSILON_DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm: Default value for epsilon.
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.estimation.measurements.ObservableSatellite
equals(Object) - Method in class org.orekit.files.iirv.IIRVMessage
equals(Object) - Method in class org.orekit.files.iirv.IIRVVector: Compares two IIRV vectors for equality based on their string representations, include message metadata information.
equals(Object) - Method in class org.orekit.files.iirv.terms.base.IIRVVectorTerm
equals(Object) - Method in class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration
equals(Object) - Method in class org.orekit.files.sinex.AntennaKey
equals(Object) - Method in class org.orekit.gnss.SatInSystem
equals(Object) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader.LineParameters: Check if the instance represents the same parameters as given line parameters.
equals(Object) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Check if the instance represents the same parameters as given line parameters.
equals(Object) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters: Check if the instance represents the same parameters as given line parameters.
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.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.time.TimeOffset
equals(Object) - Method in class org.orekit.utils.units.Unit: Check if the instance represents the same unit as another instance.
EQUATORIAL_RADIUS - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Oblate spheroid equatorial radius of central body.
EQUINOCTIAL - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType: Equinoctial elements (a, af, ag, L=M+ω+frΩ, χ, ψ, fr).
EQUINOCTIAL - org.orekit.orbits.OrbitType: Type for orbital representation in EquinoctialOrbit and FieldEquinoctialOrbit parameters.
EquinoctialLongitudeArgumentUtility - Class in org.orekit.orbits: Utility methods for converting between different longitude arguments used by EquinoctialOrbit.
EQUINOCTIALMOD - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType: Modified equinoctial elements (p=a(1−e²), af, ag, L'=υ+ω+frΩ, χ, ψ, fr).
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, double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Creates a new instance with derivatives and with cached position angle same as value inputted.
EquinoctialOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Creates a new instance.
EquinoctialOrbit(double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Creates a new instance without derivatives and with cached position angle same as value inputted.
EquinoctialOrbit(double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Creates a new instance.
EquinoctialOrbit(Orbit) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Constructor from any kind of orbital parameters.
EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Constructor from Cartesian parameters.
EquinoctialOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Constructor from Cartesian parameters.
EQW - org.orekit.frames.LOFType: Constant for Equinoctial Coordinate System (X axis aligned with ascending node, Z axis aligned with orbital momentum).
EQW_INERTIAL - org.orekit.files.ccsds.definitions.OrbitRelativeFrame: Equinoctial coordinate system (X towards ascending node, Z towards momentum).
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: Empty constructor.
ESA - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment: Earth Sensor Assembly.
ESO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory: Escape Orbit.
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, with derivatives.
estimate(int, int, SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Estimate the theoretical value of the measurement, with derivatives.
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, boolean, int, Position, Position) - Method in class org.orekit.estimation.iod.IodLambert: Estimate an initial orbit from two position measurements.
estimate(Frame, boolean, int, PV, PV) - Method in class org.orekit.estimation.iod.IodLambert: Estimate an initial orbit from two PV measurements.
estimate(Frame, Vector3D, Vector3D, Vector3D, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, double, double) - Method in class org.orekit.estimation.iod.IodGooding: Estimate orbit from three line of sight.
estimate(Frame, Vector3D, Vector3D, Vector3D, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, double, double, int, boolean) - Method in class org.orekit.estimation.iod.IodGooding: Estimate orbit from three line of sight.
estimate(Frame, Vector3D, AbsoluteDate, Vector3D, Vector3D, AbsoluteDate, Vector3D, Vector3D, AbsoluteDate, Vector3D) - Method in class org.orekit.estimation.iod.IodGauss: Estimate and orbit based on Gauss Intial Orbit Determination method.
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, AngularAzEl, AngularAzEl, AngularAzEl) - Method in class org.orekit.estimation.iod.IodGauss: Estimate and orbit based on Gauss Intial Orbit Determination method.
estimate(Frame, AngularAzEl, AngularAzEl, AngularAzEl) - Method in class org.orekit.estimation.iod.IodGooding: Estimate orbit from three angular (i.e., azimuth - elevation) observations.
estimate(Frame, AngularAzEl, AngularAzEl, AngularAzEl) - Method in class org.orekit.estimation.iod.IodLaplace: Estimate the orbit from three angular observations at the same location.
estimate(Frame, AngularAzEl, AngularAzEl, AngularAzEl, double, double) - Method in class org.orekit.estimation.iod.IodGooding: Estimate orbit from three angular observations.
estimate(Frame, AngularAzEl, AngularAzEl, AngularAzEl, double, double, int, boolean) - Method in class org.orekit.estimation.iod.IodGooding: Estimate orbit from three angular observations.
estimate(Frame, AngularAzEl, AngularAzEl, AngularAzEl, int, boolean) - Method in class org.orekit.estimation.iod.IodGooding: Estimate orbit from three angular (i.e., azimuth - elevation) observations.
estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec) - Method in class org.orekit.estimation.iod.IodGauss: Estimate and orbit based on Gauss Intial Orbit Determination method.
estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec) - Method in class org.orekit.estimation.iod.IodGooding: Estimate orbit from three angular (i.e., right ascension - declination) observations.
estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec) - Method in class org.orekit.estimation.iod.IodLaplace: Estimate the orbit from three angular observations at the same location.
estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec, double, double) - Method in class org.orekit.estimation.iod.IodGooding: Estimate orbit from three angular observations.
estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec, double, double, int, boolean) - Method in class org.orekit.estimation.iod.IodGooding: Estimate orbit from three angular observations.
estimate(Frame, AngularRaDec, AngularRaDec, AngularRaDec, int, boolean) - Method in class org.orekit.estimation.iod.IodGooding: Estimate orbit from three angular (i.e., right ascension - declination) observations.
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, PVCoordinates, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D) - Method in class org.orekit.estimation.iod.IodLaplace: Estimate orbit from three line of sight angles at the same location.
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(EstimatedMeasurementBase<T>) - Constructor for class org.orekit.estimation.measurements.EstimatedMeasurement: Constructor from measurement base.
EstimatedMeasurement(T, int, int, SpacecraftState[], TimeStampedPVCoordinates[]) - Constructor for class org.orekit.estimation.measurements.EstimatedMeasurement: Simple constructor.
EstimatedMeasurementBase<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements: Class holding an estimated theoretical value associated to an observed measurement.
EstimatedMeasurementBase(T, int, int, SpacecraftState[], TimeStampedPVCoordinates[]) - Constructor for class org.orekit.estimation.measurements.EstimatedMeasurementBase: Simple constructor.
EstimatedMeasurementBase.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.
estimatedMeasurementsParameters(ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder: Configure the estimated measurement parameters.
estimatedMeasurementsParameters(ParameterDriversList, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder: Configure the estimated measurement parameters.
EstimatedModel - Class in org.orekit.models.earth.troposphere: An estimated tropospheric model.
EstimatedModel(double, double, double, TroposphereMappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedModel: Build a new instance using the given environmental conditions.
EstimatedModel(TroposphereMappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedModel: Build a new instance using a standard atmosphere model.
EstimatedModel(TroposphericModel, TroposphereMappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedModel: Build a new instance using the given environmental conditions.
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.
estimateRate(Rotation, Rotation, double) - Static method in class org.orekit.utils.AngularCoordinates: 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.
estimateWithoutDerivatives(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Estimate the theoretical value of the measurement, without derivatives.
estimateWithoutDerivatives(int, int, SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Estimate the theoretical value of the measurement, without derivatives.
estimateWithoutDerivatives(SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Estimate the theoretical value of the measurement, without derivatives.
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.
estimationStep(ObservedMeasurement<?>) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimator: Process a single measurement.
estimationTypeChanged(boolean, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver: Notify that a parameter estimation type (continuous or step) has been changed.
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.
ETR - Static variable in class org.orekit.files.iirv.terms.OriginIdentificationTerm: NASA/USFC Eastern Test Range (ETR) OriginIdentification.
ETR - Static variable in class org.orekit.files.iirv.terms.RoutingIndicatorTerm: NASA/USFC Eastern Test Range (ETR) RoutingIndicator.
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.
EULER_ANGLE - org.orekit.files.ccsds.ndm.adm.AttitudeType: Euler angles.
EULER_ANGLE_ANGVEL - org.orekit.files.ccsds.ndm.adm.AttitudeType: Euler angles and angular velocity.
EULER_ANGLE_DERIVATIVE - org.orekit.files.ccsds.ndm.adm.AttitudeType: Euler angles and rotation rate.
EULER_ANGLES - org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType: Euler angles.
EULER_DIR - org.orekit.files.ccsds.ndm.adm.apm.EulerKey: Rotation direction entry (ADM V1 only).
EULER_FRAME_A - org.orekit.files.ccsds.ndm.adm.apm.EulerKey: First reference frame entry (only for ADM V1).
EULER_FRAME_B - org.orekit.files.ccsds.ndm.adm.apm.EulerKey: Second reference frame entry (only for ADM V1).
EULER_RATE - org.orekit.files.ccsds.ndm.adm.acm.RateElementsType: Euler rates.
EULER_ROT_SEQ - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey: Rotation sequence entry.
EULER_ROT_SEQ - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey: Rotation sequence entry.
EULER_ROT_SEQ - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey: Rotation order entry for Euler angles.
EULER_ROT_SEQ - org.orekit.files.ccsds.ndm.adm.apm.EulerKey: Rotation sequence entry.
eulerAngle - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Euler angle sub-section.
eulerAngleAngVel - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Euler angle/angular velocity sub-section.
eulerAngleDerivative - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Euler angle/derivative sub-section.
eulerAngleRate - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey: Euler angle/rate sub-section (only for ADM V1).
EulerFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion: Builder for EulerFieldIntegrator.
EulerFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.EulerFieldIntegratorBuilder: Constructor.
EulerFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.EulerFieldIntegratorBuilder: Constructor using a "fielded" step.
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.
evaluate(FieldVector3D<T>) - Method in enum org.orekit.forces.maneuvers.Control3DVectorCostType: Evaluate the cost of the input seen as a 3D control vector.
evaluate(Vector3D) - Method in enum org.orekit.forces.maneuvers.Control3DVectorCostType: Evaluate the cost of the input seen as a 3D control vector.
evaluate(GroundStation, FieldSpacecraftState<Gradient>, Gradient[]) - Method in interface org.orekit.estimation.measurements.modifiers.ParametricModelEffectGradient: Evaluate the parametric model effect.
evaluate(GroundStation, SpacecraftState) - Method in interface org.orekit.estimation.measurements.modifiers.ParametricModelEffect: Evaluate the parametric model effect.
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).
evaluateFieldPenaltyFunction(T) - Method in class org.orekit.control.indirect.adjoint.cost.FieldLogarithmicBarrierCartesianFuel: Evaluate the penalty term (without the weight), assumed to be a function of the control norm.
evaluateFieldPenaltyFunction(T) - Method in class org.orekit.control.indirect.adjoint.cost.FieldPenalizedCartesianFuelCost: Evaluate the penalty term (without the weight), assumed to be a function of the control norm.
evaluateFieldPenaltyFunction(T) - Method in class org.orekit.control.indirect.adjoint.cost.FieldQuadraticPenaltyCartesianFuel: Evaluate the penalty term (without the weight), assumed to be a function of the control norm.
evaluateHamiltonian(FieldSpacecraftState<T>) - Method in class org.orekit.control.indirect.adjoint.FieldCartesianAdjointDerivativesProvider: Evaluate the Hamiltonian from Pontryagin's Maximum Principle.
evaluateHamiltonian(SpacecraftState) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointDerivativesProvider: Evaluate the Hamiltonian from Pontryagin's Maximum Principle.
evaluatePenaltyFunction(double) - Method in class org.orekit.control.indirect.adjoint.cost.LogarithmicBarrierCartesianFuel: Evaluate the penalty term (without the weight), assumed to be a function of the control norm.
evaluatePenaltyFunction(double) - Method in class org.orekit.control.indirect.adjoint.cost.PenalizedCartesianFuelCost: Evaluate the penalty term (without the weight), assumed to be a function of the control norm.
evaluatePenaltyFunction(double) - Method in class org.orekit.control.indirect.adjoint.cost.QuadraticPenaltyCartesianFuel: Evaluate the penalty term (without the weight), assumed to be a function of the control norm.
evaluateStep(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState: Evaluate the impact of the proposed step on the event detector.
evaluateStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState: 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.
evaluationPerformed(KalmanEstimation) - Method in class org.orekit.estimation.sequential.RtsSmoother
EVENT_DATE_TOO_CLOSE - org.orekit.errors.OrekitMessages: EVENT_DATE_TOO_CLOSE.
EventBasedScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation: Scheduler based on EventDetector for generating measurements sequences.
EventBasedScheduler(MeasurementBuilder<T>, DatesSelector, Predicate<EstimatedMeasurementBase<T>>, Propagator, EventDetector, SignSemantic) - Constructor for class org.orekit.estimation.measurements.generation.EventBasedScheduler: Simple constructor.
EventBasedScheduler(MeasurementBuilder<T>, DatesSelector, Propagator, EventDetector, SignSemantic) - Constructor for class org.orekit.estimation.measurements.generation.EventBasedScheduler: Simple constructor.
EventDetectionSettings - Class in org.orekit.propagation.events: Class containing parameters for event detection.
EventDetectionSettings(double, double, int) - Constructor for class org.orekit.propagation.events.EventDetectionSettings: Constructor with maximum check as double.
EventDetectionSettings(AdaptableInterval, double, int) - Constructor for class org.orekit.propagation.events.EventDetectionSettings: Constructor.
EventDetector - Interface in org.orekit.propagation.events: This interface represents space-dynamics aware events detectors.
EventDetectorsProvider - Interface in org.orekit.propagation.events: Interface for building event detectors for force models and maneuver parameters.
EventEnablingPredicateFilter - Class in org.orekit.propagation.events: Wrapper used to detect events only when enabled by an external predicated function.
EventEnablingPredicateFilter(EventDetectionSettings, EventDetector, EnablingPredicate) - Constructor for class org.orekit.propagation.events.EventEnablingPredicateFilter: Constructor with full parameters.
EventEnablingPredicateFilter(EventDetector, EnablingPredicate) - Constructor for class org.orekit.propagation.events.EventEnablingPredicateFilter: Wrap an event detector.
EventHandler - Interface in org.orekit.propagation.events.handlers: An interface defining how to handle events occurring during propagation.
eventIsEnabled(FieldSpacecraftState<T>, FieldEventDetector<T>, T) - Method in interface org.orekit.propagation.events.FieldEnablingPredicate: Compute an event enabling function of state.
eventIsEnabled(SpacecraftState, EventDetector, double) - Method in interface org.orekit.propagation.events.EnablingPredicate: Compute an event enabling function of state.
EventMultipleHandler - 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(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldContinueOnEvent: Specific implementation of the eventOccurred interface.
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldCountingHandler: Handle an event.
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler: Handle an event.
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldRecallLastOccurrence: Handle an event.
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldResetDerivativesOnEvent: Specific implementation of the eventOccurred interface.
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnDecreasing: Handle a detection event and choose what to do next.
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnEvent: Specific implementation of the eventOccurred interface.
eventOccurred(FieldSpacecraftState<T>, FieldEventDetector<T>, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnIncreasing: Handle a detection event and choose what to do next.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.attitudes.AttitudesSequence.Switch: Handle an event.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.attitudes.AttitudesSwitcher.InstantaneousSwitch: Handle an event.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.ContinueOnEvent: Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.CountingHandler: Handle an event.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in interface org.orekit.propagation.events.handlers.EventHandler: Handle an event.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler: Handle an event.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.RecallLastOccurrence: Handle an event.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.ResetDerivativesOnEvent: Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnDecreasing: Handle a detection event and choose what to do next.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnEvent: Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnIncreasing: Handle a detection event and choose what to do next.
EventShifter - Class in org.orekit.propagation.events: Wrapper shifting events occurrences times.
EventShifter(EventDetectionSettings, EventDetector, boolean, double, double) - Constructor for class org.orekit.propagation.events.EventShifter: Protected constructor with full parameters.
EventShifter(EventDetector, 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(EventDetectionSettings, T, FilterType) - Constructor for class org.orekit.propagation.events.EventSlopeFilter: Constructor with full parameters.
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.
EXCEPTIONAL_DATA_CONTEXT - org.orekit.errors.OrekitMessages: EXCEPTIONAL_DATA_CONTEXT.
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: Empty constructor.
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.
exitSection(Generator) - Method in class org.orekit.files.ccsds.section.AbstractWriter: Exit the section.
EXP - org.orekit.models.earth.displacement.PsdCorrection.TimeEvolution: Exponential evolution.
ExplicitRungeKuttaIntegratorBuilder - Interface in org.orekit.propagation.conversion: This interface is for builders of explicit Runge-Kutta integrators (adaptive or not).
expressCovarianceInDesiredOutput(Orbit, StateCovariance) - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator: Express covariance in output configuration defined at this instance construction.
EXT - org.orekit.files.sp3.SP3OrbitType: extrapolated or predicted.
extend(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.
extend(FieldVector3D<Gradient>, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter: Add zero derivatives.
extend(FieldAbsoluteDate<Gradient>, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter: Add zero derivatives.
EXTENDED_MISSION - org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus: Object in extended mission.
ExtendedPositionProvider - Interface in org.orekit.utils: Interface for position providers (including for Field).
ExtendedPositionProviderAdapter - Class in org.orekit.utils: Adapter from ExtendedPositionProvider to TransformProvider.
ExtendedPositionProviderAdapter(Frame, ExtendedPositionProvider, String) - Constructor for class org.orekit.utils.ExtendedPositionProviderAdapter: Simple constructor.
ExtendedPVCoordinatesProvider - Interface in org.orekit.utils: Deprecated.
since 13.0. Use ExtendedPositionProvider instead.
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.AbstractEncodedMessage: 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.
extractClockModel() - Method in class org.orekit.files.sp3.SP3Ephemeris: Extract the clock model.
extractClockModel() - Method in class org.orekit.files.sp3.SP3Segment: Extract the clock model.
extractClockModel(int) - Method in class org.orekit.files.rinex.observation.RinexObservation: Extract the receiver clock model.
extractClockModel(String, int) - Method in class org.orekit.files.rinex.clock.RinexClock: Extract the clock model.
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(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(double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel: Extract the proper parameter drivers' values from the array in input of the pathDelay method.
extractParameters(double[], AbsoluteDate) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Extract the proper parameter drivers' values from the array in input of the updateShortPeriodTerms 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(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(T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel: Extract the proper parameter drivers' values from the array in input of the pathDelay method.
extractParameters(T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Extract the proper parameter drivers' values from the array in input of the updateShortPeriodTerms method.
extractRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap: Extract a range of the map.
ExtremumApproachDetector - Class in org.orekit.propagation.events: Finder for extremum approach events.
ExtremumApproachDetector(EventDetectionSettings, EventHandler, PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.ExtremumApproachDetector: Constructor.
ExtremumApproachDetector(PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.ExtremumApproachDetector: Constructor with default values.

F

F0 - Static variable in interface org.orekit.gnss.GnssSignal: Common frequency F0 in Hz (10.23 MHz).
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.
FAILED_AUTHENTICATION - org.orekit.errors.OrekitMessages: FAILED_AUTHENTICATION.
FDOA - Class in org.orekit.estimation.measurements: Class modeling a Frequency Difference of Arrival measurement with a satellite as emitter and two ground stations as receivers.
FDOA(GroundStation, GroundStation, double, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.FDOA: Simple constructor.
FDOABuilder - Class in org.orekit.estimation.measurements.generation: Builder for FDOA measurements.
FDOABuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.FDOABuilder: Simple constructor.
FEASIBLE_MEASUREMENT_WHEN_NEGATIVE - org.orekit.estimation.measurements.generation.SignSemantic: Semantic for detectors that have negative g function when measurements are feasible.
FEASIBLE_MEASUREMENT_WHEN_POSITIVE - org.orekit.estimation.measurements.generation.SignSemantic: Semantic for detectors that have positive g function when measurements are feasible.
FEBRUARY - org.orekit.time.Month: February.
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.AbstractListCrawler: Feed a data file loader by browsing the data collection.
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(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.
feed(DataLoader) - Method in class org.orekit.data.AbstractSelfFeedingLoader: Feed the given loader with AbstractSelfFeedingLoader.getDataProvidersManager() and AbstractSelfFeedingLoader.getSupportedNames().
FEMTOSECOND - Static variable in class org.orekit.time.TimeOffset: Split time representing 1 femtosecond.
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.AbstractEncodedMessage: Fetch the next byte from the message.
fetchByte() - Method in class org.orekit.gnss.metric.parser.ByteArrayEncodedMessage: Fetch the next byte from the message.
fetchByte() - Method in class org.orekit.gnss.metric.parser.HexadecimalSequenceEncodedMessage: Fetch the next byte from the message.
fetchByte() - Method in class org.orekit.gnss.metric.parser.InputStreamEncodedMessage: 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.
FIELD_TOO_LONG - org.orekit.errors.OrekitMessages: FIELD_TOO_LONG.
FieldAbsoluteDate<T extends CalculusFieldElement<T>> - Class in org.orekit.time: This class represents a specific instant in time.
FieldAbsoluteDate(Field<T>) - Constructor for class org.orekit.time.FieldAbsoluteDate: Create an instance with a default value (FieldAbsoluteDate.getJ2000Epoch(Field)).
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, int, int, int, int, TimeOffset, 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, 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, TimeOffset, 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>, 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>, Instant) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an instant in utc time scale.
FieldAbsoluteDate(Field<T>, Instant, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an instant in a time scale.
FieldAbsoluteDate(Field<T>, Instant, UTCScale) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an instant in the 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(Field<T>, AbsoluteDate) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an AbsoluteDate.
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>, DateComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from a location 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(AbsoluteDate, long, TimeUnit, Field<T>) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an elapsed duration since another instant.
FieldAbsoluteDate(AbsoluteDate, T) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an elapsed duration since another instant.
FieldAbsoluteDate(FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an elapsed duration since 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.
FieldAbsoluteDate(FieldAbsoluteDate<T>, long, TimeUnit) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an elapsed duration since another instant.
FieldAbsoluteDate(FieldAbsoluteDate<T>, TimeOffset) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an elapsed duration since another instant.
FieldAbsoluteDate(FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an elapsed duration since another instant.
FieldAbsolutePVCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils: Field implementation of AbsolutePVCoordinates.
FieldAbsolutePVCoordinates(Field<T>, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates: Build from Field and non-Fielded object.
FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates: Build from position and velocity.
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) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates: Builds a FieldAbsolutePVCoordinates triplet from a FieldVector3D<DerivativeStructure>.
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>, FieldAbsolutePVCoordinates<T>, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates: Subtractive constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates: Multiplicative 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
FieldAbsolutePVCoordinatesHermiteInterpolator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.utils: Class using a Hermite interpolator to interpolate absolute position-velocity-acceleration coordinates.
FieldAbsolutePVCoordinatesHermiteInterpolator(int, double, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator: Constructor.
FieldAbsolutePVCoordinatesHermiteInterpolator(int, Frame) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator: Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
FieldAbsolutePVCoordinatesHermiteInterpolator(int, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator: Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
FieldAbsolutePVCoordinatesHermiteInterpolator(Frame) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator: Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
FieldAbstractAlmanac<T extends CalculusFieldElement<T>,O extends AbstractAlmanac<O>> - Class in org.orekit.propagation.analytical.gnss.data: Base class for GNSS almanacs.
FieldAbstractAlmanac(Function<V, T>, FieldAbstractAlmanac<V, O>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldAbstractAlmanac: Constructor from different field instance.
FieldAbstractAlmanac(Field<T>, O) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldAbstractAlmanac: Constructor from non-field instance.
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.
FieldAbstractCartesianCost<T extends CalculusFieldElement<T>> - Class in org.orekit.control.indirect.adjoint.cost: Abstract class for cost with Cartesian coordinates.
FieldAbstractCartesianCost(String, T) - Constructor for class org.orekit.control.indirect.adjoint.cost.FieldAbstractCartesianCost: Constructor.
FieldAbstractDetector<D extends FieldAbstractDetector<D,T>,T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Common parts shared by several orbital events finders.
FieldAbstractDetector(FieldEventDetectionSettings<T>, FieldEventHandler<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).
FieldAbstractIntegratorBuilder<T extends CalculusFieldElement<T>,W extends AbstractFieldIntegrator<T>> - Class in org.orekit.propagation.conversion: This abstract class implements some of the required methods for integrators in propagators conversion.
FieldAbstractIntegratorBuilder() - Constructor for class org.orekit.propagation.conversion.FieldAbstractIntegratorBuilder
FieldAbstractNavigationMessage<T extends CalculusFieldElement<T>,O extends AbstractNavigationMessage<O>> - Class in org.orekit.propagation.analytical.gnss.data: Base class for GNSS navigation messages.
FieldAbstractNavigationMessage(Function<V, T>, FieldAbstractNavigationMessage<V, O>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldAbstractNavigationMessage: Constructor from different field instance.
FieldAbstractNavigationMessage(Field<T>, O) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldAbstractNavigationMessage: Constructor from non-field instance.
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.
FieldAbstractStateModifier<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation: Abstract base class for modifying state during propagation.
FieldAbstractStateModifier() - Constructor for class org.orekit.propagation.FieldAbstractStateModifier
FieldAdaptableInterval<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.events.intervals: This interface represents an event checking interval that depends on state.
FieldAdapterDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Deprecated.
since 13.0. Use FieldDetectorModifier instead.
FieldAdapterDetector(FieldEventDetector<T>) - Constructor for class org.orekit.propagation.events.FieldAdapterDetector: Deprecated.

Build an adaptor wrapping an existing detector.
FieldAdditionalDataProvider<O,T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation: This interface allows to modify FieldSpacecraftState and set up additional data.
FieldAdditionalDerivativesProvider<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.integration: Provider for additional derivatives.
FieldAltitudeDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Finder for satellite altitude crossing events.
FieldAltitudeDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector: Protected constructor with full parameters.
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(Field<T>, AngularCoordinates) - Constructor for class org.orekit.utils.FieldAngularCoordinates: Builds a FieldAngularCoordinates from a field and a regular AngularCoordinates.
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(FieldRotation) - Constructor for class org.orekit.utils.FieldAngularCoordinates: Builds a FieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.
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.
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(FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector: Constructor with full parameters.
FieldApsideDetector(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(Field<T>, Map<String, T[]>) - Constructor for class org.orekit.utils.FieldArrayDictionary: Constructor from a map.
FieldArrayDictionary(FieldArrayDictionary<T>) - Constructor for class org.orekit.utils.FieldArrayDictionary: Constructor from another dictionary.
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(Field<T>, Attitude) - Constructor for class org.orekit.attitudes.FieldAttitude: Builds an instance for a regular Attitude.
FieldAttitude(Frame, TimeStampedFieldAngularCoordinates<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(FieldAbsoluteDate<T>, Frame, FieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude: Creates a new instance.
FieldAttitudeInterpolator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.attitudes: Class for attitude interpolation.
FieldAttitudeInterpolator(Frame, FieldTimeInterpolator<TimeStampedFieldAngularCoordinates<KK>, KK>) - Constructor for class org.orekit.attitudes.FieldAttitudeInterpolator: Constructor.
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.
FieldAzimuthalGradientCoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.models.earth.troposphere: Container for the azimuthal gradient coefficients gn_h, ge_h, gn_w and ge_w.
FieldAzimuthalGradientCoefficients(T, T, T, T) - Constructor for class org.orekit.models.earth.troposphere.FieldAzimuthalGradientCoefficients: Simple constructor.
FieldBeidouAlmanac<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss.data: Class for BeiDou almanac.
FieldBeidouAlmanac(Function<V, T>, FieldBeidouAlmanac<V>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldBeidouAlmanac: Constructor from different field instance.
FieldBeidouAlmanac(Field<T>, BeidouAlmanac) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldBeidouAlmanac: Constructor from non-field instance.
FieldBeidouCivilianNavigationMessage<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a Beidou civilian navigation message.
FieldBeidouCivilianNavigationMessage(Function<V, T>, FieldBeidouCivilianNavigationMessage<V>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Constructor from different field instance.
FieldBeidouCivilianNavigationMessage(Field<T>, BeidouCivilianNavigationMessage) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Constructor from non-field instance.
FieldBeidouLegacyNavigationMessage<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a BeiDou navigation message.
FieldBeidouLegacyNavigationMessage(Function<V, T>, FieldBeidouLegacyNavigationMessage<V>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldBeidouLegacyNavigationMessage: Constructor from different field instance.
FieldBeidouLegacyNavigationMessage(Field<T>, BeidouLegacyNavigationMessage) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldBeidouLegacyNavigationMessage: Constructor from non-field instance.
FieldBetaAngleDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Finder for beta angle crossing events.
FieldBetaAngleDetector(Field<T>, T, FieldPVCoordinatesProvider<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldBetaAngleDetector: Class constructor.
FieldBetaAngleDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, T, FieldPVCoordinatesProvider<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldBetaAngleDetector: Protected constructor with full parameters.
FieldBetaAngleDetector(T) - Constructor for class org.orekit.propagation.events.FieldBetaAngleDetector: Solar beta angle 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.
FieldBooleanDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: This class provides AND and OR operations for event detectors.
FieldBooleanDetector(List<FieldEventDetector<T>>, FieldBooleanDetector.Operator, FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.FieldBooleanDetector: Private constructor with all the parameters.
FieldBoundedCartesianEnergy<T extends CalculusFieldElement<T>> - Class in org.orekit.control.indirect.adjoint.cost: Class for bounded energy cost with Cartesian coordinates.
FieldBoundedCartesianEnergy(String, T, T) - Constructor for class org.orekit.control.indirect.adjoint.cost.FieldBoundedCartesianEnergy: Constructor.
FieldBoundedCartesianEnergy(String, T, T, FieldEventDetectionSettings<T>) - Constructor for class org.orekit.control.indirect.adjoint.cost.FieldBoundedCartesianEnergy: 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>, 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>, 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, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Build a propagator from orbit, attitude provider 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>, AttitudeProvider, T, double, T, double, double, double, double, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Build a propagator from orbit, attitude provider, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, PropagationType, double, double, int) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Build a propagator from orbit, attitude provider, mass and potential.
FieldBrouwerLyddanePropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, PropagationType, double, OsculatingToMeanConverter) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Build a propagator from orbit, attitude provider, mass 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, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Private helper constructor.
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, 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>, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Build a propagator from orbit and potential provider.
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>, 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>, T, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Build a propagator from orbit, mass and potential provider.
FieldCartesianAdjointDerivativesProvider<T extends CalculusFieldElement<T>> - Class in org.orekit.control.indirect.adjoint: Class defining the Field version of the adjoint dynamics for Cartesian coordinates, as defined in the Pontryagin Maximum Principle.
FieldCartesianAdjointDerivativesProvider(FieldCartesianCost<T>, CartesianAdjointEquationTerm...) - Constructor for class org.orekit.control.indirect.adjoint.FieldCartesianAdjointDerivativesProvider: Constructor.
FieldCartesianCost<T extends CalculusFieldElement<T>> - Interface in org.orekit.control.indirect.adjoint.cost: Interface to definite cost function in the frame of Pontryagin's Maximum Principle using Cartesian coordinates.
FieldCartesianFlightDurationCost<T extends CalculusFieldElement<T>> - Class in org.orekit.control.indirect.adjoint.cost: Class for minimizing the flight duration (a.k.a. time of flight) with Cartesian coordinates.
FieldCartesianFlightDurationCost(String, T, T) - Constructor for class org.orekit.control.indirect.adjoint.cost.FieldCartesianFlightDurationCost: Constructor.
FieldCartesianFuelCost<T extends CalculusFieldElement<T>> - Class in org.orekit.control.indirect.adjoint.cost: Class for fuel cost with Cartesian coordinates.
FieldCartesianFuelCost(String, T, T) - Constructor for class org.orekit.control.indirect.adjoint.cost.FieldCartesianFuelCost: Constructor with default detection settings.
FieldCartesianFuelCost(String, T, T, FieldEventDetectionSettings<T>) - Constructor for class org.orekit.control.indirect.adjoint.cost.FieldCartesianFuelCost: Constructor.
FieldCartesianOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits: This class holds Cartesian orbital parameters.
FieldCartesianOrbit(Field<T>, CartesianOrbit) - Constructor for class org.orekit.orbits.FieldCartesianOrbit: Constructor from Field and CartesianOrbit.
FieldCartesianOrbit(Field<T>, Orbit) - Constructor for class org.orekit.orbits.FieldCartesianOrbit: Constructor from Field and Orbit.
FieldCartesianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCartesianOrbit: Constructor from any kind of orbital parameters.
FieldCartesianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCartesianOrbit: Constructor from Cartesian parameters.
FieldCartesianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldCartesianOrbit: Constructor from Cartesian parameters.
FieldCellInterpolator<T extends CalculusFieldElement<T>> - Class in org.orekit.models.earth.weather: Interpolator within a grid cell.
FieldChronologicalComparator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.time: Comparator for FieldTimeStamped instance.
FieldChronologicalComparator() - Constructor for class org.orekit.time.FieldChronologicalComparator: Simple constructor.
FieldCircularLatitudeArgumentUtility - Class in org.orekit.orbits: Utility methods for converting between different latitude arguments used by FieldCircularOrbit.
FieldCircularOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits: This class handles circular orbital parameters.
FieldCircularOrbit(Field<T>, CircularOrbit) - Constructor for class org.orekit.orbits.FieldCircularOrbit: Constructor from Field and CircularOrbit.
FieldCircularOrbit(Field<T>, Orbit) - Constructor for class org.orekit.orbits.FieldCircularOrbit: Constructor from Field and Orbit.
FieldCircularOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCircularOrbit: Constructor from any kind of orbital parameters.
FieldCircularOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit: Constructor from Cartesian parameters.
FieldCircularOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit: Constructor from Cartesian parameters.
FieldCircularOrbit(T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit: Creates a new instance without derivatives and with cached position angle same as value inputted.
FieldCircularOrbit(T, T, T, T, T, T, PositionAngleType, PositionAngleType, 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, PositionAngleType, 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, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit: Creates a new instance.
FieldCivilianNavigationMessage<T extends CalculusFieldElement<T>,O extends CivilianNavigationMessage<O>> - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a GPS/QZNSS civilian navigation message.
FieldCivilianNavigationMessage(Function<V, T>, FieldCivilianNavigationMessage<V, O>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Constructor from different field instance.
FieldCivilianNavigationMessage(Field<T>, O) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Constructor from non-field instance.
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.
FieldClockCorrectionsProvider<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss: Provider for clock corrections as additional states.
FieldClockCorrectionsProvider(FieldGNSSClockElements<T>, double) - Constructor for class org.orekit.propagation.analytical.gnss.FieldClockCorrectionsProvider: Simple constructor.
FieldClockOffset<T extends CalculusFieldElement<T>> - Class in org.orekit.time: Container for time stamped clock offset.
FieldClockOffset(FieldAbsoluteDate<T>, T, T, T) - Constructor for class org.orekit.time.FieldClockOffset: Simple constructor.
FieldClockOffsetHermiteInterpolator<T extends CalculusFieldElement<T>> - Class in org.orekit.time: bHermite interpolator of time stamped clock offsets.
FieldClockOffsetHermiteInterpolator(int) - Constructor for class org.orekit.time.FieldClockOffsetHermiteInterpolator: Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
FieldClockOffsetHermiteInterpolator(int, double) - Constructor for class org.orekit.time.FieldClockOffsetHermiteInterpolator: Constructor.
FieldCombinedDerivatives<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.integration: Container for additional derivatives.
FieldCombinedDerivatives(T[], T[]) - Constructor for class org.orekit.propagation.integration.FieldCombinedDerivatives: Simple constructor.
FieldCommonGnssData<T extends CalculusFieldElement<T>,O extends CommonGnssData<O>> - Class in org.orekit.propagation.analytical.gnss.data: Container for common GNSS data contained in almanac and navigation messages.
FieldCommonGnssData(Function<V, T>, FieldCommonGnssData<V, O>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldCommonGnssData: Constructor from different field instance.
FieldCommonGnssData(Field<T>, O) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldCommonGnssData: Constructor from non-field instance.
FieldContinueOnEvent<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: Empty constructor.
FieldControlSwitchDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.control.indirect.adjoint.cost: Abstract event detector for singularities in adjoint dynamics.
FieldControlSwitchDetector(FieldEventDetectionSettings<T>) - Constructor for class org.orekit.control.indirect.adjoint.cost.FieldControlSwitchDetector: Constructor.
FieldCountAndContinue<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers: Event handler counting event occurrences and always returning Action.CONTINUE.
FieldCountAndContinue(int) - Constructor for class org.orekit.propagation.events.handlers.FieldCountAndContinue: Constructor.
FieldCountingHandler<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers: Abstract class for handlers counting event occurrences.
FieldCountingHandler(int, Action) - Constructor for class org.orekit.propagation.events.handlers.FieldCountingHandler: Constructor.
FieldCylindricalShadowEclipseDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Event detector for eclipses from a single, infinitely-distant light source, occulted by a spherical central body.
FieldCylindricalShadowEclipseDetector(ExtendedPositionProvider, T, FieldEventDetectionSettings<T>, FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.FieldCylindricalShadowEclipseDetector: Constructor.
FieldCylindricalShadowEclipseDetector(ExtendedPositionProvider, T, FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.FieldCylindricalShadowEclipseDetector: Constructor with default detection settings.
FieldDataDictionary<T extends CalculusFieldElement<T>> - Class in org.orekit.utils: String → Object mapping, for small number of keys.
FieldDataDictionary(Field<T>) - Constructor for class org.orekit.utils.FieldDataDictionary: Constructor with default initial capacity.
FieldDataDictionary(Field<T>, int) - Constructor for class org.orekit.utils.FieldDataDictionary: Constructor with specified capacity.
FieldDataDictionary(Field<T>, Map<String, Object>) - Constructor for class org.orekit.utils.FieldDataDictionary: Constructor from a map.
FieldDataDictionary(FieldDataDictionary<T>) - Constructor for class org.orekit.utils.FieldDataDictionary: Constructor from another dictionary.
FieldDataDictionary.Entry - Class in org.orekit.utils: Entry in a dictionary.
FieldDateDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Finder for date events.
FieldDateDetector(Field<T>, FieldTimeStamped<T>...) - Constructor for class org.orekit.propagation.events.FieldDateDetector: Build a new instance.
FieldDateDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, double, FieldTimeStamped<T>...) - Constructor for class org.orekit.propagation.events.FieldDateDetector: Protected constructor with full parameters.
FieldDateDetector(FieldAbsoluteDate<T>) - Constructor for class org.orekit.propagation.events.FieldDateDetector: Build a new instance from a fielded date.
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, Frame, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldDeepSDP4: Constructor for a unique initial TLE.
FieldDeepSDP4(FieldTLE<T>, AttitudeProvider, T, 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.
FieldDetectorModifier<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.events: Base class for modifying an existing getDetector().
FieldDSSTGravityContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces: This class is a container for the common parameters used in DSSTTesseral and DSSTZonal.
FieldDSSTJ2SquaredClosedFormContext<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces: This class is a container for the common parameters used in DSSTJ2SquaredClosedForm.
FieldDSSTJ2SquaredClosedFormContext(FieldAuxiliaryElements<T>, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext: 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>) - 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.
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.
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.
FieldDSSTThirdBodyDynamicContext<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.
FieldDSSTThirdBodyDynamicContext(FieldAuxiliaryElements<T>, CelestialBody, T[]) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Constructor.
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>, 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>, 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, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from FieldOrbit, attitude provider 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>, AttitudeProvider, T, double, T, double, double, double, double, double, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double, PropagationType, double, int) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double, PropagationType, OsculatingToMeanConverter) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from FieldOrbit, attitude provider, mass 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, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Private helper constructor.
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, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from orbit, attitude provider, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from FieldOrbit and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from orbit 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>, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from FieldOrbit, mass and potential provider.
FieldEclipseDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Finder for satellite eclipse related events.
FieldEclipseDetector(Field<T>, ExtendedPositionProvider, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector: Build a new eclipse detector.
FieldEclipseDetector(Field<T>, OccultationEngine) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector: Build a new eclipse detector.
FieldEclipseDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, OccultationEngine, T, boolean) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector: Protected constructor with full parameters.
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(FieldEventDetectionSettings<T>, FieldEventHandler<T>, double, ElevationMask, AtmosphericRefractionModel, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector: Protected constructor with full parameters.
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.
FieldElevationExtremumDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Detector for elevation extremum with respect to a ground point.
FieldElevationExtremumDetector(Field<T>, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationExtremumDetector: Build a new detector.
FieldElevationExtremumDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationExtremumDetector: Protected constructor with full parameters.
FieldElevationExtremumDetector(T, T, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationExtremumDetector: Build a detector.
FieldEllipse<T extends CalculusFieldElement<T>> - Class in org.orekit.bodies: Model of a 2D ellipse in 3D space.
FieldEllipse(FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>, T, T, Frame) - Constructor for class org.orekit.bodies.FieldEllipse: Simple constructor.
FieldEnablingPredicate<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.events: This interface represents an event enabling predicate function.
FieldEphemerisGenerator<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation: Generator for ephemerides.
FieldEquinoctialLongitudeArgumentUtility - Class in org.orekit.orbits: Utility methods for converting between different longitude arguments used by FieldEquinoctialOrbit.
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(Field<T>, EquinoctialOrbit) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit: Constructor from Field and EquinoctialOrbit.
FieldEquinoctialOrbit(Field<T>, Orbit) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit: Constructor from Field and Orbit.
FieldEquinoctialOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit: Constructor from any kind of orbital parameters.
FieldEquinoctialOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit: Constructor from Cartesian parameters.
FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit: Constructor from Cartesian parameters.
FieldEquinoctialOrbit(T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit: Creates a new instance.
FieldEquinoctialOrbit(T, T, T, T, T, T, PositionAngleType, PositionAngleType, 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, PositionAngleType, 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, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit: Creates a new instance.
FieldEventDetectionSettings<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Class containing parameters for event detection.
FieldEventDetectionSettings(double, T, int) - Constructor for class org.orekit.propagation.events.FieldEventDetectionSettings: Constructor with maximum check as double.
FieldEventDetectionSettings(Field<T>, EventDetectionSettings) - Constructor for class org.orekit.propagation.events.FieldEventDetectionSettings: Constructor from non-Field settings.
FieldEventDetectionSettings(FieldAdaptableInterval<T>, T, int) - Constructor for class org.orekit.propagation.events.FieldEventDetectionSettings: Constructor.
FieldEventDetector<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.events: This interface represents space-dynamics aware events detectors.
FieldEventEnablingPredicateFilter<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Wrapper used to detect events only when enabled by an external predicated function.
FieldEventEnablingPredicateFilter(FieldEventDetectionSettings<T>, FieldEventDetector<T>, FieldEnablingPredicate<T>) - Constructor for class org.orekit.propagation.events.FieldEventEnablingPredicateFilter: Constructor with full parameters.
FieldEventEnablingPredicateFilter(FieldEventDetector<T>, FieldEnablingPredicate<T>) - Constructor for class org.orekit.propagation.events.FieldEventEnablingPredicateFilter: Wrap an event detector.
FieldEventHandler<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.events.handlers: An interface defining how to handle events occurring during propagation..
FieldEventShifter<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Wrapper shifting events occurrences times.
FieldEventShifter(FieldEventDetectionSettings<T>, FieldEventDetector<T>, boolean, T, T) - Constructor for class org.orekit.propagation.events.FieldEventShifter: Constructor with full parameters.
FieldEventShifter(FieldEventDetector<T>, boolean, T, T) - Constructor for class org.orekit.propagation.events.FieldEventShifter: Build a new instance.
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.
FieldEventSlopeFilter<D extends FieldEventDetector<T>,T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Wrapper used to detect only increasing or decreasing events.
FieldEventSlopeFilter(D, FilterType) - Constructor for class org.orekit.propagation.events.FieldEventSlopeFilter: Wrap an event detector.
FieldEventSlopeFilter(FieldEventDetectionSettings<T>, D, FilterType) - Constructor for class org.orekit.propagation.events.FieldEventSlopeFilter: Constructor with full parameters.
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.
FieldExplicitRungeKuttaIntegratorBuilder<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.conversion: This interface is the top-level abstraction to build first order integrators for propagators conversion.
FieldExtremumApproachDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Finder for extremum approach events.
FieldExtremumApproachDetector(Field<T>, FieldPVCoordinatesProvider<T>) - Constructor for class org.orekit.propagation.events.FieldExtremumApproachDetector: Constructor with default values.
FieldExtremumApproachDetector(Field<T>, PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.FieldExtremumApproachDetector: Constructor with default values.
FieldExtremumApproachDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, FieldPVCoordinatesProvider<T>) - Constructor for class org.orekit.propagation.events.FieldExtremumApproachDetector: Constructor.
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.
FieldFunctionalDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, Function<FieldSpacecraftState<T>, T>) - Constructor for class org.orekit.propagation.events.FieldFunctionalDetector: Protected constructor.
FieldGalileoAlmanac<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss.data: Class for Galileo almanac.
FieldGalileoAlmanac(Function<V, T>, FieldGalileoAlmanac<V>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldGalileoAlmanac: Constructor from different field instance.
FieldGalileoAlmanac(Field<T>, GalileoAlmanac) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldGalileoAlmanac: Constructor from non-field instance.
FieldGalileoNavigationMessage<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a Galileo navigation message.
FieldGalileoNavigationMessage(Function<V, T>, FieldGalileoNavigationMessage<V>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldGalileoNavigationMessage: Constructor from different field instance.
FieldGalileoNavigationMessage(Field<T>, GalileoNavigationMessage) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldGalileoNavigationMessage: Constructor from non-field instance.
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(Field<T>, GeodeticPoint) - Constructor for class org.orekit.bodies.FieldGeodeticPoint: Build a new instance from a GeodeticPoint.
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.
FieldGNSSClockElements<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.analytical.gnss.data: This interface provides the minimal set of clock elements needed by the FieldClockCorrectionsProvider.
FieldGnssOrbitalElements<T extends CalculusFieldElement<T>,O extends GNSSOrbitalElements<O>> - Class in org.orekit.propagation.analytical.gnss.data: This class provides the minimal set of orbital elements needed by the FieldGnssPropagator.
FieldGnssOrbitalElements(Function<V, T>, FieldGnssOrbitalElements<V, O>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements: Constructor from different field instance.
FieldGnssOrbitalElements(Field<T>, O) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements: Constructor from non-field instance.
FieldGnssOrbitalElements(T, double, int, TimeScales, SatelliteSystem) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements: Simple constructor.
FieldGnssPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss: Common handling of FieldAbstractAnalyticalPropagator methods for GNSS propagators.
FieldGnssPropagatorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss: This nested class aims at building a GNSSPropagator.
FieldGnssPropagatorBuilder(FieldGnssOrbitalElements<T, ?>) - Constructor for class org.orekit.propagation.analytical.gnss.FieldGnssPropagatorBuilder: Initializes the builder.
FieldGnssPropagatorBuilder(FieldGnssOrbitalElements<T, ?>, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.FieldGnssPropagatorBuilder: Initializes the builder.
FieldGPSAlmanac<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss.data: This class holds a GPS almanac as read from SEM or YUMA files.
FieldGPSAlmanac(Function<V, T>, FieldGPSAlmanac<V>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldGPSAlmanac: Constructor from different field instance.
FieldGPSAlmanac(Field<T>, GPSAlmanac) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldGPSAlmanac: Constructor from non-field instance.
FieldGPSCivilianNavigationMessage<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a GPS navigation message.
FieldGPSCivilianNavigationMessage(Function<V, T>, FieldGPSCivilianNavigationMessage<V>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldGPSCivilianNavigationMessage: Constructor from different field instance.
FieldGPSCivilianNavigationMessage(Field<T>, GPSCivilianNavigationMessage) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldGPSCivilianNavigationMessage: Constructor from non-field instance.
FieldGPSLegacyNavigationMessage<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a GPS navigation message.
FieldGPSLegacyNavigationMessage(Function<V, T>, FieldGPSLegacyNavigationMessage<V>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldGPSLegacyNavigationMessage: Constructor from different field instance.
FieldGPSLegacyNavigationMessage(Field<T>, GPSLegacyNavigationMessage) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldGPSLegacyNavigationMessage: Constructor from non-field instance.
FieldHansenTesseralLinear<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen: Hansen coefficients K(t,n,s) for t!
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.
Fieldifier - Class in org.orekit.utils: Utility class used to convert class to their Field equivalent.
fieldify(Field<T>, RealMatrix) - Static method in class org.orekit.utils.Fieldifier: Fieldify given matrix with given field.
fieldify(Field<T>, StateCovariance) - Static method in class org.orekit.utils.Fieldifier: Fieldify given state covariance with given field.
FieldImpulseManeuver<T extends CalculusFieldElement<T>> - Class in org.orekit.forces.maneuvers: Impulse maneuver model for propagators working with Fields.
FieldImpulseManeuver(FieldEventDetector<T>, FieldVector3D<T>, T) - Constructor for class org.orekit.forces.maneuvers.FieldImpulseManeuver: Build a new instance.
FieldImpulseManeuver(FieldEventDetector<T>, AttitudeProvider, FieldVector3D<T>, T) - Constructor for class org.orekit.forces.maneuvers.FieldImpulseManeuver: Build a new instance.
FieldImpulseManeuver(FieldEventDetector<T>, AttitudeProvider, FieldVector3D<T>, T, Control3DVectorCostType) - Constructor for class org.orekit.forces.maneuvers.FieldImpulseManeuver: Deprecated.
since 13.0
FieldImpulseManeuver(FieldEventDetector<T>, AttitudeProvider, FieldImpulseProvider<T>, T, Control3DVectorCostType) - Constructor for class org.orekit.forces.maneuvers.FieldImpulseManeuver: Build a new instance.
FieldImpulseProvider<T extends CalculusFieldElement<T>> - Interface in org.orekit.forces.maneuvers: Interface providing velocity increment vectors to impulsive maneuvers (Field version).
FieldInertia<T extends CalculusFieldElement<T>> - Class in org.orekit.attitudes: Container for inertia of a 3D object.
FieldInertiaAxis<T extends CalculusFieldElement<T>> - Class in org.orekit.attitudes: Container for inertial axis.
FieldInertiaAxis(T, FieldVector3D<T>) - Constructor for class org.orekit.attitudes.FieldInertiaAxis: Simple constructor to pair a moment of inertia with its associated axis.
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>, AttitudeProvider, PropagationType, FieldDenseOutputModel<T>, FieldDataDictionary<T>, List<FieldAdditionalDataProvider<?, T>>, String[], int[]) - Constructor for class org.orekit.propagation.integration.FieldIntegratedEphemeris: Creates a new instance of IntegratedEphemeris.
FieldIntelsatElevenElements<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.intelsat: This class is a container for a single set of Intelsat's 11 Elements data.
FieldIntelsatElevenElements(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements: Constructor.
FieldIntelsatElevenElementsPropagator<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.intelsat: This class provides elements to propagate Intelsat's 11 elements.
FieldIntelsatElevenElementsPropagator(FieldIntelsatElevenElements<T>) - Constructor for class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator: Default constructor.
FieldIntelsatElevenElementsPropagator(FieldIntelsatElevenElements<T>, Frame, Frame) - Constructor for class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator: Constructor.
FieldIntelsatElevenElementsPropagator(FieldIntelsatElevenElements<T>, Frame, Frame, AttitudeProvider, T) - Constructor for class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator: Constructor.
FieldInterpolationGrid<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.semianalytical.dsst.utilities: Interface for interpolation grids.
FieldIRNSSAlmanac<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss.data: Class for IRNSS almanac.
FieldIRNSSAlmanac(Function<V, T>, FieldIRNSSAlmanac<V>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldIRNSSAlmanac: Constructor from different field instance.
FieldIRNSSAlmanac(Field<T>, IRNSSAlmanac) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldIRNSSAlmanac: Constructor from non-field instance.
FieldIRNSSNavigationMessage<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in an IRNSS navigation message.
FieldIRNSSNavigationMessage(Function<V, T>, FieldIRNSSNavigationMessage<V>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldIRNSSNavigationMessage: Constructor from different field instance.
FieldIRNSSNavigationMessage(Field<T>, IRNSSNavigationMessage) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldIRNSSNavigationMessage: Constructor from non-field instance.
FieldKeplerianAnomalyUtility - Class in org.orekit.orbits: Utility methods for converting between different Keplerian anomalies.
FieldKeplerianOrbit<T extends CalculusFieldElement<T>> - Class in org.orekit.orbits: This class handles traditional Keplerian orbital parameters.
FieldKeplerianOrbit(Field<T>, KeplerianOrbit) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Constructor from Field and KeplerianOrbit.
FieldKeplerianOrbit(Field<T>, Orbit) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Constructor from Field and Orbit.
FieldKeplerianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Constructor from any kind of orbital parameters.
FieldKeplerianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Constructor from Cartesian parameters.
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Constructor from Cartesian parameters.
FieldKeplerianOrbit(T, T, T, T, T, T, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Creates a new instance.
FieldKeplerianOrbit(T, T, T, T, T, T, PositionAngleType, PositionAngleType, 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, PositionAngleType, 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, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Creates a new instance.
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>, 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.
FieldKeplerianPropagator(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator: Build a propagator from orbit and central attraction coefficient μ.
FieldKinematicTransform<T extends CalculusFieldElement<T>> - Interface in org.orekit.frames: A transform that only includes translation and rotation as well as their respective rates.
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(FieldEventDetectionSettings<T>, FieldEventHandler<T>, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeCrossingDetector: Protected constructor with full parameters.
FieldLatitudeCrossingDetector(T, T, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeCrossingDetector: Build a detector.
FieldLatitudeRangeCrossingDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Detector for geographic latitude crossing.
FieldLatitudeRangeCrossingDetector(Field<T>, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeRangeCrossingDetector: Build a new detector.
FieldLatitudeRangeCrossingDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeRangeCrossingDetector: Private constructor with full parameters.
FieldLatitudeRangeCrossingDetector(T, T, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeRangeCrossingDetector: Build a detector.
FieldLegacyNavigationMessage<T extends CalculusFieldElement<T>,O extends LegacyNavigationMessage<O>> - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a GPS/QZNSS legacy navigation message.
FieldLegacyNavigationMessage(Function<V, T>, FieldLegacyNavigationMessage<V, O>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldLegacyNavigationMessage: Constructor from different field instance.
FieldLegacyNavigationMessage(Field<T>, O) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldLegacyNavigationMessage: Constructor from non-field instance.
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[][], SortedMap<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.
FieldLogarithmicBarrierCartesianFuel<T extends CalculusFieldElement<T>> - Class in org.orekit.control.indirect.adjoint.cost: Fuel cost penalized with a logarithmic term, which is a barrier so is not defined for epsilon equal to 0 or 1.
FieldLogarithmicBarrierCartesianFuel(String, T, T, T) - Constructor for class org.orekit.control.indirect.adjoint.cost.FieldLogarithmicBarrierCartesianFuel: Constructor.
FieldLongitudeCrossingDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Detector for geographic longitude crossing.
FieldLongitudeCrossingDetector(Field<T>, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeCrossingDetector: Build a new detector.
FieldLongitudeCrossingDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeCrossingDetector: Protected constructor with full parameters.
FieldLongitudeCrossingDetector(T, T, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeCrossingDetector: Build a detector.
FieldLongitudeRangeCrossingDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Detector for geographic longitude crossing.
FieldLongitudeRangeCrossingDetector(Field<T>, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector: Build a new detector.
FieldLongitudeRangeCrossingDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector: Protected constructor with full parameters.
FieldLongitudeRangeCrossingDetector(T, T, OneAxisEllipsoid, double, double) - Constructor for class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector: Build a detector.
FieldManeuverTriggerDetector<W extends CalculusFieldElement<W>,T extends FieldEventDetector<W>> - Class in org.orekit.forces.maneuvers.trigger: Wrapper for event detection triggering maneuvers (Field version).
FieldManeuverTriggerDetector(T, FieldEventHandler<W>) - Constructor for class org.orekit.forces.maneuvers.trigger.FieldManeuverTriggerDetector: Constructor.
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.
fieldNaturalToProper(Gradient[], FieldTransform<Gradient>, Frame) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier: Natural to proper correction for aberration of light.
fieldNaturalToProper(Gradient[], FieldTransform<Gradient>, Frame, DataContext) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier: Natural to proper correction for aberration of light.
FieldNegateDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: An event detector that negates the sign on another event detector's g function.
FieldNegateDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, FieldEventDetector<T>) - Constructor for class org.orekit.propagation.events.FieldNegateDetector: Protected constructor.
FieldNegateDetector(FieldEventDetector<T>) - Constructor for class org.orekit.propagation.events.FieldNegateDetector: Create a new event detector that negates an existing event detector.
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(FieldEventDetectionSettings<T>, FieldEventHandler<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector: Protected constructor with full parameters.
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.
FieldODEIntegratorBuilder<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.conversion: This interface is the top-level abstraction to build first order integrators for propagators conversion.
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(EventDetectionSettings, EventHandler, PVCoordinatesProvider, double, VisibilityTrigger, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector: Protected constructor with full parameters.
FieldOfViewDetector(PVCoordinatesProvider, double, VisibilityTrigger, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector: Build a new instance.
FieldOfViewDetector(PVCoordinatesProvider, 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.
FieldOrbitBlender<KK extends CalculusFieldElement<KK>> - Class in org.orekit.orbits: Orbit blender.
FieldOrbitBlender(SmoothStepFactory.FieldSmoothStepFunction<KK>, FieldAbstractAnalyticalPropagator<KK>, Frame) - Constructor for class org.orekit.orbits.FieldOrbitBlender: Default constructor.
FieldOrbitHermiteInterpolator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.orbits: Class using a Hermite interpolator to interpolate orbits.
FieldOrbitHermiteInterpolator(int, double, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.orbits.FieldOrbitHermiteInterpolator: Constructor.
FieldOrbitHermiteInterpolator(int, Frame) - Constructor for class org.orekit.orbits.FieldOrbitHermiteInterpolator: Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
FieldOrbitHermiteInterpolator(int, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.orbits.FieldOrbitHermiteInterpolator: Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
FieldOrbitHermiteInterpolator(Frame) - Constructor for class org.orekit.orbits.FieldOrbitHermiteInterpolator: Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
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.
FieldParameterDrivenDateIntervalDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, DateDriver, DateDriver, DateDriver, ParameterDriver) - Constructor for class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector: Protected constructor with full parameters.
FieldPenalizedCartesianFuelCost<T extends CalculusFieldElement<T>> - Class in org.orekit.control.indirect.adjoint.cost: Abstract class for fuel cost with a penalty term proportional to a weight parameter epsilon.
FieldPenalizedCartesianFuelCost(String, T, T, T) - Constructor for class org.orekit.control.indirect.adjoint.cost.FieldPenalizedCartesianFuelCost: Constructor.
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.
FieldPressureTemperature<T extends CalculusFieldElement<T>> - Class in org.orekit.models.earth.weather: Container for pressure and temperature.
FieldPressureTemperature(Field<T>, PressureTemperatureHumidity) - Constructor for class org.orekit.models.earth.weather.FieldPressureTemperature: Simple constructor.
FieldPressureTemperature(T, T, T) - Constructor for class org.orekit.models.earth.weather.FieldPressureTemperature: Simple constructor.
FieldPressureTemperatureHumidity<T extends CalculusFieldElement<T>> - Class in org.orekit.models.earth.weather: Container for pressure, temperature, and humidity.
FieldPressureTemperatureHumidity(Field<T>, PressureTemperatureHumidity) - Constructor for class org.orekit.models.earth.weather.FieldPressureTemperatureHumidity: Simple constructor.
FieldPressureTemperatureHumidity(T, T, T, T, T, T) - Constructor for class org.orekit.models.earth.weather.FieldPressureTemperatureHumidity: Simple constructor.
FieldProbabilityOfCollision<T extends CalculusFieldElement<T>> - Class in org.orekit.ssa.metrics: Container for values relative to the probability of collision : Value of the probability of collision. Name of the method with which it was computed. Upper and lower limit of the value if the method provides them (such as Laas2015 for example). Flag defining if the probability was maximized in any way (such as Alfriend1999Max for example).
FieldProbabilityOfCollision(T, String) - Constructor for class org.orekit.ssa.metrics.FieldProbabilityOfCollision: Constructor with default values of 0 for the upper/lower limits and default false flag for maximum probability.
FieldProbabilityOfCollision(T, String, boolean) - Constructor for class org.orekit.ssa.metrics.FieldProbabilityOfCollision: Constructor with default values of 0 for the upper and lower limits.
FieldProbabilityOfCollision(T, T, T, String, boolean) - Constructor for class org.orekit.ssa.metrics.FieldProbabilityOfCollision: Constructor.
FieldPropagationStepRecorder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.sampling: Step handler recording states.
FieldPropagationStepRecorder() - Constructor for class org.orekit.propagation.sampling.FieldPropagationStepRecorder: Constructor.
FieldPropagator<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation: This interface provides a way to propagate an orbit at any time.
fieldProperToNatural(Gradient[], FieldTransform<Gradient>, Frame) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier: Proper to natural correction for aberration of light.
fieldProperToNatural(Gradient[], FieldTransform<Gradient>, Frame, DataContext) - Static method in class org.orekit.estimation.measurements.modifiers.AberrationModifier: Proper to natural correction for aberration of light.
FieldPVCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils: Simple container for Position/Velocity pairs, using CalculusFieldElement.
FieldPVCoordinates(double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Multiplicative constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - 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(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(Field<T>, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Builds a FieldPVCoordinates from a field and a regular PVCoordinates.
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(FieldVector3D) - Constructor for class org.orekit.utils.FieldPVCoordinates: Builds a FieldPVCoordinates triplet from a FieldVector3D<FieldDerivative>.
FieldPVCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Subtractive constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Multiplicative constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, 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, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Multiplicative constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates) - 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(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinatesProvider<T extends CalculusFieldElement<T>> - Interface in org.orekit.utils: Interface for PV coordinates providers.
FieldQuadraticPenaltyCartesianFuel<T extends CalculusFieldElement<T>> - Class in org.orekit.control.indirect.adjoint.cost: Fuel cost penalized with a quadratic term.
FieldQuadraticPenaltyCartesianFuel(String, T, T, T) - Constructor for class org.orekit.control.indirect.adjoint.cost.FieldQuadraticPenaltyCartesianFuel: Constructor with default event detection settings.
FieldQuadraticPenaltyCartesianFuel(String, T, T, T, FieldEventDetectionSettings<T>) - Constructor for class org.orekit.control.indirect.adjoint.cost.FieldQuadraticPenaltyCartesianFuel: Constructor.
FieldQZSSAlmanac<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss.data: This class holds a QZSS almanac as read from YUMA files.
FieldQZSSAlmanac(Function<V, T>, FieldQZSSAlmanac<V>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldQZSSAlmanac: Constructor from different field instance.
FieldQZSSAlmanac(Field<T>, QZSSAlmanac) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldQZSSAlmanac: Constructor from non-field instance.
FieldQZSSCivilianNavigationMessage<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a QZSS navigation message.
FieldQZSSCivilianNavigationMessage(Function<V, T>, FieldQZSSCivilianNavigationMessage<V>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldQZSSCivilianNavigationMessage: Constructor from different field instance.
FieldQZSSCivilianNavigationMessage(Field<T>, QZSSCivilianNavigationMessage) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldQZSSCivilianNavigationMessage: Constructor from non-field instance.
FieldQZSSLegacyNavigationMessage<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.analytical.gnss.data: Container for data contained in a QZSS navigation message.
FieldQZSSLegacyNavigationMessage(Function<V, T>, FieldQZSSLegacyNavigationMessage<V>) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldQZSSLegacyNavigationMessage: Constructor from different field instance.
FieldQZSSLegacyNavigationMessage(Field<T>, QZSSLegacyNavigationMessage) - Constructor for class org.orekit.propagation.analytical.gnss.data.FieldQZSSLegacyNavigationMessage: Constructor from non-field instance.
FieldRecallLastOccurrence<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers: Event handler wrapping another, arbitrary one whilst remembering date of last detection.
FieldRecallLastOccurrence(FieldEventHandler<T>) - Constructor for class org.orekit.propagation.events.handlers.FieldRecallLastOccurrence: Constructor.
FieldRecordAndContinue<T extends CalculusFieldElement<T>> - 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>>) - Constructor for class org.orekit.propagation.events.handlers.FieldRecordAndContinue: Create a handler using the given collection to store events.
FieldRecordAndContinue.Event<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers: A single event detected during propagation.
FieldRelativeDistanceDetector<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events: Detector of specific value for the distance relative to another trajectory (using the Euclidean norm).
FieldRelativeDistanceDetector(FieldEventDetectionSettings<T>, FieldEventHandler<T>, FieldPVCoordinatesProvider<T>, T) - Constructor for class org.orekit.propagation.events.FieldRelativeDistanceDetector: Constructor.
FieldRelativeDistanceDetector(FieldPVCoordinatesProvider<T>, T) - Constructor for class org.orekit.propagation.events.FieldRelativeDistanceDetector: Constructor with default values.
FieldResetDerivativesOnEvent<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.events.handlers: Event handler which will always return continue as a state.
FieldResetDerivativesOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldResetDerivativesOnEvent
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, Frame, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldSGP4: Constructor for a unique initial TLE.
FieldSGP4(FieldTLE<T>, AttitudeProvider, T, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldSGP4: Constructor for a unique initial TLE.
FieldShiftingPVCoordinatesProvider<T extends CalculusFieldElement<T>> - Class in org.orekit.utils: Provider using simple FieldPVCoordinates.shiftedBy(CalculusFieldElement) shiftedBy} and frame transforms for evolution.
FieldShiftingPVCoordinatesProvider(TimeStampedFieldPVCoordinates<T>, Frame) - Constructor for class org.orekit.utils.FieldShiftingPVCoordinatesProvider: Simple constructor.
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.
FieldShortTermEncounter2DDefinition<T extends CalculusFieldElement<T>> - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod: Defines the encounter between two collision object at time of closest approach assuming a short-term encounter model .
FieldShortTermEncounter2DDefinition(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Constructor.
FieldShortTermEncounter2DDefinition(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T, EncounterLOFType, double) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Constructor.
FieldShortTermEncounter2DDefinition(FieldOrbit<T>, FieldStateCovariance<T>, T, FieldOrbit<T>, FieldStateCovariance<T>, T) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Constructor.
FieldShortTermEncounter2DDefinition(FieldOrbit<T>, FieldStateCovariance<T>, T, FieldOrbit<T>, FieldStateCovariance<T>, T, EncounterLOFType, double) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Constructor.
FieldSortedListTrimmer - Class in org.orekit.utils: A trimmer for externally stored chronologically sorted lists.
FieldSortedListTrimmer(int) - Constructor for class org.orekit.utils.FieldSortedListTrimmer: Create a new cache with the given neighbors size and data.
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, meant primarily for propagation.
FieldSpacecraftState(Field<T>, SpacecraftState) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Convert a FieldSpacecraftState.
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>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Deprecated.
since 13.0, use withXXX
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, FieldDataDictionary<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit, attitude, mass, additional states and derivatives.
FieldSpacecraftState(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Deprecated.
since 13.0, use withXXX
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>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Deprecated.
since 13.0, use withXXX
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T, FieldDataDictionary<T>, FieldArrayDictionary<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit, attitude and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Deprecated.
since 13.0, use withXXX
FieldSpacecraftStateInterpolator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.propagation: Generic class for spacecraft state interpolator.
FieldSpacecraftStateInterpolator(int, double, Frame) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator: Constructor to create a customizable Hermite interpolator for every spacecraft state field.
FieldSpacecraftStateInterpolator(int, double, Frame, Frame) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator: Constructor to create a customizable Hermite interpolator for every spacecraft state field.
FieldSpacecraftStateInterpolator(int, double, Frame, Frame, CartesianDerivativesFilter, AngularDerivativesFilter) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator: Constructor.
FieldSpacecraftStateInterpolator(int, double, Frame, FieldTimeInterpolator<FieldOrbit<KK>, KK>, FieldTimeInterpolator<FieldAbsolutePVCoordinates<KK>, KK>, FieldTimeInterpolator<TimeStampedField<KK>, KK>, FieldTimeInterpolator<FieldAttitude<KK>, KK>, FieldTimeInterpolator<TimeStampedField<KK>, KK>) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator: Constructor.
FieldSpacecraftStateInterpolator(int, Frame) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator: Constructor to create a customizable Hermite interpolator for every spacecraft state field.
FieldSpacecraftStateInterpolator(int, Frame, Frame) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator: Constructor to create a customizable Hermite interpolator for every spacecraft state field.
FieldSpacecraftStateInterpolator(Frame) - Constructor for class org.orekit.propagation.FieldSpacecraftStateInterpolator: Simplest constructor to create a default Hermite interpolator for every spacecraft state field.
FieldStateCovariance<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation: This class is the representation of a covariance matrix at a given date.
FieldStateCovariance(FieldMatrix<T>, FieldAbsoluteDate<T>, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.FieldStateCovariance: Constructor.
FieldStateCovariance(FieldMatrix<T>, FieldAbsoluteDate<T>, LOF) - Constructor for class org.orekit.propagation.FieldStateCovariance: Constructor.
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, PositionAngleType, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.FieldStateMapper: Simple constructor.
FieldStaticTransform<T extends CalculusFieldElement<T>> - Interface in org.orekit.frames: A transform that only includes translation and rotation.
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<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: Empty constructor.
FieldStopOnEvent<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: Empty constructor.
FieldStopOnIncreasing<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: Empty constructor.
FieldTimeDerivativesEquations<T extends CalculusFieldElement<T>> - Interface in org.orekit.propagation.numerical: Interface summing up the contribution of several forces into orbit and mass derivatives.
FieldTimeInterpolator<T extends FieldTimeStamped<KK>,KK extends CalculusFieldElement<KK>> - Interface in org.orekit.time: This interface represents objects that can interpolate a time stamped value with respect to time.
FieldTimeShiftable<T extends FieldTimeShiftable<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.
FieldTimeStampedCache<T extends FieldTimeStamped<KK>,KK extends CalculusFieldElement<KK>> - Interface in org.orekit.utils: Interface for a data structure that can provide concurrent access to FieldTimeStamped data surrounding a given date.
FieldTimeStampedPair<F extends FieldTimeStamped<KK>,S extends FieldTimeStamped<KK>,KK extends CalculusFieldElement<KK>> - Class in org.orekit.time: Pair of time stamped values being defined at the same date.
FieldTimeStampedPair(F, S) - Constructor for class org.orekit.time.FieldTimeStampedPair: Constructor.
FieldTimeStampedPair(F, S, double) - Constructor for class org.orekit.time.FieldTimeStampedPair: Constructor.
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(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.
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.
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, Frame, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Protected constructor for derived classes.
FieldTLEPropagator(FieldTLE<T>, AttitudeProvider, T, T[]) - Constructor for class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Protected constructor for derived classes.
FieldTrackingCoordinates<T extends CalculusFieldElement<T>> - Class in org.orekit.utils: Container for azimut/elevation/range coordinates as seen from a ground point.
FieldTrackingCoordinates(Field<T>, TrackingCoordinates) - Constructor for class org.orekit.utils.FieldTrackingCoordinates: Build a new instance from a TrackingCoordinates.
FieldTrackingCoordinates(T, T, T) - Constructor for class org.orekit.utils.FieldTrackingCoordinates: Simple constructor.
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>, FieldRotation<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a rotation transform.
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>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a translation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldRotation<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a combined translation and 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>, FieldTransform<T>, FieldTransform<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a transform by combining two existing ones.
FieldTransform(FieldAbsoluteDate<T>, FieldAngularCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a translation transform, with its first time derivative.
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.
FieldTroposphericDelay<T extends CalculusFieldElement<T>> - Class in org.orekit.models.earth.troposphere: Container for tropospheric delay.
FieldTroposphericDelay(T, T, T, T) - Constructor for class org.orekit.models.earth.troposphere.FieldTroposphericDelay: Simple constructor.
FieldUnboundedCartesianEnergy<T extends CalculusFieldElement<T>> - Class in org.orekit.control.indirect.adjoint.cost: Class for unbounded energy cost with Cartesian coordinates.
FieldUnboundedCartesianEnergy(String, T) - Constructor for class org.orekit.control.indirect.adjoint.cost.FieldUnboundedCartesianEnergy: Constructor.
FieldUnboundedCartesianEnergy(String, T, FieldEventDetectionSettings<T>) - Constructor for class org.orekit.control.indirect.adjoint.cost.FieldUnboundedCartesianEnergy: Constructor.
FieldUnboundedCartesianEnergyNeglectingMass<T extends CalculusFieldElement<T>> - Class in org.orekit.control.indirect.adjoint.cost: Class for unbounded energy cost with Cartesian coordinates neglecting the mass consumption.
FieldUnboundedCartesianEnergyNeglectingMass(String, Field<T>) - Constructor for class org.orekit.control.indirect.adjoint.cost.FieldUnboundedCartesianEnergyNeglectingMass: Constructor.
FieldViennaACoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.models.earth.troposphere: Container for the ViennaOne and ViennaThree coefficients a_h and a_w.
FieldViennaACoefficients(T, T) - Constructor for class org.orekit.models.earth.troposphere.FieldViennaACoefficients: 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(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.
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.
fillHistory(IERSConventions.NutationCorrectionConverter, SortedSet<EOPEntry>) - Method in interface org.orekit.frames.EopHistoryLoader: Load celestial body.
filter(boolean) - Method in class org.orekit.utils.ParameterDriversList: Filter parameters to keep only one type of selection status.
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.TruncatingFilter: Filter the data source.
filter(DataSource) - Method in class org.orekit.data.UnixCompressFilter: Filter the data source.
filter(DataSource) - Method in class org.orekit.files.rinex.HatanakaCompressFilter: Filter the data source.
filter(DataSource) - Method in class org.orekit.files.sp3.NsgfV00Filter: 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_SMOOTHER - org.orekit.files.ccsds.definitions.AdMethodType: Method smoothing noisy processes.
filterData(ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencyHatchFilter: This method filters the provided data given the state of the filter.
filterData(ObservationData, ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter: This method filters the provided data given the state of the filter.
filterDataSet(List<ObservationDataSet>, SatelliteSystem, int, ObservationType) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother: Applies a Single Frequency Hatch filter to a list of ObservationDataSet.
filterDataSet(List<ObservationDataSet>, SatelliteSystem, int, ObservationType, ObservationType) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother: Applies a Dual Frequency Hatch filter to a list of ObservationDataSet.
filterLine(int, String) - Method in class org.orekit.data.LineOrientedFilteringReader: Filter one line.
filterRelevant(ObservedMeasurement<?>, SpacecraftState[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil: Filter relevant states for a measurement.
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.acm.AcmParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Finalize data after parsing.
finalizeData() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Finalize data after parsing.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.KalmanModel: Finalize estimation.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Finalize estimation.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess: Finalize estimation.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Finalize estimation.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel: Finalize estimation.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Finalize header after parsing.
finalizeHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Finalize header after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser: Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Finalize metadata after parsing.
finalizeMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser: Finalize metadata after parsing.
finalizeMetadata() - 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.
finalizeMetadata(ContextBinding) - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata: Finalize the metadata.
finalizeOperationsObservationGrid() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Finalize estimation operations on the observation grid.
finalizeOperationsObservationGrid() - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess: Finalize estimation operations on the observation grid.
finalizeOperationsObservationGrid() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Finalize estimation operations on the observation grid.
FIND_ROOT - org.orekit.errors.OrekitMessages: FIND_ROOT.
findByName(String) - Method in class org.orekit.utils.ParameterDriversList: Find a delegating driver by name.
findByName(List<ParameterDriver>, String) - Static method in interface org.orekit.utils.ParameterDriversProvider: Find if a parameter driver with a given name already exists in a list of parameter drivers.
findDelegatingSpanNameBySpanName(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(SatInSystem) - Method in class org.orekit.gnss.antenna.AntexLoader: Find the time map for a specific satellite antenna.
finish(List<SpacecraftState>) - Method in interface org.orekit.propagation.sampling.MultiSatFixedStepHandler: Finalize propagation.
finish(List<SpacecraftState>) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler: Finalize propagation.
finish(List<SpacecraftState>) - Method in class org.orekit.propagation.sampling.MultisatStepNormalizer: Finalize propagation.
finish(FieldSpacecraftState<T>) - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver: This method finalizes the event detector's job.
finish(FieldSpacecraftState<T>) - Method in interface org.orekit.forces.maneuvers.FieldImpulseProvider: Method called at end of propagation.
finish(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldBooleanDetector
finish(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldDetectorModifier: This method finalizes the event detector's job.
finish(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector: This method finalizes the event detector's job.
finish(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventSlopeFilter: This method finalizes the event detector's job.
finish(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventState: This method finalizes the event detector's job.
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(FieldSpacecraftState<T>, FieldEventDetector<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler: This method finalize event handler at the end of a propagation.
finish(FieldSpacecraftState<T>, FieldEventDetector<T>) - Method in class org.orekit.propagation.events.handlers.FieldRecallLastOccurrence: This method finalize event handler at the end of a propagation.
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.ocm.StreamingOcmWriter.BlockWriter: 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(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: This method finalizes the event detector's job.
finish(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.ImpulseProvider: Method called at end of propagation.
finish(SpacecraftState) - Method in class org.orekit.propagation.events.BooleanDetector
finish(SpacecraftState) - Method in interface org.orekit.propagation.events.DetectorModifier: This method finalizes the event detector's job.
finish(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector: This method finalizes the event detector's job.
finish(SpacecraftState) - Method in class org.orekit.propagation.events.EventSlopeFilter: This method finalizes the event detector's job.
finish(SpacecraftState) - Method in class org.orekit.propagation.events.EventState: This method finalizes the event detector's job.
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.
finish(SpacecraftState, EventDetector) - Method in interface org.orekit.propagation.events.handlers.EventHandler: This method finalizes the event handler's job.
finish(SpacecraftState, EventDetector) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
finish(SpacecraftState, EventDetector) - Method in class org.orekit.propagation.events.handlers.RecallLastOccurrence: This method finalizes the event handler's job.
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.
FIRST_VECTOR_ONLY - org.orekit.files.iirv.IIRVMessage.IncludeMessageMetadata: Include message metadata fields in the first line of the first vector (when SequenceNumberTerm is 0), and omit for all other vectors in a given IIRV message file.
firstLineParser() - Method in class org.orekit.files.sinex.AbstractSinexParser: Get parser for the first line.
firstLineParser() - Method in class org.orekit.files.sinex.SinexBiasParser: Get parser for the first line.
firstLineParser() - Method in class org.orekit.files.sinex.SinexParser: Get parser for the first line.
fit() - Method in class org.orekit.utils.SecularAndHarmonic: Fit parameters.
fit(EOPHistory) - Method in class org.orekit.frames.EOPFitter: Fit raw history.
fit(EOPHistory, ToDoubleFunction<EOPEntry>) - Method in class org.orekit.frames.SingleParameterFitter: Perform secular and harmonic fitting.
FIT - org.orekit.files.sp3.SP3OrbitType: fitted.
FIXED - org.orekit.files.stk.STKEphemerisFile.STKCoordinateSystem: Fixed frame.
FIXED_F10P7 - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Fixed (time invariant) value of the Solar Flux Unit daily proxy F10.7.
FIXED_F10P7_MEAN - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Fixed (time invariant) value of the Solar Flux Unit 81-day running center-average proxy F10.7.
FIXED_GEOMAG_AP - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Fixed (time invariant) value of the planetary 3-hour-range geomagnetic index aₚ.
FIXED_GEOMAG_DST - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Fixed (time invariant) value of the planetary 1-hour-range geomagnetic index Dst.
FIXED_GEOMAG_KP - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Fixed (time invariant) value of the planetary 3-hour-range geomagnetic index Kₚ.
FIXED_M10P7 - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Fixed (time invariant) value of the Solar Flux daily proxy M10.7.
FIXED_M10P7_MEAN - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Fixed (time invariant) value of the Solar Flux 81-day running center-average proxy M10.7.
FIXED_S10P7 - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Fixed (time invariant) value of the Solar Flux daily proxy S10.7.
FIXED_S10P7_MEAN - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Fixed (time invariant) value of the Solar Flux 81-day running center-average proxy S10.7.
FIXED_Y10P7 - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Fixed (time invariant) value of the Solar Flux daily proxy Y10.7.
FIXED_Y10P7_MEAN - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey: Fixed (time invariant) value of the Solar Flux 81-day running center-average proxy Y10.7.
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.
FixedPanel - Class in org.orekit.forces: Class representing one panel of a satellite, fixed with respect to satellite body.
FixedPanel(Vector3D, double, boolean, double, double, double, double) - Constructor for class org.orekit.forces.FixedPanel: Simple constructor.
FixedPointConverter - Class in org.orekit.propagation.conversion.osc2mean: Class enabling conversion from osculating to mean orbit for a given theory using a fixed-point algorithm.
FixedPointConverter() - Constructor for class org.orekit.propagation.conversion.osc2mean.FixedPointConverter: Default constructor.
FixedPointConverter(double, int, double) - Constructor for class org.orekit.propagation.conversion.osc2mean.FixedPointConverter: Constructor.
FixedPointConverter(MeanTheory) - Constructor for class org.orekit.propagation.conversion.osc2mean.FixedPointConverter: Constructor.
FixedPointConverter(MeanTheory, double, int, double) - Constructor for class org.orekit.propagation.conversion.osc2mean.FixedPointConverter: Constructor.
FixedPointOsculatingToAveragedConverter<T extends AveragedOrbitalState> - Class in org.orekit.propagation.conversion.averaging.converters: Abstract class for osculating-to-averaged converters based on a fixed-point algorithm.
FixedPointOsculatingToAveragedConverter(double, int) - Constructor for class org.orekit.propagation.conversion.averaging.converters.FixedPointOsculatingToAveragedConverter: Protected constructor.
FixedPointTleGenerationAlgorithm - Class in org.orekit.propagation.analytical.tle.generation: Fixed Point method to reverse SGP4 and SDP4 propagation algorithm and generate a usable TLE from a spacecraft state.
FixedPointTleGenerationAlgorithm() - Constructor for class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm: Default constructor.
FixedPointTleGenerationAlgorithm(double, int, double) - Constructor for class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm: Constructor.
FixedPointTleGenerationAlgorithm(double, int, double, TimeScale, Frame) - Constructor for class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm: 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.
FixedTimeBoundaryOrbits - Class in org.orekit.control.indirect.shooting.boundary: Defines two-point boundary values for indirect shooting methods with Cartesian coordinates.
FixedTimeBoundaryOrbits(Orbit, Orbit) - Constructor for class org.orekit.control.indirect.shooting.boundary.FixedTimeBoundaryOrbits: Constructor.
FixedTimeCartesianBoundaryStates - Class in org.orekit.control.indirect.shooting.boundary: Defines two-point boundary values for indirect shooting methods with Cartesian coordinates.
FixedTimeCartesianBoundaryStates(AbsolutePVCoordinates, AbsolutePVCoordinates) - Constructor for class org.orekit.control.indirect.shooting.boundary.FixedTimeCartesianBoundaryStates: 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.
FootprintOverlapDetector(EventDetectionSettings, EventHandler, FieldOfView, OneAxisEllipsoid, SphericalPolygonsSet, double, List<FootprintOverlapDetector.SamplingPoint>) - Constructor for class org.orekit.propagation.events.FootprintOverlapDetector: Protected constructor with full parameters.
FORCED - Static variable in class org.orekit.files.iirv.terms.VectorTypeTerm: Forced VectorType.
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.
ForceModelModifier - Interface in org.orekit.forces: Interface to wrap another force model.
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: Deprecated.
As of 13.0, because Static method does not utilize inheritance benefits from Formatter. Use AccurateFormatter.toString(double) instead.
format(int, int, int, int, int, double) - Static method in class org.orekit.utils.AccurateFormatter: Deprecated.
As of 13.0, because static method does not utilize inheritance benefits from Formatter and does not check format standards of date time. Use AccurateFormatter.toString(int, int, int, int, int, double) instead.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.Acm: Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.Aem: Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.Apm: Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.cdm.Cdm: Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm: Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.Oem: Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.Omm: Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Key for format version.
FORMAT_VERSION_KEY - Static variable in class org.orekit.files.ccsds.ndm.tdm.Tdm: Key for format version.
formatIntegerOrNaN(int, int) - Static method in class org.orekit.files.ilrs.CRD: Format the integer value as a string, or the string VALUE_NOT_AVAILABLE.
Formatter - Interface in org.orekit.utils: Formatter used to produce strings from data.
formatUtcOffset() - Method in class org.orekit.time.TimeComponents: Get the UTC offset as a string in ISO8601 format.
formFieldRelativePosition(FieldAbsoluteDate<T>, T[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm: Form relative position vector w.r.t. body.
formRelativePosition(AbsoluteDate, double[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm: Form relative position vector w.r.t. body.
forwardSignalTimeOfFlight(TimeStampedFieldPVCoordinates<T>, FieldVector3D<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.estimation.measurements.TDOA: Compute propagation delay on a link leg (typically downlink or uplink).This differs from signalTimeOfFlight through advancing rather than delaying the emitter.
forwardSignalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate) - Static method in class org.orekit.estimation.measurements.TDOA: Compute propagation delay on a link leg (typically downlink or uplink).
FOSTER_1992 - org.orekit.files.ccsds.definitions.PocMethodType: Foster 1992 method.
Frame - Class in org.orekit.frames: Tridimensional references frames class.
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, TransformProvider, String, boolean) - Constructor for class org.orekit.frames.Frame: Build a frame from its transform with respect to its parent.
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, Transform, String, boolean) - Constructor for class org.orekit.frames.Frame: Build a frame from its transform with respect to its parent.
FRAME_ALREADY_ATTACHED - org.orekit.errors.OrekitMessages: FRAME_ALREADY_ATTACHED.
FRAME_ANCESTOR_OF_BOTH_FRAMES - org.orekit.errors.OrekitMessages: FRAME_ANCESTOR_OF_BOTH_FRAMES.
FRAME_ANCESTOR_OF_NEITHER_FRAME - org.orekit.errors.OrekitMessages: FRAME_ANCESTOR_OF_NEITHER_FRAME.
FRAME_NO_NTH_ANCESTOR - org.orekit.errors.OrekitMessages: FRAME_NO_NTH_ANCESTOR.
FRAME_NOT_ALLOWED - org.orekit.errors.OrekitMessages: FRAME_NOT_ALLOWED.
FRAME_NOT_ATTACHED - org.orekit.errors.OrekitMessages: FRAME_NOT_ATTACHED.
FrameAdapter - Class in org.orekit.utils: Adapter from Frame to ExtendedPositionProvider.
FrameAdapter(Frame) - Constructor for class org.orekit.utils.FrameAdapter: Simple constructor.
FrameAlignedProvider - Class in org.orekit.attitudes: This class handles an attitude provider aligned with a frame or a fixed offset to it.
FrameAlignedProvider(Rotation) - Constructor for class org.orekit.attitudes.FrameAlignedProvider: Creates new instance.
FrameAlignedProvider(Rotation, Frame) - Constructor for class org.orekit.attitudes.FrameAlignedProvider: Creates new instance with a fixed attitude in the given frame.
FrameAlignedProvider(Frame) - Constructor for class org.orekit.attitudes.FrameAlignedProvider: Creates new instance aligned with the given frame.
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.
frameName(Frame) - Static method in class org.orekit.gnss.IGSUtils: Guess a frame name.
Frames - Interface in org.orekit.frames: A collection of commonly used Frames.
FRAMES_MISMATCH - org.orekit.errors.OrekitMessages: FRAMES_MISMATCH.
FramesFactory - Class in org.orekit.frames: Factory for predefined reference frames.
FREE_FLIGHT - Static variable in class org.orekit.files.iirv.terms.VectorTypeTerm: Free flight (routine on-orbit) VectorType.
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.
FREQ_OFFSET - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey: Frequency offset entry.
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.
fromIIRVTerms(IIRVVectorTerm<?>...) - Static method in class org.orekit.files.iirv.terms.CheckSumTerm: Constructs an IIRV checksum from a series of IIRVTerm instances.
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.
fromSI(T) - Method in class org.orekit.utils.units.Unit: Convert a value from SI units.
FrRangeMeasurement(AbsoluteDate, double, int, String, int, int, int, int, int) - Constructor for class org.orekit.files.ilrs.CRD.FrRangeMeasurement: Constructor.
FULL - org.orekit.files.ccsds.ndm.odm.ocm.Ordering: Full symmetric Matrix.
FULL_RATE - org.orekit.files.ilrs.CRDHeader.DataType: Full rate.
FUNCTION_NOT_IMPLEMENTED - org.orekit.errors.OrekitMessages: FUNCTION_NOT_IMPLEMENTED.
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.
FunctionalDetector(EventDetectionSettings, EventHandler, ToDoubleFunction<SpacecraftState>) - Constructor for class org.orekit.propagation.events.FunctionalDetector: Private constructor.
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(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.FieldBetaAngleDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldBooleanDetector
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldCylindricalShadowEclipseDetector: 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 interface org.orekit.propagation.events.FieldDetectorModifier: 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 class org.orekit.propagation.events.FieldElevationExtremumDetector: Compute the value of the detection 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.FieldEventEnablingPredicateFilter: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventShifter: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventSlopeFilter: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldExtremumApproachDetector: The g is positive when the primary object is getting further away from the secondary object and is negative when it is getting closer to it.
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.FieldLatitudeRangeCrossingDetector: Compute the value of the detection function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldLongitudeCrossingDetector: Compute the value of the detection function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector: Compute the value of the detection function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNegateDetector
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector: 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(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldRelativeDistanceDetector: The g is positive when the relative distance is larger or equal than the threshold, non-positive otherwise.
g(SpacecraftState) - Method in class org.orekit.attitudes.AttitudesSequence.Switch: 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.BetaAngleDetector: 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.CylindricalShadowEclipseDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.DateDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in interface org.orekit.propagation.events.DetectorModifier: 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(SpacecraftState) - Method in class org.orekit.propagation.events.ExtremumApproachDetector: The g is positive when the primary object is getting further away from the secondary object and is negative when it is getting closer to it.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FieldOfViewDetector: 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.LatitudeRangeCrossingDetector: 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.LongitudeRangeCrossingDetector: 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.
g(SpacecraftState) - Method in class org.orekit.propagation.events.RelativeDistanceDetector: The g is positive when the relative distance is larger or equal than the threshold, non-positive otherwise.
G0_STANDARD_GRAVITY - Static variable in interface org.orekit.utils.Constants: Standard gravity constant, used in maneuvers definition: 9.80665 m/s².
G01 - org.orekit.gnss.PredefinedGnssSignal: GPS L1 (1575.42 MHz).
G02 - org.orekit.gnss.PredefinedGnssSignal: GPS L2 (1227.6 MHz).
G05 - org.orekit.gnss.PredefinedGnssSignal: GPS L5 (1176.45 MHz).
GAGAN - org.orekit.files.rinex.navigation.SbasId: GPS Aided Geo Augmented Navigation.
GAL - org.orekit.files.rinex.navigation.IonosphericCorrectionType: Galileo.
GAL - org.orekit.files.rinex.navigation.UtcId: UTCGAL.
GAL - org.orekit.gnss.metric.ntrip.NavigationSystem: Galileo.
GAL - org.orekit.gnss.ObservationTimeScale: Galileo time scale.
Galileo - Class in org.orekit.gnss.attitude: Attitude providers for Galileo navigation satellites.
Galileo(double, AbsoluteDate, AbsoluteDate, ExtendedPositionProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Galileo: Simple constructor.
GALILEO - org.orekit.files.sp3.SP3FileType: Galileo only file.
GALILEO - org.orekit.gnss.SatelliteSystem: Galileo system.
GALILEO - org.orekit.gnss.TimeSystem: GALILEO.
GALILEO - org.orekit.time.GNSSDate.GNSSDateType: Galileo.
GALILEO_0A - org.orekit.gnss.antenna.SatelliteType: Galileo In-Orbit Validation Element A (GIOVE-A).
GALILEO_0B - org.orekit.gnss.antenna.SatelliteType: Galileo In-Orbit Validation Element B (GIOVE-B).
GALILEO_1 - org.orekit.gnss.antenna.SatelliteType: Galileo IOV : GSAT 0101-0104.
GALILEO_2 - org.orekit.gnss.antenna.SatelliteType: Galileo FOC : GSAT 0201-0222.
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(FieldGalileoAlmanac<T>) - Constructor for class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac: Constructor from field instance.
GalileoAlmanac(TimeScales, SatelliteSystem) - 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(FieldGalileoNavigationMessage<T>) - Constructor for class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Constructor from field instance.
GalileoNavigationMessage(TimeScales, SatelliteSystem) - 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.
GAQD - Static variable in class org.orekit.files.iirv.terms.OriginatorRoutingIndicatorTerm: GAQD OriginatorRoutingIndicator.
GatheringSubscriber - Class in org.orekit.estimation.measurements.generation: Subscriber that gather all generated measurements in a sorted set.
GatheringSubscriber() - Constructor for class org.orekit.estimation.measurements.generation.GatheringSubscriber: Simple constructor.
GCQU - Static variable in class org.orekit.files.iirv.terms.OriginatorRoutingIndicatorTerm: GCQU OriginatorRoutingIndicator.
GCRF - org.orekit.files.ccsds.definitions.CelestialBodyFrame: Geocentric Celestial Reference Frame.
GCRF - org.orekit.frames.Predefined: GCRF frame.
GDOP - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey: Generalize Dilution Of Precision.
GE_H - org.orekit.models.earth.weather.SeasonalModelType: Hydrostatic East gradient coefficient model.
GE_W - org.orekit.models.earth.weather.SeasonalModelType: Wet East gradient coefficient model.
GEGOUT - org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients: Coefficients computed by Pascal Gégout, CNRS / UMR5563 (GET).
generate(Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler: Generate a sequence of measurements.
generate(Map<ObservableSatellite, OrekitStepInterpolator>) - Method in interface org.orekit.estimation.measurements.generation.Scheduler: Generate a sequence of measurements.
generate(FieldSpacecraftState<T>, FieldTLE<T>) - Method in class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm: Generate a TLE from a given spacecraft state and a template TLE.
generate(FieldSpacecraftState<T>, FieldTLE<T>) - Method in class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm: Generate a TLE from a given spacecraft state and a template TLE.
generate(FieldSpacecraftState<T>, FieldTLE<T>) - Method in interface org.orekit.propagation.analytical.tle.generation.TleGenerationAlgorithm: Generate a TLE from a given spacecraft state and a template TLE.
generate(SpacecraftState, TLE) - Method in class org.orekit.propagation.analytical.tle.generation.FixedPointTleGenerationAlgorithm: Generate a TLE from a given spacecraft state and a template TLE.
generate(SpacecraftState, TLE) - Method in class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm: Generate a TLE from a given spacecraft state and a template TLE.
generate(SpacecraftState, TLE) - Method in interface org.orekit.propagation.analytical.tle.generation.TleGenerationAlgorithm: Generate a TLE from a given spacecraft state and a template TLE.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.Generator: Generate 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 class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.SolarActivityGenerator: 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.
generateData(boolean, boolean, RotationOrder, boolean, TimeStampedAngularCoordinates) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType: Generate the attitude data corresponding to the attitude type.
generateDataFromEarliestToLatestDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.SolarActivityGenerator: Generate a list of parameters between earliest and latest dates.
GeneratedMeasurementSubscriber - Interface in org.orekit.estimation.measurements.generation: Interface for subscribing to generated measurements events.
generateException(Exception) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Generate a parse exception for this entry.
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.
generateKeplerianOrbit(Frame) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: 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.
generateTesseralPolynomials(int, int, int, int, int, int, PolynomialFunction[][], PolynomialFunction[][]) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities: Generate the polynomials needed in the linear transformation.
generateThirdBodyPolynomials(int, int, int, int, PolynomialFunction[][], PolynomialFunction[][]) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities: Generate the polynomials needed in the linear transformation.
generateTLE() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm: Generate TLE from OMM file.
generateZonalPolynomials(int, int, int, int, int, PolynomialFunction[][], PolynomialFunction[][]) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities: Generate the polynomials needed in the linear transformation.
Generator - Class in org.orekit.estimation.measurements.generation: Main generator for observed measurements.
Generator - Interface in org.orekit.files.ccsds.utils.generation: Generation interface for CCSDS messages.
Generator() - Constructor for class org.orekit.estimation.measurements.generation.Generator: Build a generator with no sequences generator.
GenericGNSS - Class in org.orekit.gnss.attitude: Attitude providers for navigation satellites for which no specialized model is known.
GenericGNSS(AbsoluteDate, AbsoluteDate, ExtendedPositionProvider, 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.
GenericTimeStampedCache(int, int, double, double, TimeStampedGenerator<T>, double) - Constructor for class org.orekit.utils.GenericTimeStampedCache: Simple constructor with overriding minimum step.
GEO - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCategory: Geosynchronous Earth Orbit, with i > 3°, 35586 < hp < 35986 km, 35586 < ha < 35986 km.
GEO - org.orekit.propagation.analytical.gnss.data.BeidouSatelliteType: Geostationary satellite.
GEOCENTRIC_MEAN_B1950 - Static variable in class org.orekit.files.iirv.terms.CoordinateSystemTerm: Geocentric mean of 1950.0 (B1950.0) CoordinateSystemTerm.
GEOCENTRIC_MEAN_OF_J2000 - Static variable in class org.orekit.files.iirv.terms.CoordinateSystemTerm: Geocentric mean of 2000.0 (J2000.0) CoordinateSystemTerm.
GEOCENTRIC_TRUE_OF_DATE_ROTATING - Static variable in class org.orekit.files.iirv.terms.CoordinateSystemTerm: Geocentric True-of-Date Rotating (GTOD) CoordinateSystemTerm.
GEODETIC - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType: Geodetic elements (λ, ΦGD, β, A, h, vre).
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.
geodeticToIsometricLatitude(double) - Method in class org.orekit.bodies.OneAxisEllipsoid: Compute the isometric latitude corresponding to the provided latitude.
geodeticToIsometricLatitude(T) - Method in class org.orekit.bodies.OneAxisEllipsoid: Compute the isometric latitude corresponding to the provided latitude.
GeographicZoneDetector - Class in org.orekit.propagation.events: Detector for entry/exit of a zone defined by geographic boundaries.
GeographicZoneDetector(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector: Build a detector.
GeographicZoneDetector(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector: Build a new detector.
GeographicZoneDetector(EventDetectionSettings, EventHandler, BodyShape, SphericalPolygonsSet, EnclosingBall<Sphere2D, S2Point>, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector: Protected constructor with full parameters.
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: Empty constructor.
GeoMagneticModelParser - Class in org.orekit.models.earth: Loads geomagnetic field models from a given input stream.
GeoMagneticModelParser() - Constructor for class org.orekit.models.earth.GeoMagneticModelParser: Empty constructor.
GEOMETRY_FREE - org.orekit.estimation.measurements.gnss.CombinationType: Geometry-free combination.
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(int) - Method in class org.orekit.files.iirv.IIRVMessage: Gets the IIRVVector located at a given index in the message.
get(String) - Method in class org.orekit.utils.DataDictionary: Get the value corresponding to a key.
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(String) - Method in class org.orekit.utils.FieldDataDictionary: Get the value corresponding to a key.
get(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap: Get the entry valid at a specified date.
get(FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap: 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.attitudes.FieldInertiaAxis: Get the inertia axis.
getA() - Method in class org.orekit.attitudes.InertiaAxis: Get the inertia axis.
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.bodies.FieldEllipse: Get the semi major 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.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.semianalytical.dsst.forces.DSSTGravityContext: Getter for the a.
getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext: 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.FieldDSSTGravityContext: A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Get A = sqrt(μ * a).
getA(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ConstantViennaAProvider: Get coefficients array for VMF mapping function.
getA(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.ViennaAProvider: Get coefficients array for VMF mapping function.
getA(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature: Get coefficients array for VMF mapping function.
getA(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ConstantViennaAProvider: Get coefficients array for VMF mapping function.
getA(GeodeticPoint, AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.ViennaAProvider: Get coefficients array for VMF mapping function.
getA(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature: Get coefficients array for VMF mapping function.
getA0() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage: Get the constant term of the offset.
getA0() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get A0 field.
getA1() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage: Get the linear term of the offset.
getA1() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get A₁ field.
getA2() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage: Get the quadratic term of the offset.
getA4() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext: Get the semi major axis to the power 4.
getA4() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext: Get the semi major axis to the power 4.
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.
getAbsoluteDate(int) - Method in class org.orekit.files.iirv.IIRVVector: Creates an AbsoluteDate instance (in UTC), with time components given by the VectorEpochTerm, and date components from the DayOfYearTerm / inputted year.
getAbsorption() - Method in class org.orekit.forces.Panel: Get radiation pressure absorption coefficient.
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.
getAbsPVAInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator: Get absolute position-velocity-acceleration interpolator.
getAbsPVAInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator: Get absolute position-velocity-acceleration interpolator.
getAcceleration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: Get acceleration.
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.time.ClockOffset: Get acceleration.
getAcceleration() - Method in class org.orekit.time.FieldClockOffset: Get acceleration.
getAcceleration() - Method in class org.orekit.utils.FieldPVCoordinates: Gets the acceleration.
getAcceleration() - Method in class org.orekit.utils.PVCoordinates: Gets the acceleration.
getAcceleration(Transform, double[]) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm: Evaluates the inertial acceleration vector.
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(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(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(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(AbsoluteDate, double[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm: Compute the acceleration vector.
getAcceleration(AbsoluteDate, double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm: Compute the acceleration vector.
getAcceleration(AbsoluteDate, double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term: Compute the acceleration vector.
getAcceleration(AbsoluteDate, double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointKeplerianTerm: Compute the acceleration vector.
getAcceleration(AbsoluteDate, double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointSingleBodyTerm: Compute the acceleration vector.
getAcceleration(AbsoluteDate, double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointThirdBodyTerm: Compute the acceleration vector.
getAccelerationDirection(FieldSpacecraftState<T>) - Method in class org.orekit.forces.empirical.AbstractParametricAcceleration: Computes the acceleration's direction in the propagation frame.
getAccelerationDirection(SpacecraftState) - Method in class org.orekit.forces.empirical.AbstractParametricAcceleration: Computes the acceleration's direction in the propagation frame.
getAccelerationDirectionSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: Get one σ angular off-nominal acceleration direction.
getAccelerationInterpolation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: Get interpolation mode between current and next acceleration line.
getAccelerationMagnitudeSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: 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() - Method in interface org.orekit.gnss.metric.messages.common.AccuracyProvider: Get the accuracy of the ephemeris data from an accuracy index.
getAccuracy() - Method in class org.orekit.gnss.metric.messages.common.GlonassUserRangeAccuracy: Get the accuracy of the ephemeris data from an accuracy index.
getAccuracy() - Method in class org.orekit.gnss.metric.messages.common.SignalInSpaceAccuracy: Get the accuracy of the ephemeris data from an accuracy index.
getAccuracy() - Method in class org.orekit.gnss.metric.messages.common.UserRangeAccuracy: Get the accuracy of the ephemeris data from an accuracy index.
getAccuracy(String) - Method in class org.orekit.files.sp3.SP3Header: Get the formal accuracy.
getAccuracyProvider() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData: Get the accuracy provider of the ephemeris message.
getAcmDataElements() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata: Get the list of elements of information data blocks included in this 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.
getActiveProvider(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel: Getter for active provider at input date.
getActualOdSpan() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters: Get the actual OD time based on the observations available and the RECOMMENDED_OD_SPAN.
getActualOdSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get actual time span used for the OD of the object.
getActuatorUsed() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver: Get the actuator used.
getAdaptableInterval(TopocentricFrame, double, double, double) - Static method in class org.orekit.propagation.events.intervals.ElevationDetectionAdaptableIntervalFactory: Method providing a candidate AdaptableInterval for arbitrary elevation detection with forward propagation.
getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the adapted propagator.
getAdditionalCovMetadataBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData: Get the additional covariance metadata logical block.
getAdditionalData(String) - Method in class org.orekit.propagation.FieldSpacecraftState: Get an additional data.
getAdditionalData(String) - Method in class org.orekit.propagation.SpacecraftState: Get an additional data.
getAdditionalData(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.gnss.FieldClockCorrectionsProvider: Get the additional data.
getAdditionalData(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractStateModifier: Get the additional data.
getAdditionalData(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalDataProvider: Get the additional data.
getAdditionalData(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.Duration: Get the additional data.
getAdditionalData(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate: Get the additional data.
getAdditionalData(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate: Get the additional data.
getAdditionalData(SpacecraftState) - Method in class org.orekit.propagation.AbstractStateModifier: Get the additional data.
getAdditionalData(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalDataProvider: Get the additional data.
getAdditionalData(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester: Get the additional data.
getAdditionalData(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider: Get the additional data.
getAdditionalData(SpacecraftState) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider: Get the additional data.
getAdditionalDataProviders() - Method in class org.orekit.propagation.AbstractPropagator: Get an unmodifiable list of providers for additional data.
getAdditionalDataProviders() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get an unmodifiable list of providers for additional data.
getAdditionalDataProviders() - Method in interface org.orekit.propagation.FieldPropagator: Get an unmodifiable list of providers for additional data.
getAdditionalDataProviders() - Method in interface org.orekit.propagation.Propagator: Get an unmodifiable list of providers for additional data.
getAdditionalDataValues() - Method in class org.orekit.propagation.FieldSpacecraftState: Get an unmodifiable map of additional states.
getAdditionalDataValues() - Method in class org.orekit.propagation.SpacecraftState: Get an unmodifiable map of additional data.
getAdditionalDerivatives() - Method in class org.orekit.propagation.integration.CombinedDerivatives: Get the derivatives related to the additional state.
getAdditionalDerivatives() - Method in class org.orekit.propagation.integration.FieldCombinedDerivatives: Get the derivatives related to the additional state.
getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the list of additional equations.
getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get an unmodifiable list of providers for additional derivatives.
getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get an unmodifiable list of providers for additional derivatives.
getAdditionalParametersBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData: Get the additional parameters logical block.
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.
getAdditionalStateInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator: Get additional state interpolator.
getAdditionalStateInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator: Get additional state interpolator.
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.
getAdjointDimension() - Method in class org.orekit.control.indirect.adjoint.cost.AbstractCartesianCost: Getter for adjoint vector dimension.
getAdjointDimension() - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost: Getter for adjoint vector dimension.
getAdjointDimension() - Method in class org.orekit.control.indirect.adjoint.cost.FieldAbstractCartesianCost: Getter for adjoint vector dimension.
getAdjointDimension() - Method in interface org.orekit.control.indirect.adjoint.cost.FieldCartesianCost: Getter for adjoint vector dimension.
getAdjointDimension() - Method in class org.orekit.control.indirect.adjoint.cost.FieldUnboundedCartesianEnergyNeglectingMass: Getter for adjoint vector dimension.
getAdjointDynamicsProvider() - Method in class org.orekit.control.indirect.shooting.propagation.ShootingPropagationSettings: Getter for adjoint dynamics provider.
getAdjointName() - Method in class org.orekit.control.indirect.adjoint.cost.AbstractCartesianCost: Getter for adjoint vector name.
getAdjointName() - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost: Getter for adjoint vector name.
getAdjointName() - Method in class org.orekit.control.indirect.adjoint.cost.FieldAbstractCartesianCost: Getter for adjoint vector name.
getAdjointName() - Method in interface org.orekit.control.indirect.adjoint.cost.FieldCartesianCost: Getter for adjoint vector name.
getAdjointName() - Method in class org.orekit.control.indirect.adjoint.cost.FieldUnboundedCartesianEnergyNeglectingMass: Getter for adjoint vector name.
getAdjointName() - Method in interface org.orekit.control.indirect.shooting.propagation.AdjointDynamicsProvider: Getter for adjoint vector name.
getAdjointName() - Method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProvider: Getter for adjoint vector name.
getAdjointVelocityNorm(double[]) - Method in class org.orekit.control.indirect.adjoint.cost.AbstractCartesianCost: Computes the Euclidean norm of the adjoint velocity vector.
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.
getAdmMsgLink() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the unique identifier of Attitude Data Message(s) that are linked (relevant) to this Conjunction 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.
getADot() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for the change rate in semi-major axis.
getADot() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Getter for the change rate in semi-major axis.
getADot() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for the change rate in semi-major axis.
getADot() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Getter for the change rate in semi-major axis.
getADot() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements: Getter for the change rate in semi-major axis.
getADot() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Getter for the change rate in semi-major axis.
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: Gets the Zeroth Order Clock Correction.
getAf0() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCommonGnssData: Gets the Zeroth Order Clock Correction.
getAf0() - Method in interface org.orekit.propagation.analytical.gnss.data.FieldGNSSClockElements: Gets the Zeroth Order Clock Correction.
getAf0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements: Gets the Zeroth Order Clock Correction.
getAF0() - Method in class org.orekit.gnss.rflink.gps.SubFrame1: Get af₀.
getAF0() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac: Get af₀.
getAf1() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Gets the First Order Clock Correction.
getAf1() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCommonGnssData: Gets the First Order Clock Correction.
getAf1() - Method in interface org.orekit.propagation.analytical.gnss.data.FieldGNSSClockElements: Gets the First Order Clock Correction.
getAf1() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements: Gets the First Order Clock Correction.
getAF1() - Method in class org.orekit.gnss.rflink.gps.SubFrame1: Get af₁.
getAF1() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac: Get af₁.
getAf2() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Gets the Second Order Clock Correction.
getAf2() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCommonGnssData: Gets the Second Order Clock Correction.
getAf2() - Method in interface org.orekit.propagation.analytical.gnss.data.FieldGNSSClockElements: Gets the Second Order Clock Correction.
getAf2() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements: Gets the Second Order Clock Correction.
getAF2() - Method in class org.orekit.gnss.rflink.gps.SubFrame1: Get af₂.
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.SP3Header: Returns the agency that prepared this SP3 file.
getAgencyName() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the agency name.
getAgencyName() - Method in class org.orekit.files.rinex.observation.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.
getAGoM() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Get the SGP4-XP solar radiation pressure-like coefficient Aγ/m.
getAh() - Method in class org.orekit.models.earth.troposphere.FieldViennaACoefficients: Get hydrostatic coefficient.
getAh() - Method in class org.orekit.models.earth.troposphere.ViennaACoefficients: Get hydrostatic coefficient.
getAi0() - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage: Get aᵢ₀.
getAi1() - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage: Get aᵢ₁.
getAi2() - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage: Get aᵢ₂.
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.
getAlert() - Method in class org.orekit.gnss.rflink.gps.SubFrame: Get alert flag.
getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector: Get the alignment angle (rad).
getAll() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache: Get all the data in this cache.
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.files.rinex.navigation.IonosphereBDGIMMessage: Get the α coefficients.
getAlpha() - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage: Get the α coefficients.
getAlpha() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader: Returns the alpha coefficients array.
getAlpha() - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickGalileo: Get effective ionisation level coefficients.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext: Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext: Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext: Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Get direction cosine α for central body.
getAlpha(PositionAngleType) - Method in class org.orekit.orbits.CircularOrbit: Get the latitude argument.
getAlpha(PositionAngleType) - Method in class org.orekit.orbits.FieldCircularOrbit: Get the latitude argument.
getAlpha0() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get α₀ field.
getAlpha1() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get α₁ field.
getAlpha2() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get α₂ field.
getAlpha3() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get α₃ field.
getAlpha4() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext: Get the equatorial radius of the central body to the power 4.
getAlpha4() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext: Get the equatorial radius of the central body to the power 4.
getAlphaDot(PositionAngleType) - Method in class org.orekit.orbits.CircularOrbit: Get the latitude argument derivative.
getAlphaDot(PositionAngleType) - 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.
getAltCovRefFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the value of ALT_COV_REF_FRAME as an Orekit Frame.
getAltCovType() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the flag indicating the type of alternate covariance information provided.
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.bodies.Loxodrome: Get the altitude above the reference body.
getAltitude() - Method in class org.orekit.models.earth.weather.FieldPressureTemperature: Get altitude at which weather parameters have been computed.
getAltitude() - Method in class org.orekit.models.earth.weather.PressureTemperature: Get altitude at which weather parameters have been computed.
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.
getAmbiguity(String, String, double) - Method in class org.orekit.estimation.measurements.gnss.AmbiguityCache: Get a cached driver for ambiguity.
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.
getAmplitude() - Method in class org.orekit.models.earth.displacement.PsdCorrection: Get amplitude.
getAnalysisCenterID() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the analysis center ID.
getAnalysisCenterName() - Method in class org.orekit.files.rinex.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.bodies.SexagesimalAngle: Get the corresponding angle in radians.
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.acm.AttitudeStateHistory: Get an unmodifiable list of attitude data lines.
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.
getAngularInterpolator() - Method in class org.orekit.attitudes.AttitudeInterpolator: Get time stamped angular coordinates interpolator.
getAngularInterpolator() - Method in class org.orekit.attitudes.FieldAttitudeInterpolator: Get time stamped angular coordinates interpolator.
getAngularVelocity() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get 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.
getAngularVelocityBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData: Get the angular velocity logical block.
getAngularWindUp() - Method in class org.orekit.estimation.measurements.gnss.AbstractWindUp: Get cached value of angular wind-up.
getAngVelX() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity: Get the angular velocity around X axis (rad/s).
getAngVelY() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity: Get the angular velocity around Y axis (rad/s).
getAngVelZ() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity: Get the angular velocity around Z axis (rad/s).
getAnomaly() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Get the orbit anomaly.
getAnomaly(PositionAngleType) - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the anomaly.
getAnomaly(PositionAngleType) - Method in class org.orekit.orbits.KeplerianOrbit: Get the anomaly.
getAnomalyDot(PositionAngleType) - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the anomaly derivative.
getAnomalyDot(PositionAngleType) - 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.files.rinex.observation.RinexObservationHeader: Get the azimuth of the zero direction of a fixed antenna.
getAntennaBSight() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the antenna B.Sight.
getAntennaHeight() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the antenna height.
getAntennaKey(AbsoluteDate) - Method in class org.orekit.files.sinex.Station: Get the antenna key for the given epoch.
getAntennaKeyTimeSpanMap() - Method in class org.orekit.files.sinex.Station: Get the TimeSpanMap of site antenna type.
getAntennaNumber() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the number of the antenna.
getAntennaPhaseCenter() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the antenna phasecenter.
getAntennaReferencePoint() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the position of antenna reference point for antenna on vehicle.
getAntennaType() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the type of the antenna.
getAntennaZeroDirection() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the zero direction of antenna.
getAntiSpoofing() - Method in class org.orekit.gnss.rflink.gps.SubFrame: Get anti-spoofing flag.
getAntiSpoofing(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame4E: Get the anti-spoofing for a satellite.
getAODC() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage: Getter for the Age Of Data Clock (AODC).
getAODC() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouLegacyNavigationMessage: Getter for the Age Of Data Clock (AODC).
getAODE() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage: Getter for the Age Of Data Ephemeris (AODE).
getAODE() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouLegacyNavigationMessage: Getter for the Age Of Data Ephemeris (AODE).
getAODO() - Method in class org.orekit.gnss.rflink.gps.SubFrame2: Get Age Of data Offset.
getAp() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters: Get the Ap index.
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.
getApoapsisAltitude() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the distance of the furthest point in the objects orbit above the equatorial radius of the central body.
getApoapsisDetectionAdaptableInterval() - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory: Method providing a candidate AdaptableInterval for apoapsis detection.
getApplicableWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the applicable wavelength.
getAppliedEffects() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase: Get the applied effects of modifiers.
getAppliedVoltage() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the applied voltage.
getApproachAngle() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the approach angle computed between Objects 1 and 2 in the RTN coordinate frame relative to object 1.
getApproxPos() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the Approximate Marker Position.
getAProvider() - Method in class org.orekit.models.earth.troposphere.AbstractVienna: Get provider for Vienna a_h and a_w coefficients.
getApsideDetectionAdaptableInterval() - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory: Method providing a candidate AdaptableInterval for arbitrary apside detection.
getArbitraryEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Get an arbitrary date.
getArcMinute() - Method in class org.orekit.bodies.SexagesimalAngle: Get arc-minute part of the angle.
getArcSecond() - Method in class org.orekit.bodies.SexagesimalAngle: Get arc-second part of the angle.
getArea() - Method in class org.orekit.forces.Panel: Get panel area.
getAreaDRG() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the effective area of the object exposed to atmospheric drag.
getAreaPC() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the actual area of the object.
getAreaPCMax() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the maximum area of the object to be used to compute the collision probability.
getAreaPCMin() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Set the minimum area of the object to be used to compute the collision probability.
getAreaSRP() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the effective area of the object exposed to solar radiation pressure.
getAstronomicalAmplitudesMap() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader: Get astronomical amplitudes map.
getAtmosphere() - Method in class org.orekit.forces.drag.AbstractDragForceModel: Get the atmospheric model.
getAtmosphere() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the atmospheric model.
getAtmosphericModel() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get name of atmospheric model.
getAtmosphericModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get name of atmospheric model.
getAttBasis() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata: Get basis of this attitude state time history data.
getAttBasisID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata: Get identification number of the orbit determination or simulation upon which this attitude is based.
getAttID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata: Get attitude identification number.
getAttitude() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the attitude.
getAttitude() - Method in class org.orekit.propagation.SpacecraftState: Get the attitude.
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.ApmData: Get the attitude.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, 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.AlignedAndConstrained: 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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProviderModifier: 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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, 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.FrameAlignedProvider: 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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, 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.LofOffsetPointing: 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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, 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.TabulatedProvider: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TorqueFree: 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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AlignedAndConstrained: 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(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProviderModifier: 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(PVCoordinatesProvider, AbsoluteDate, 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.FrameAlignedProvider: 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(PVCoordinatesProvider, AbsoluteDate, 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(PVCoordinatesProvider, AbsoluteDate, 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(PVCoordinatesProvider, AbsoluteDate, 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.TorqueFree: 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(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the attitude corresponding to an orbital state.
getAttitudeActuatorType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: Get the type of actuator for attitude control.
getAttitudeBlocks() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData: Get attitude state histories logical blocks.
getAttitudeControlAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: Get the accuracy of attitude control.
getAttitudeControlMode() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: Get the attitude control mode.
getAttitudeDeterminationBlock() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData: Get attitude determination logical block.
getAttitudeInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator: Get attitude interpolator.
getAttitudeInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator: Get attitude interpolator.
getAttitudeKnowledgeAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: Get the accuracy of attitude knowledge.
getAttitudeModelParameters(double[]) - Method in class org.orekit.forces.maneuvers.Maneuver: Extract attitude model' parameters from the parameters' array called in by the ForceModel interface.
getAttitudeModelParameters(T[]) - Method in class org.orekit.forces.maneuvers.Maneuver: Extract attitude model' parameters from the parameters' array called in by the ForceModel interface.
getAttitudeOverride() - Method in class org.orekit.forces.empirical.AbstractParametricAcceleration: Getter for attitude override.
getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.AbstractImpulseManeuver: 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.OrbitPhysicalProperties: Get the overall accuracy of spacecraft to maintain attitude.
getAttitudeProvider() - Method in class org.orekit.control.indirect.shooting.propagation.ShootingPropagationSettings: Getter for the attitude provider.
getAttitudeProvider() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory: Get the attitude provider for this attitude ephemeris segment.
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 interface org.orekit.propagation.conversion.PropagatorBuilder: 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.
getAttitudeRotation(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.attitudes.AttitudeProvider: Computed the rotation given the input state and parameters' values.
getAttitudeRotation(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.attitudes.AttitudeRotationModel: Computed the rotation given the input state and parameters' values.
getAttitudeRotation(SpacecraftState, double[]) - Method in interface org.orekit.attitudes.AttitudeProvider: Computed the rotation given the input state and parameters' values.
getAttitudeRotation(SpacecraftState, double[]) - Method in interface org.orekit.attitudes.AttitudeRotationModel: Computed the rotation given the input state and parameters' values.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AlignedAndConstrained: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FixedRate: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FrameAlignedProvider: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffset: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.SpinStabilized: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AlignedAndConstrained: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FrameAlignedProvider: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeRotation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized: Compute the attitude-related rotation corresponding to an orbital state.
getAttitudeStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination: Get attitude states.
getAttitudeStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory: Get the attitude states.
getAttitudeType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState: Get the type of the elements.
getAttitudeType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata: Get attitude element set type.
getAttitudeType() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get the format of the data lines in the message.
getAttoSeconds() - Method in class org.orekit.time.TimeOffset: Get the normalized attoseconds part of the time.
getAttPrevID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata: Get identification number of previous attitude.
getAugmentedInitialState(int) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter: Compute the additional state from the additionalEquations.
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() - 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.
getAuthentication(String) - Static method in enum org.orekit.gnss.metric.ntrip.Authentication: Get the authentication type corresponding to a keyword.
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.acm.AttitudeState: Get which derivatives of position are available in this state.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory: Get which derivatives of angular data are available in this attitude ephemeris segment.
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.iirv.IIRVSegment: 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.SP3Ephemeris: Get the available derivatives.
getAvailableDerivatives() - Method in class org.orekit.files.sp3.SP3Segment: Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
getAvailableObservationPairs() - Method in class org.orekit.files.sinex.DifferentialSignalBias: Get all available observation type pairs for the satellite.
getAvailableObservations() - Method in class org.orekit.files.sinex.ObservableSpecificSignalBias: Get all available observation types for the satellite.
getAvailableSatelliteSystems() - Method in class org.orekit.files.sinex.StationDifferentialSignalBias: Get the satellite systems available for the station.
getAvailableSatelliteSystems() - Method in class org.orekit.files.sinex.StationObservableSpecificSignalBias: Get the satellite systems available for the station.
getAveragedCircularEx() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle: Getter for averaged circular ex.
getAveragedCircularEy() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle: Getter for averaged circular ey.
getAveragedEccentricity() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle: Getter for the averaged eccentricity.
getAveragedElements() - Method in interface org.orekit.propagation.conversion.averaging.AveragedOrbitalState: Getter for the averaged orbital elements.
getAveragedElements() - Method in class org.orekit.propagation.conversion.averaging.BrouwerLyddaneOrbitalState: Getter for the averaged orbital elements.
getAveragedElements() - Method in class org.orekit.propagation.conversion.averaging.DSST6X0OrbitalState: Getter for the averaged orbital elements.
getAveragedElements() - Method in class org.orekit.propagation.conversion.averaging.EcksteinHechlerOrbitalState: Getter for the averaged orbital elements.
getAveragedElements() - Method in class org.orekit.propagation.conversion.averaging.SGP4OrbitalState: Getter for the averaged orbital elements.
getAveragedEquinoctialEx() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle: Getter for the averaged equinoctial ex.
getAveragedEquinoctialEy() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle: Getter for the averaged equinoctial ey.
getAveragedHx() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle: Getter for the averaged hx.
getAveragedHy() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle: Getter for the averaged hy.
getAveragedInclination() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle: Getter for averaged inclination.
getAveragedInclination() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle: Getter for the averaged inclination.
getAveragedMeanAnomaly() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle: Getter for the averaged mean anomaly.
getAveragedMeanLatitudeArgument() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle: Getter for averaged mean latitude argument.
getAveragedMeanLongitudeArgument() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle: Getter for the averaged mean longitude argument.
getAveragedPerigeeArgument() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle: Getter for the averaged perigee argument.
getAveragedRightAscensionOfTheAscendingNode() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle: Getter for averaged RAAN.
getAveragedRightAscensionOfTheAscendingNode() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle: Getter for the averaged RAAN.
getAveragedSemiMajorAxis() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle: Getter for averaged semi-major axis.
getAveragedSemiMajorAxis() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle: Getter for the averaged semi-major axis.
getAveragedSemiMajorAxis() - Method in class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle: Getter for the averaged semi-major axis.
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
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.
getAw() - Method in class org.orekit.models.earth.troposphere.FieldViennaACoefficients: Get wet coefficient.
getAw() - Method in class org.orekit.models.earth.troposphere.ViennaACoefficients: Get wet coefficient.
getAx2oA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext: Getter for the ax2oA.
getAx2oA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext: Getter for the ax2oA.
getAxis() - Method in class org.orekit.models.earth.displacement.PsdCorrection: Get correction axis.
getAxisNormalToCollisionPlane() - Method in class org.orekit.frames.encounter.DefaultEncounterLOF: Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.
getAxisNormalToCollisionPlane() - Method in interface org.orekit.frames.encounter.EncounterLOF: Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.
getAxisNormalToCollisionPlane() - Method in class org.orekit.frames.encounter.ValsecchiEncounterFrame: Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.
getAxisNormalToCollisionPlane(Field<T>) - Method in class org.orekit.frames.encounter.DefaultEncounterLOF: Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.
getAxisNormalToCollisionPlane(Field<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF: Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.
getAxisNormalToCollisionPlane(Field<T>) - Method in class org.orekit.frames.encounter.ValsecchiEncounterFrame: Get the axis normal to the collision plane (i, j or k) in this encounter local orbital frame.
getAzimuth() - Method in class org.orekit.bodies.Loxodrome: Get the azimuth.
getAzimuth() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement: Get the azimuth angle.
getAzimuth() - Method in class org.orekit.utils.FieldTrackingCoordinates: Get the azimuth.
getAzimuth() - Method in class org.orekit.utils.TrackingCoordinates: Get the azimuth.
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.
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.
getAzimuthRate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement: Get the azimuth rate.
getAzr() - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickParameters: Get effective sunspot number.
getb() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext: Get b = 1 / (1 + sqrt(1 - e²)) = 1 / (1 + B).
getb() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Get b = 1 / (1 + sqrt(1 - e²)) = 1 / (1 + B).
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.bodies.FieldEllipse: Get the semi minor axis.
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).
getB2Bot() - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickParameters: Get the F2 layer thickness parameter (bottom).
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(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.
getBaseName(T) - Method in class org.orekit.data.AbstractListCrawler: Get the base name of an input.
getBaseOffsets() - Method in class org.orekit.time.UTCScale: Get the base offsets.
getBaseProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get a time-independent provider containing base harmonics coefficients.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointingAttitudeModifier: Compute the base system state at given date, without modifications.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointingAttitudeModifier: Compute the base system state at given date, without modifications.
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.DSSTThirdBodyDynamicContext: 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.FieldDSSTThirdBodyDynamicContext: 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.DSSTThirdBodyDynamicContext: Get B³.
getBBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Get B³.
getBDGIMMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get the ionosphere BDGIM messages.
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.
getBE(double) - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickParameters: Get the E layer thickness parameter.
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(GnssSignal) - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults: Return the date of validity beginning of the detector.
getBeginTime() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver: Get start time of actual maneuver, relative to t₀.
getBeidouCivilianNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get all the Beidou navigation messages contained in the file.
getBeidouCivilianNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get the Beidou navigation messages for the given satellite Id.
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.
getBeidouLegacyNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get all the Beidou navigation messages contained in the file.
getBeidouLegacyNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get the Beidou navigation messages for the given satellite Id.
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.
getBeidouToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data: Get the Beidou time of clock.
getBeta() - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage: Get the β coefficients.
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.DSSTGravityContext: Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext: Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext: Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Get direction cosine β for central body.
getBeta0() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get β₀ field.
getBeta1() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get β₁ field.
getBeta2() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get β₂ field.
getBeta3() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get β₃ field.
getBetaAngleThreshold() - Method in class org.orekit.propagation.events.BetaAngleDetector: The beta angle threshold (radians).
getBetaAngleThreshold() - Method in class org.orekit.propagation.events.FieldBetaAngleDetector: The beta angle threshold (radians).
getBF1(double) - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickParameters: Get the F1 layer thickness parameter.
getBGDE1E5a() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGalileoNavigationMessage: Getter for the E1/E5a broadcast group delay.
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.FieldGalileoNavigationMessage: Getter for the the Broadcast Group Delay E5b/E1.
getBGDE5bE1() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Getter for the the Broadcast Group Delay E5b/E1.
getBias(ObservationType, ObservationType, AbsoluteDate) - Method in class org.orekit.files.sinex.DifferentialSignalBias: Get the value of the Differential Signal Bias for a given observation pair at a given date.
getBias(ObservationType, AbsoluteDate) - Method in class org.orekit.files.sinex.ObservableSpecificSignalBias: Get the value of the Observable-specific Signal Bias for a given observation type at a given date.
getBiasMode() - Method in class org.orekit.files.sinex.BiasDescription: Get the bias mode.
getBinKurtosis() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement: Get the bin kurtosis from the mean of raw accepted time-of-flight values minus the trend function.
getBinPeakMinusMean() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement: Get the bin peak - mean value.
getBinRms() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement: Get the bin RMS from the mean of raw accepted time-of-flight values minus the trend function.
getBinSkew() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement: Get the bin skew from the mean of raw accepted time-of-flight values minus the trend function.
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.DSSTGravityContext: Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext: Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext: Get B / A.
getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Get B / A.
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext: Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext: Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext: Get BoABpo = B / A(1 + B).
getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Get BoABpo = B / A(1 + B).
getBody() - Method in class org.orekit.bodies.Loxodrome: Get the body on which the loxodrome is defined.
getBody() - Method in class org.orekit.files.ccsds.definitions.BodyFacade: Get the celestial body.
getBody() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory: Get central 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.FieldLatitudeRangeCrossingDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.FieldLongitudeCrossingDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector: 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.LatitudeRangeCrossingDetector: 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.events.LongitudeRangeCrossingDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Get third body.
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.
getBodyFixedToInertialTransform() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext: Getter for the bodyFixedToInertialTransform.
getBodyFixedToInertialTransform() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext: Getter for the bodyFixedToInertialTransform.
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
getBodyName() - Method in class org.orekit.forces.gravity.AbstractBodyAttraction: Getter for the body's name.
getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody: Get a body oriented, body centered frame.
getBodyPosition(AbsoluteDate, Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm: Get body's position.
getBodyPosition(AbsoluteDate, Frame) - Method in class org.orekit.forces.gravity.AbstractBodyAttraction: Get the body's position vector.
getBodyPosition(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.forces.gravity.AbstractBodyAttraction: Get the body's position vector.
getBodyPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.forces.gravity.AbstractBodyAttraction: Get the body's position-velocity-acceleration vector.
getBodyPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.forces.gravity.AbstractBodyAttraction: Get the body's position-velocity-acceleration vector.
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.OrbitPhysicalProperties: 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 at tle date.
getBStar(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLE: Get the ballistic coefficient at a specific date.
getBTerm() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Get the SGP4-XP drag-like coefficient.
getBufferedReader() - Method in class org.orekit.data.LineOrientedFilteringReader: Get the underlying line-oriented reader.
getBuilder() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler: Get the builder associated with this scheduler.
getBuilder() - Method in interface org.orekit.estimation.measurements.generation.Scheduler: Get the builder associated with this scheduler.
getBuilders() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator
getBusModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: 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.forces.DSSTJ2SquaredClosedFormContext: Get the cosine of the inclination.
getC() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext: Get the cosine of the inclination.
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.
getC1cCodePhaseBias() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the code phase bias correction for GLONASS PredefinedObservationType.C1C signal.
getC1pCodePhaseBias() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the code phase bias correction for GLONASS PredefinedObservationType.C1P signal.
getC2cCodePhaseBias() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the code phase bias correction for GLONASS PredefinedObservationType.C2C signal.
getC2n0(int) - Method in class org.orekit.models.earth.ReferenceEllipsoid: Get the fully normalized coefficient C_2n,0 for the normal gravity potential.
getC2pCodePhaseBias() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the code phase bias correction for GLONASS PredefinedObservationType.C2P signal.
getCache() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData: Get underlying cache.
getCache() - Method in class org.orekit.time.SampledClockModel: Get the clock offsets cache.
getCachedPositionAngleType() - Method in class org.orekit.orbits.CircularOrbit: Get the cached PositionAngleType.
getCachedPositionAngleType() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the cached PositionAngleType.
getCachedPositionAngleType() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the cached PositionAngleType.
getCachedPositionAngleType() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the cached PositionAngleType.
getCachedPositionAngleType() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the cached PositionAngleType.
getCachedPositionAngleType() - Method in class org.orekit.orbits.KeplerianOrbit: Get the cached PositionAngleType.
getCachedPositionAngleType() - Method in interface org.orekit.orbits.PositionAngleBased: Get the cached PositionAngleType.
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.
getCalibrationData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the calibration data for the data block.
getCalibrationDetailData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the calibration detail data for the data block.
getCalibrationDetailRecords() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the CalibrationDetail record(s) related to the default system configuration id.
getCalibrationDetailRecords(String) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the CalibrationDetail record(s) related to the given systemConfigurationId.
getCalibrationRecords() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the Calibration record(s) related to the default system configuration id.
getCalibrationRecords(String) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the Calibration record(s) related to the given systemConfigurationId.
getCalibrationTargetRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration: Get the calibration target configuration record.
getCalibrationTargetRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Get calibration target configuration record related to the systemRecord.
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.
getCaOrPFlag() - Method in class org.orekit.gnss.rflink.gps.SubFrame1: Get C/A or P flag.
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() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the carrier phase.
getCarrierPhase(String) - Static method in enum org.orekit.gnss.metric.ntrip.CarrierPhase: Get the carrier phase corresponding to a code.
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(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.
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.
getCartesianPoint() - Method in class org.orekit.frames.TopocentricFrame: Get the surface point defining the origin of the frame.
getCasters() - Method in class org.orekit.gnss.metric.ntrip.SourceTable: Get the casters records.
getCatalogName() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata: Get the specification of satellite catalog source.
getCatalogName() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the satellite catalog used for the object.
getCatalogName() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the specification of satellite catalog source.
getCcsdsEpoch() - Method in class org.orekit.time.AbstractTimeScales
getCcsdsEpoch() - 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).
getCCSDSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4).
getCCSDSName() - Method in enum org.orekit.files.ccsds.definitions.PocMethodType: Get CCSDS compatible name.
getCCSDSType() - Method in enum org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType: Get the CCSDS type if used by the SANA registry.
getCDAreaOverMass() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the object’s Cd x A/m used to propagate the state vector and covariance to TCA.
getCdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the Unique identifier of Conjunction Data Message linked to this Orbit Data Message.
getCdrgdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [7,7] in covariance matrix (with index starting at 1).
getCdrgdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [7,7] in covariance matrix (with index starting at 1).
getCdrgn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [7,3] in covariance matrix (with index starting at 1).
getCdrgndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [7,6] in covariance matrix (with index starting at 1).
getCdrgr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [7,1] in covariance matrix (with index starting at 1).
getCdrgrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [7,4] in covariance matrix (with index starting at 1).
getCdrgt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [7,2] in covariance matrix.
getCdrgtdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [7,5] in covariance matrix (with index starting at 1).
getCdrgx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [7,1] in covariance matrix (with index starting at 1).
getCdrgxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [7,4] in covariance matrix (with index starting at 1).
getCdrgy() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [7,2] in covariance matrix.
getCdrgydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [7,5] in covariance matrix (with index starting at 1).
getCdrgz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [7,3] in covariance matrix (with index starting at 1).
getCdrgzdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [7,6] in covariance matrix (with index starting at 1).
getCelestialBodies() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the instance of CelestialBodies that is called by the static methods in this class.
getCelestialBodies() - Method in class org.orekit.data.CompositeDataContext
getCelestialBodies() - Method in interface org.orekit.data.DataContext: Get a factory constructing CelestialBodys based on the auxiliary data in this context.
getCelestialBodies() - Method in class org.orekit.data.ExceptionalDataContext
getCelestialBodies() - Method in class org.orekit.data.LazyLoadedDataContext
getCelestialBody() - Method in enum org.orekit.files.ccsds.definitions.CenterName: Get the celestial body corresponding to the CCSDS constant.
getCelestialBody(CelestialBodies) - Method in enum org.orekit.files.ccsds.definitions.CenterName: Get the celestial body corresponding to the CCSDS constant.
getCelestialBodyProvider() - Method in class org.orekit.propagation.events.BetaAngleDetector: Coordinate provider for the celestial body.
getCelestialBodyProvider() - Method in class org.orekit.propagation.events.FieldBetaAngleDetector: Coordinate provider for the celestial body.
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.bodies.FieldEllipse: 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.ocm.TrajectoryStateHistoryMetadata: Get the origin of reference frame.
getCenter() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata: 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.files.rinex.observation.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(FieldVector2D<T>) - Method in class org.orekit.bodies.FieldEllipse: Find the center of curvature (point on the evolute) at the nadir of a point.
getCenterOfCurvature(Vector2D) - Method in class org.orekit.bodies.Ellipse: Find the center of curvature (point on the evolute) at the nadir of a point.
getCenterOfMassCorrection() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement: Get the target center of mass.
getCenterOfMassOffset() - Method in class org.orekit.files.ilrs.CPFHeader: Get the approximate center of mass to reflector offset.
getCenterOfPressure() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties: Get the location of center of pressure.
getCenterOfPressureReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties: Get reference frame for center of pressure.
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.
getCentralDate(AbsoluteDate, AbsoluteDate, AbsoluteDate, double) - Static method in class org.orekit.time.AbstractTimeInterpolator: Get the central date to use to find neighbors while taking into account extrapolation threshold.
getCentralDate(AbsoluteDate, ImmutableTimeStampedCache<T>, double) - Static method in class org.orekit.time.AbstractTimeInterpolator: Get the central date to use to find neighbors while taking into account extrapolation threshold.
getCentralDate(FieldAbsoluteDate<KK>, FieldAbsoluteDate<KK>, FieldAbsoluteDate<KK>, double) - Static method in class org.orekit.time.AbstractFieldTimeInterpolator: Get the central date to use to find neighbors while taking into account extrapolation threshold.
getCentralDate(FieldAbsoluteDate<KK>, ImmutableFieldTimeStampedCache<T, KK>, double) - Static method in class org.orekit.time.AbstractFieldTimeInterpolator: Get the central date to use to find neighbors while taking into account extrapolation threshold.
getChi() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext: Getter for the chi.
getChi() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext: Get Χ = 1 / sqrt(1 - e²) = 1 / B.
getChi2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext: Getter for the chi2.
getChi2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext: Get Χ².
getChi3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Getter for the Χ³.
getChi3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Getter for the Χ³.
getChildren() - Method in class org.orekit.frames.OrphanFrame: Get all children of the instance.
getCic() - Method in class org.orekit.gnss.rflink.gps.SubFrame3: Get Cic.
getCic() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get amplitude of the cosine harmonic correction term to the angle of inclination.
getCicDriver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get the driver for 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.gnss.rflink.gps.SubFrame3: Get Cis.
getCis() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get amplitude of the sine harmonic correction term to the angle of inclination.
getCisDriver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get the driver for 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.
getClassicalRungeKuttaIntegratorSettings(double) - Static method in class org.orekit.control.indirect.shooting.propagation.ShootingIntegrationSettingsFactory: Returns shooting integration settings according to the classical Runge Kutta scheme.
getClassification() - Method in class org.orekit.files.ccsds.section.Header: Get the classification/caveats.
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.
getClockAcceleration() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine: Getter for the clock acceleration.
getClockAccelerationDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to change station clock acceleration (which is related to measurement date).
getClockAccelerationDriver() - Method in class org.orekit.estimation.measurements.ObservableSatellite: Get the clock acceleration parameter driver.
getClockAccelerationSigma() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine: Getter for the clock acceleration sigma.
getClockAccuracy() - Method in class org.orekit.files.sp3.SP3Coordinate: Get the clock accuracy.
getClockBase() - Method in class org.orekit.files.sp3.SP3Header: Get the base for clock/clock-rate accuracy.
getClockBias() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine: Getter for the clock bias.
getClockBiasSigma() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine: Getter for the clock bias sigma.
getClockConstraint() - Method in class org.orekit.files.rinex.clock.RinexClock.ReferenceClock: Getter for the clock constraint.
getClockCorrection() - Method in class org.orekit.files.sp3.SP3Coordinate: Get the clock correction value.
getClockCorrection() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmClockCorrectionData: Get the clock correction data.
getClockCorrection() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData: Get the clock correction data.
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.files.rinex.clock.RinexClock: Getter for an unmodifiable map of clock data.
getClockDataTypes() - Method in class org.orekit.files.rinex.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.files.rinex.clock.RinexClock.ReferenceClock: Getter for the clock ID.
getClockOffsetApplied() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the application flag for realtime-derived receiver clock offset.
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.files.rinex.clock.RinexClock.ClockDataLine: Getter for the clock rate.
getClockRateAccuracy() - Method in class org.orekit.files.sp3.SP3Coordinate: Get the clock rate accuracy.
getClockRateChange() - Method in class org.orekit.files.sp3.SP3Coordinate: Get the clock rate.
getClockRateSigma() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine: Getter for the clock rate sigma.
getCndotn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [6,3] in covariance matrix (with index starting at 1).
getCndotndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [6,6] in covariance matrix (with index starting at 1).
getCndotr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [6,1] in covariance matrix (with index starting at 1).
getCndotrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [6,4] in covariance matrix (with index starting at 1).
getCndott() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [6,2] in covariance matrix (with index starting at 1).
getCndottdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [6,5] in covariance matrix (with index starting at 1).
getCnm() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data: Get the cosine parameters of spherical harmonics expansion of degree N and order M.
getCnn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [3,3] in covariance matrix (with index starting at 1).
getCnr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [3,1] in covariance matrix (with index starting at 1).
getCnt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [3,2] in covariance matrix (with index starting at 1).
getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext: Get co2AB = C / 2AB.
getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTGravityContext: 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.FieldDSSTGravityContext: Get Co2AB = C / 2AB.
getCodeBias() - Method in class org.orekit.gnss.metric.messages.common.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(AbsoluteDate, Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients: 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.
getCoefficients(FieldAbsoluteDate<T>, Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients: 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.
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.
getCollisionPercentile() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the array of 1 to n elements indicating the percentile(s) for which estimates of the collision probability are provided in the COLLISION_PROBABILITY variable.
getCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the probability (between 0.0 and 1.0) that Object1 and Object2 will collide.
getCollisionProbaMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the method that was used to calculate the collision probability.
getCombinationType() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationData: Get the type of the combination of measurements used to build the instance.
getCombinedFrequency() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationData: Get the value of the combined frequency in MHz.
getCombinedFrequency(GnssSignal, GnssSignal) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination: Get the combined frequency of two measurements.
getCombinedFrequency(GnssSignal, GnssSignal) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCombination: Get the combined frequency of two measurements.
getCombinedFrequency(GnssSignal, GnssSignal) - Method in class org.orekit.estimation.measurements.gnss.IonosphereFreeCombination: Get the combined frequency of two measurements.
getCombinedFrequency(GnssSignal, GnssSignal) - Method in class org.orekit.estimation.measurements.gnss.NarrowLaneCombination: Get the combined frequency of two measurements.
getCombinedFrequency(GnssSignal, GnssSignal) - Method in class org.orekit.estimation.measurements.gnss.WideLaneCombination: Get the combined frequency of two measurements.
getCombinedProvider(TransformProvider, TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils: Combine two transform providers.
getCombinedRadius() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Get combined radius.
getCombinedRadius() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Get combined radius.
getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination: 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, double) - Method in class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCombination: Get the combined observed value of two measurements.
getCombinedValue(double, GnssSignal, double, GnssSignal) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination: Get the combined observed value of two measurements.
getCombinedValue(double, GnssSignal, double, GnssSignal) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCombination: Get the combined observed value of two measurements.
getCombinedValue(double, GnssSignal, double, GnssSignal) - Method in class org.orekit.estimation.measurements.gnss.IonosphereFreeCombination: Get the combined observed value of two measurements.
getCombinedValue(double, GnssSignal, double, GnssSignal) - Method in class org.orekit.estimation.measurements.gnss.NarrowLaneCombination: Get the combined observed value of two measurements.
getCombinedValue(double, GnssSignal, double, GnssSignal) - Method in class org.orekit.estimation.measurements.gnss.WideLaneCombination: Get the combined observed value of two measurements.
getComment() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get comment for relative metadata.
getComments() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData: Get the comments.
getComments() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData: Get the comments.
getComments() - Method in class org.orekit.files.ccsds.ndm.Ndm: Get an unmodifiable view of the comments.
getComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer: Get the comments.
getComments() - Method in class org.orekit.files.ilrs.CPF: Get the comments contained in the file.
getComments() - Method in class org.orekit.files.ilrs.CRD: Get the comments contained in the file.
getComments() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the comments.
getComments() - Method in class org.orekit.files.rinex.RinexFile: Get an unmodifiable view of the comments.
getComments() - Method in class org.orekit.files.sp3.SP3Header: Get the comments.
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.
getCompleteName(T) - Method in class org.orekit.data.AbstractListCrawler: Get the complete name of a input.
getComponents() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration: Get the components (config ids) for system configuration.
getComponents(int) - Method in class org.orekit.time.AbsoluteDate: Split the instance into date/time components for a local time.
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.AbsoluteDate: 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.AbsoluteDate: Split the instance into date/time components for a time zone.
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.AbsoluteDate: 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.
getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate: Split the instance into date/time components.
getComponents(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate: Split the instance into date/time components.
getCompressionEncryption() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the compression/encryption algorithm applied.
getConditionChecker() - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting: Getter for the boundary condition checker.
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.
getConfigurationId() - Method in class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration: Get the configuration ID.
getConfigurationRecord(String) - Method in class org.orekit.files.ilrs.CRDConfiguration: Get configuration record corresponding to the configId.
getConfigurationRecordMap() - Method in class org.orekit.files.ilrs.CRDConfiguration: Get the configuration records map.
getConfigurationRecords() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the system configuration records.
getConjunctionId() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the Originator’s ID that uniquely identifies the conjunction to which the message refers.
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, AbsoluteDate) - 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, AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.GravityFields: Get a constant gravity field normalized coefficients provider frozen at a given epoch.
getConstantNormalizedProvider(int, int, AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields: Get a constant gravity field normalized coefficients provider frozen at a given epoch.
getConstantUnnormalizedProvider(int, int, AbsoluteDate) - 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, AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.GravityFields: Get a constant gravity field unnormalized coefficients provider frozen at a given epoch.
getConstantUnnormalizedProvider(int, int, AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields: Get a constant gravity field unnormalized coefficients provider frozen at a given epoch.
getConstellation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the name of the constellation this space object belongs to.
getConstellation() - Method in class org.orekit.orbits.WalkerConstellationSlot: Get the constellation.
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.
getContentAsFreeTextList() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as a list of free-text strings.
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 normalized strings.
getContentAsNormalizedString() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry.
getContentAsUppercaseCharacter() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as an uppercase character.
getContentAsUppercaseList() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as a list of normalized and uppercased strings.
getContentAsUppercaseString() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as normalized and uppercased.
getContentAsVector() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the content of the entry as a vector.
getContext() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter: Get the current context.
getContext() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter: Get the current context.
getControl3DVectorCostType() - Method in class org.orekit.forces.maneuvers.AbstractImpulseManeuver: Get the control vector's cost type.
getControl3DVectorCostType() - Method in class org.orekit.forces.maneuvers.Maneuver: Get the control vector's cost type.
getControl3DVectorCostType() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the control vector's cost type.
getControl3DVectorCostType() - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel: Get the control vector's cost type.
getControl3DVectorCostType() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel: Get the control vector's cost type.
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.
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() - 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.iirv.IIRVSegment: 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.SP3Segment: Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
getCoordinates(SpacecraftState, int, int) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement: Get Cartesian coordinates as derivatives.
getCoordinateSystem() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current CoordinateSystemTerm value.
getCoordinateSystem() - Method in class org.orekit.files.iirv.IIRVVector: Gets the coordinate system term.
getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3Header: Returns the coordinate system of the entries in this orbit file.
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.
getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the estimated measurement.
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.
getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the corrected spacecraft states.
getCorrection() - Method in class org.orekit.files.rinex.observation.PhaseShiftCorrection: Get the Phase Shift Corrections.
getCorrection() - Method in class org.orekit.files.rinex.observation.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.
getCosineAz() - Method in class org.orekit.models.earth.ionosphere.nequick.Ray: Get the cosine of azimuth of satellite as seen from ray-perigee.
getCosparID() - Method in class org.orekit.gnss.antenna.SatelliteAntenna: Get COSPAR ID.
getCost() - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointDerivativesProvider: Getter for the cost.
getCost() - Method in class org.orekit.control.indirect.adjoint.FieldCartesianAdjointDerivativesProvider: Getter for the cost.
getCostDerivativeProvider(String) - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost: Get the derivatives provider to be able to integrate the cost function.
getCostDerivativeProvider(String) - Method in interface org.orekit.control.indirect.adjoint.cost.FieldCartesianCost: Get the derivatives provider to be able to integrate the cost function.
getCount() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase: 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
getCovariance(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris: Get the covariance at given date.
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.adm.acm.AcmData: Get covariance logical blocks.
getCovarianceBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData: Get covariance logical blocks.
getCovarianceInterpolator() - Method in class org.orekit.propagation.analytical.Ephemeris: Get covariance interpolator.
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.estimation.sequential.PhysicalEstimatedState: Get the physical covariance matrix.
getCovarianceMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance: Get the Position/Velocity covariance matrix.
getCovarianceMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the method name used to calculate covariance during OD.
getCovarianceOrbitType() - Method in class org.orekit.propagation.StateCovarianceMatrixProvider: Get the orbit type in which the covariance matrix is expressed.
getCovariances() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistory: Get the covariances.
getCovariances() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistory: Get the covariances.
getCovarianceSource() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the source of the covariance data.
getCovarianceType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination: Get type of attitude error state.
getCovBasis() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata: Get basis of this covariance time history data.
getCovBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata: Get basis of this covariance time history data.
getCovBasisID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata: Get identification number of the orbit determination or simulation upon which this covariance is based.
getCovBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata: Get identification number of the orbit determination or simulation upon which this covariance is based.
getCovConfidence() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the measure of the confidence in the covariance errors matching reality.
getCovConfidence() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata: Get the measure of confidence in covariance error matching reality.
getCovConfidenceMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the method used for the calculation of COV_CONFIDENCE.
getCovFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata: Get epoch of the covariance reference frame.
getCovID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata: Get covariance identification number.
getCovID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata: Get covariance identification number.
getCovNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata: Get identification number of next covariance.
getCovOrdering() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata: Get covariance ordering.
getCovPrevID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata: Get identification number of previous covariance.
getCovPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata: Get identification number of previous covariance.
getCovReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata: Get reference frame of the covariance.
getCovReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata: Get reference frame of the covariance.
getCovScaleMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata: Get the maximum scale factor to apply to achieve realism.
getCovScaleMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata: Get the minimum scale factor to apply to achieve realism.
getCovType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata: Get covariance element set type.
getCovType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata: Get covariance element set type.
getCovUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadata: Get covariance element set units.
getCr3bpSystem() - Method in class org.orekit.orbits.RichardsonExpansion: Get the considered CR3BP system.
getCRAreaOverMass() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the object’s Cr x A/m used to propagate the state vector and covariance to TCA.
getCrc() - Method in class org.orekit.gnss.rflink.gps.SubFrame3: Get Crc.
getCrc() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get amplitude of the cosine harmonic correction term to the orbit radius.
getCrcDriver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get the driver for the amplitude of the cosine harmonic correction term to the orbit radius.
getCrdotn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [4, 3] in covariance matrix (with index starting at 1) .
getCrdotr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [4,1] in covariance matrix (with index starting at 1).
getCrdotrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [4, 4] in covariance matrix (with index starting at 1).
getCrdott() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [4,2] in covariance matrix (with index starting at 1).
getCreationDate() - Method in class org.orekit.files.ccsds.section.Header: Get the message creation date and time in UTC.
getCreationDate() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the creation date.
getCreationDate() - Method in class org.orekit.files.rinex.section.RinexBaseHeader: Getter for the creation date.
getCreationDate() - Method in class org.orekit.files.sinex.AbstractSinex: Get the creation date of the parsed SINEX file.
getCreationDate() - Method in class org.orekit.files.sinex.ParseInfo: Get creation date.
getCreationDateComponents() - Method in class org.orekit.files.rinex.section.RinexBaseHeader: Getter for the creation date of the file as a string.
getCreationDateString() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the creation date of the file as a string.
getCreationTimeString() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the creation time of the file as a string.
getCreationTimeZone() - Method in class org.orekit.files.rinex.section.RinexBaseHeader: Getter for the creation time zone of the file as a string.
getCreationTimeZoneString() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the creation time zone of the file as a string.
getCrossSectionalArea() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current CrossSectionalAreaTerm value.
getCrossSectionalArea() - Method in class org.orekit.files.iirv.IIRVVector: Gets the cross-sectional area term.
getCrr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [1,1] in covariance matrix (with index starting at 1).
getCrs() - Method in class org.orekit.gnss.rflink.gps.SubFrame2: Get Crs.
getCrs() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get amplitude of the sine harmonic correction term to the orbit radius.
getCrsDriver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get the driver for 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.
getcScaleFactor() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata: Get the (median) suggested covariance scale factor.
getcScaleFactorMax() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata: Get the maximum suggested covariance scale factor.
getcScaleFactorMin() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata: Get the minimum suggested covariance scale factor.
getCsig3eigvec3() - Method in class org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovariance: Get the Sigma/Eigenvectors Covariance data.
getCsrpdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [8,7] in covariance matrix (with index starting at 1).
getCsrpdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [8,7] in covariance matrix (with index starting at 1).
getCsrpn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [8,3] in covariance matrix (with index starting at 1).
getCsrpndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [8,6] in covariance matrix (with index starting at 1).
getCsrpr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [8,1] in covariance matrix (with index starting at 1).
getCsrprdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [8,4] in covariance matrix (with index starting at 1).
getCsrpsrp() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [8,8] in covariance matrix (with index starting at 1).
getCsrpsrp() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [8,8] in covariance matrix (with index starting at 1).
getCsrpt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [8,2] in covariance matrix (with index starting at 1).
getCsrptdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [8,5] in covariance matrix (with index starting at 1).
getCsrpx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [8,1] in covariance matrix (with index starting at 1).
getCsrpxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [8,4] in covariance matrix (with index starting at 1).
getCsrpy() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [8,2] in covariance matrix (with index starting at 1).
getCsrpydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [8,5] in covariance matrix (with index starting at 1).
getCsrpz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [8,3] in covariance matrix (with index starting at 1).
getCsrpzdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [8,6] in covariance matrix (with index starting at 1).
getCtdotn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [5,3] in covariance matrix (with index starting at 1).
getCtdotr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [5, 1] in covariance matrix (with index starting at 1).
getCtdotrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [5,4] in covariance matrix (with index starting at 1).
getCtdott() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [5,2] in covariance matrix (with index starting at 1).
getCtdottdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [5,5] in covariance matrix (with index starting at 1).
getCthrdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [9,7] in covariance matrix (with index starting at 1).
getCthrdrg() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [9,7] in covariance matrix (with index starting at 1).
getCthrn() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [9,3] in covariance matrix (with index starting at 1).
getCthrndot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [9,6] in covariance matrix (with index starting at 1).
getCthrr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [9,1] in covariance matrix (with index starting at 1).
getCthrrdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [9,4] in covariance matrix (with index starting at 1).
getCthrsrp() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [9,8] in covariance matrix (with index starting at 1).
getCthrsrp() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [9,8] in covariance matrix (with index starting at 1).
getCthrt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [9,2] in covariance matrix (with index starting at 1).
getCthrtdot() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [9,5] in covariance matrix (with index starting at 1).
getCthrthr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [9,9] in covariance matrix (with index starting at 1).
getCthrthr() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [9,9] in covariance matrix (with index starting at 1).
getCthrx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [9,1] in covariance matrix (with index starting at 1).
getCthrxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [9,4] in covariance matrix (with index starting at 1).
getCthry() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [9,2] in covariance matrix (with index starting at 1).
getCthrydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [9,5] in covariance matrix (with index starting at 1).
getCthrz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [9,3] in covariance matrix (with index starting at 1).
getCthrzdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [9,6] in covariance matrix (with index starting at 1).
getCtr() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [2,1] in covariance matrix (with index starting at 1).
getCtr81Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the centered 81-day arithmetic average of F10.7 (adjusted).
getCtr81Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the centered 81-day arithmetic average of F10.7 (observed).
getCtt() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the object [2,2] in covariance matrix (with index starting at 1).
getCuc() - Method in class org.orekit.gnss.rflink.gps.SubFrame2: Get Cuc.
getCuc() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get amplitude of the cosine harmonic correction term to the argument of latitude.
getCucDriver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get the driver for 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.AbstractKalmanEstimator: 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.SemiAnalyticalKalmanModel: Get the current date.
getCurrentDate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the current date.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator: 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.SemiAnalyticalKalmanModel: Get the current measurement number.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: 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.gnss.rflink.gps.SubFrame2: Get Cus.
getCus() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get amplitude of the sine harmonic correction term to the argument of latitude.
getCusDriver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get the driver for the amplitude of the sine harmonic correction term to the argument of latitude.
getCxdotx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [4,1] in covariance matrix (with index starting at 1).
getCxdotxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [4, 4] in covariance matrix (with index starting at 1).
getCxdoty() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [4,2] in covariance matrix (with index starting at 1).
getCxdotz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [4, 3] in covariance matrix (with index starting at 1) .
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 ).
getCxx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [1,1] in covariance matrix (with index starting at 1).
getCycleDuration() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get for 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.
getCydotx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [5, 1] in covariance matrix (with index starting at 1).
getCydotxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [5,4] in covariance matrix (with index starting at 1).
getCydoty() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [5,2] in covariance matrix (with index starting at 1).
getCydotydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [5,5] in covariance matrix (with index starting at 1).
getCydotz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [5,3] in covariance matrix (with index starting at 1).
getCyx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [2,1] in covariance matrix (with index starting at 1).
getCyy() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [2,2] in covariance matrix (with index starting at 1).
getCzdotx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [6,1] in covariance matrix (with index starting at 1).
getCzdotxdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [6,4] in covariance matrix (with index starting at 1).
getCzdoty() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [6,2] in covariance matrix (with index starting at 1).
getCzdotydot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [6,5] in covariance matrix (with index starting at 1).
getCzdotz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [6,3] in covariance matrix (with index starting at 1).
getCzdotzdot() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [6,6] in covariance matrix (with index starting at 1).
getCzx() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [3,1] in covariance matrix (with index starting at 1).
getCzy() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [3,2] in covariance matrix (with index starting at 1).
getCzz() - Method in class org.orekit.files.ccsds.ndm.cdm.XYZCovariance: Get the object [3,3] in covariance matrix (with index starting at 1).
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.
getDamping() - Method in class org.orekit.propagation.conversion.osc2mean.FixedPointConverter: Gets damping ratio.
getDarkCount() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the dark count.
getData() - Method in class org.orekit.files.ccsds.ndm.adm.acm.Acm: Get the data from the single segment.
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.DataDictionary: Get an unmodifiable view of the dictionary entries.
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.FieldDataDictionary: 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.
getDataId() - Method in class org.orekit.gnss.rflink.gps.SubFrame45: Get data ID.
getDataMap() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionMessage: Get the all data parsed in the RTCM correction message.
getDataObject1() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm: Get the file data.
getDataObject2() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm: Get the file data.
getDataProvidersManager() - Method in class org.orekit.data.AbstractSelfFeedingLoader: Get the data provider manager.
getDataProvidersManager() - Method in class org.orekit.data.LazyLoadedDataContext: Get the provider of auxiliary data for this data context.
getDataProvidersManager() - Method in class org.orekit.frames.LazyLoadedEop: Get the data providers manager for this instance.
getDataQuality() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the dataQuality.
getDataQulityIndicator() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics: Get the data quality assessment indicator 0=undefined or no comment 1=clear, easily filtered data, with little or no noise 2=clear data with some noise; filtering is slightly compromised by noise level 3=clear data with a significant amount of noise, or weak data with little noise.
getDataReleaseFlag() - Method in class org.orekit.files.ilrs.CRDHeader: Get the flag indicating the data release.
getDataSet() - Method in class org.orekit.estimation.measurements.filtering.SmoothedObservationDataSet: Get the original observation data set used to compute the smoothed observation data.
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader: Get the data set.
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader: Getter for the data set.
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader: Getter for the data set.
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader: Gets the data set.
getDataSource() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current DataSourceTerm value.
getDataSource() - Method in class org.orekit.files.iirv.IIRVVector: Gets the data source term.
getDataSource() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGalileoNavigationMessage: Getter for the the data source.
getDataSource() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Getter for the the data source.
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.files.rinex.clock.RinexClock.ClockDataLine: Getter for the clock data type.
getDataType(int) - Static method in enum org.orekit.files.ilrs.CRDHeader.DataType: Get the data type for the given indicator.
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.SP3Header: 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.EstimatedMeasurementBase: Get the date.
getDate() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet: Get the date.
getDate() - Method in class org.orekit.estimation.sequential.PhysicalEstimatedState: Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovariance: Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState: Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovariance: Get the date.
getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: 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.Calibration
getDate() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement: Get the date.
getDate() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement: Get the date.
getDate() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement
getDate() - Method in class org.orekit.files.rinex.observation.ObservationDataSet: Get the date.
getDate() - Method in class org.orekit.files.sinex.SinexEopEntry: Get the date.
getDate() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Get the date of the maneuver.
getDate() - Method in class org.orekit.frames.EOPEntry: Get the date.
getDate() - Method in class org.orekit.frames.FieldTransform: Get the date.
getDate() - Method in class org.orekit.frames.Transform: Get the date.
getDate() - Method in class org.orekit.gnss.DOP: Gets the calculation date of the DOP.
getDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.LocalSolarActivity
getDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader.LineParameters
getDate() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader.LineParameters
getDate() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters
getDate() - Method in class org.orekit.orbits.FieldOrbit: Get the date of orbital parameters.
getDate() - Method in class org.orekit.orbits.Orbit: Get the date of orbital parameters.
getDate() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage: Getter for the reference date of the ephemeris.
getDate() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements: Get 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.gnss.data.GNSSOrbitalElements: Get the date.
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.conversion.averaging.AbstractAveragedOrbitalState: Get the date.
getDate() - Method in interface org.orekit.propagation.conversion.averaging.AveragedOrbitalState: Get the 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.FieldStateCovariance: 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.propagation.StateCovariance: Get the date.
getDate() - Method in class org.orekit.time.AbsoluteDate: Get the date.
getDate() - Method in class org.orekit.time.ClockOffset: 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 class org.orekit.time.FieldClockOffset: Get the date.
getDate() - Method in interface org.orekit.time.FieldTimeStamped: Get the date.
getDate() - Method in class org.orekit.time.FieldTimeStampedPair: 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.TimeStampedDouble: Get the date.
getDate() - Method in class org.orekit.time.TimeStampedField: Get the date.
getDate() - Method in class org.orekit.time.TimeStampedPair: 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.
getDateComponents(int) - Method in class org.orekit.files.iirv.terms.DayOfYearTerm: Returns the DateComponents instance that corresponds this term's value.
getDateDetector(TimeStamped...) - Method in interface org.orekit.propagation.events.EventDetectorsProvider: Method building dates' detector.
getDates() - Method in class org.orekit.propagation.events.DateDetector: Get all event dates currently managed, in chronological order.
getDates() - Method in class org.orekit.propagation.events.FieldDateDetector: Get all event field dates currently managed, in chronological order.
getDatesDetectionConstantInterval(TimeStamped...) - Static method in class org.orekit.propagation.events.intervals.DateDetectionAdaptableIntervalFactory: Return a candidate AdaptableInterval for multiple dates detection with a constant max. check.
getDatesDetectionFieldConstantInterval(FieldTimeStamped<T>...) - Static method in class org.orekit.propagation.events.intervals.DateDetectionAdaptableIntervalFactory: Return a candidate FieldAdaptableInterval for multiple dates detection with a constant max. check.
getDatesDetectionFieldInterval(FieldTimeStamped<T>...) - Static method in class org.orekit.propagation.events.intervals.DateDetectionAdaptableIntervalFactory: Return a candidate FieldAdaptableInterval for multiple dates detection.
getDatesDetectionInterval(TimeStamped...) - Static method in class org.orekit.propagation.events.intervals.DateDetectionAdaptableIntervalFactory: Return a candidate AdaptableInterval for multiple dates detection.
getDateTime() - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickParameters: Get current date time components.
getDay() - Method in class org.orekit.time.DateComponents: Get the day.
getDayFraction() - Method in class org.orekit.files.sp3.SP3Header: 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.files.iirv.IIRVVector: Gets the day of year term.
getDayOfYear() - Method in class org.orekit.time.DateComponents: Get the day number in year.
getDayOfYear(AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.AbstractVienna: Get day of year.
getDayOfYear(FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.AbstractVienna: Get day of year.
getDayOfYear(TimeScale) - Method in class org.orekit.time.AbsoluteDate: Get day of year, preserving continuity as much as possible.
getDayOfYear(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate: Get day of year, preserving continuity as much as possible.
getDcBodyFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get spacecraft body frame in which OrbitManeuverHistoryMetadata.getDcBodyTrigger() is specified.
getDcBodyTrigger() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get direction in body frame for triggering duty cycle.
getDcExecStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get the start time of initial duty cycle-based maneuver execution.
getDcExecStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: 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.OrbitManeuverHistoryMetadata: Get the maximum number of "ON" duty cycles.
getDcMinCycles() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get the minimum number of "ON" duty cycles.
getDcPhaseStartAngle() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get phase angle of pulse start.
getDcPhaseStopAngle() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get phase angle of pulse stop.
getDcpSensitivityVectorPosition() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata: Get the DCP sensitivity vector (position errors at TCA).
getDcpSensitivityVectorVelocity() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata: Get the DCP sensitivity vector (velocity errors at TCA).
getDcRefDir() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get reference direction for triggering duty cycle.
getDcRefTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get duty cycle thrust reference time.
getDcTimePulseDuration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get duty cycle pulse "ON" duration.
getDcTimePulsePeriod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: 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.OrbitManeuverHistoryMetadata: Get type of duty cycle.
getDcWindowClose() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get the end time of duty cycle-based maneuver window.
getDcWindowOpen() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: 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.
getDecreasingTimeShift() - Method in class org.orekit.propagation.events.FieldEventShifter: 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.
getDefaultDetectionSettings(AbsoluteDate, AbsoluteDate) - Static method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector: Get default detection settings.
getDefaultEclipseDetectionSettings() - Static method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Get the default eclipse detection settings.
getDefaultEclipseDetectionSettings() - Static method in class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel: Define default detection settings for eclipses.
getDefaultEclipseDetectionSettings() - Static method in class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel: Define default detection settings for eclipses.
getDefaultEventDetectionSettings() - Static method in class org.orekit.propagation.events.EventDetectionSettings: Returns default settings for event detections.
getDefaultEventDetectionSettings(Field<T>) - Static method in class org.orekit.propagation.events.FieldEventDetectionSettings: Returns default settings for event detections.
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.
getDefaultTleGenerationAlgorithm(TimeScale, Frame) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the default TLE generation algorithm.
getDefaultToleranceProvider(double) - Static method in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder: Get a default tolerance provider.
getDefaultToleranceProvider(double) - Static method in class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder: Get a default tolerance provider.
getDefaultToleranceProvider(double) - Static method in interface org.orekit.propagation.ToleranceProvider: Defines a default tolerance provider.
getDefaultVersion() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter: Get the default format version.
getDefaultVersion() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter: Get the default format version.
getDefaultYawRate(int) - Static method in class org.orekit.gnss.attitude.GPSBlockIIA: Get the default yaw rate for a satellite.
getDefinedTimeSystem() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage: Get the time system defined by this message.
getDegree() - Method in class org.orekit.bodies.SexagesimalAngle: Get degree part of the angle.
getDelaunayMultipliers() - Method in class org.orekit.models.earth.displacement.Tide: Get the multipliers for Delaunay arguments (l, l', F, D, Ω).
getDelay() - Method in class org.orekit.models.earth.troposphere.FieldTroposphericDelay: Get the total slanted delay (m).
getDelay() - Method in class org.orekit.models.earth.troposphere.TroposphericDelay: Get the total slanted delay (m).
getDelayShift() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the calibration delay shift.
getDeltaClockC0() - Method in class org.orekit.gnss.metric.messages.common.ClockCorrection: Get the delta clock C0.
getDeltaClockC1() - Method in class org.orekit.gnss.metric.messages.common.ClockCorrection: Get the delta clock C1.
getDeltaClockC2() - Method in class org.orekit.gnss.metric.messages.common.ClockCorrection: Get the delta clock C2.
getDeltai() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac: Get Δi.
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.adm.apm.Maneuver: Get mass change during maneuver.
getDeltaMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: Get mass change.
getDeltaMass() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver: Get mass change during maneuver (value is < 0).
getDeltaN() - Method in class org.orekit.gnss.rflink.gps.SubFrame2: Get Δn.
getDeltaN0() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Getter for the delta of satellite mean motion.
getDeltaN0() - Method in class org.orekit.propagation.analytical.gnss.data.FieldAbstractNavigationMessage: Getter for the delta of satellite mean motion.
getDeltaN0() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements: Getter for the delta of satellite mean motion.
getDeltaN0() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Getter for the delta of satellite mean motion.
getDeltaN0Dot() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for change rate in Δn₀.
getDeltaN0Dot() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Getter for change rate in Δn₀.
getDeltaN0Dot() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for change rate in Δn₀.
getDeltaN0Dot() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Getter for change rate in Δn₀.
getDeltaN0Dot() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements: Getter for change rate in Δn₀.
getDeltaN0Dot() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Getter for change rate in Δn₀.
getDeltaOrbitAlongTrack() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection: Get the along-track orbit correction for broadcast ephemeris.
getDeltaOrbitCrossTrack() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection: Get the cross-track orbit correction for broadcast ephemeris.
getDeltaOrbitRadial() - Method in class org.orekit.gnss.metric.messages.common.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.
getDeltaTLs() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get ΔtLS field.
getDeltaTLsf() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get ΔtLSF field.
getDeltaTN() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the deltaTauN value.
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(int) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00.FieldOutput: Get one of the stored densities.
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(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester: Get the local density.
getDensity(Vector3D, Vector3D) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester: Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere: Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.DTM2000: 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(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.JB2008: Get the local density.
getDensity(AbsoluteDate, Vector3D, 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 interface org.orekit.models.earth.atmosphere.Atmosphere: Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, 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.HarrisPriester: Get the local density at some position.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, 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.NRLMSISE00: Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
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.
getDensityForecastUncertainty() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata: Get the atmospheric density forecast error.
getDeployDirSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: Get one σ angular off-nominal deployment vector direction.
getDeployDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: Get velocity increment of deployed "child" object.
getDeployDvCda() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: 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.OrbitManeuver: Get ratio of child-to-host ΔV vectors.
getDeployDvSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: Get one σ percent error on deployment ΔV magnitude.
getDeployId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: Get identifier of resulting "child" object deployed from this host.
getDeployMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: 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() - Method in class org.orekit.time.TimeStampedDoubleAndDerivative: Get time 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.
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.
getDerivative2TargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedFieldPVCoordinates<T>, Frame) - Method in class org.orekit.attitudes.GroundPointTarget: Get a target vector.
getDerivative2TargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedFieldPVCoordinates<T>, Frame) - Method in interface org.orekit.attitudes.TargetProvider: Get a target vector.
getDerivative2TargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedPVCoordinates, Frame) - Method in class org.orekit.attitudes.GroundPointTarget: Get a target vector.
getDerivative2TargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedPVCoordinates, Frame) - Method in interface org.orekit.attitudes.TargetProvider: Get a target vector.
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.
getDescription() - Method in class org.orekit.files.sinex.SinexBias: Get the bias description.
getDesignator() - Method in class org.orekit.files.rinex.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.
getDetectionSettings() - Method in class org.orekit.control.indirect.adjoint.cost.ControlSwitchDetector
getDetectionSettings() - Method in class org.orekit.control.indirect.adjoint.cost.FieldControlSwitchDetector
getDetectionSettings() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver: Getter for the settings.
getDetectionSettings() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Getter for the settings.
getDetectionSettings() - Method in class org.orekit.propagation.events.AbstractDetector: Getter for the settings.
getDetectionSettings() - Method in interface org.orekit.propagation.events.DetectorModifier: Getter for the settings.
getDetectionSettings() - Method in interface org.orekit.propagation.events.EventDetector: Getter for the settings.
getDetectionSettings() - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter: Getter for the settings.
getDetectionSettings() - Method in class org.orekit.propagation.events.EventShifter: Getter for the settings.
getDetectionSettings() - Method in class org.orekit.propagation.events.EventSlopeFilter
getDetectionSettings() - Method in class org.orekit.propagation.events.FieldAbstractDetector: Getter for the settings.
getDetectionSettings() - Method in interface org.orekit.propagation.events.FieldDetectorModifier: Getter for the settings.
getDetectionSettings() - Method in interface org.orekit.propagation.events.FieldEventDetector: Getter for the settings.
getDetectionSettings() - Method in class org.orekit.propagation.events.FieldEventEnablingPredicateFilter: Getter for the settings.
getDetectionSettings() - Method in class org.orekit.propagation.events.FieldEventShifter
getDetectionSettings() - Method in class org.orekit.propagation.events.FieldEventSlopeFilter
getDetector() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver: Getter for wrapped detector.
getDetector() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Get the wrapped detector.
getDetector() - Method in class org.orekit.forces.maneuvers.trigger.FieldManeuverTriggerDetector
getDetector() - Method in class org.orekit.forces.maneuvers.trigger.ManeuverTriggerDetector
getDetector() - Method in class org.orekit.propagation.events.AdapterDetector: Deprecated.

Get the wrapped detector.
getDetector() - Method in interface org.orekit.propagation.events.DetectorModifier: 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.FieldAdapterDetector: Deprecated.

Get the wrapped detector.
getDetector() - Method in interface org.orekit.propagation.events.FieldDetectorModifier: Getter for wrapped detector.
getDetector() - Method in class org.orekit.propagation.events.FieldEventEnablingPredicateFilter: Get the wrapped raw detector.
getDetector() - Method in class org.orekit.propagation.events.FieldEventShifter: Get the detector for the raw unshifted event.
getDetector() - Method in class org.orekit.propagation.events.FieldEventSlopeFilter: Get the wrapped raw detector.
getDetector() - Method in class org.orekit.propagation.events.FieldNegateDetector
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.
getDetector() - Method in class org.orekit.propagation.events.NegateDetector
getDetectorChannel() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the detector channel.
getDetectorChannel() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement: Get the detector channel.
getDetectorChannel() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement: Get the detector channel.
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.
getDetectorRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Get detector configuration record related to the systemRecord.
getDetectors() - Method in class org.orekit.propagation.events.BooleanDetector: Get the list of original detectors.
getDetectors() - Method in class org.orekit.propagation.events.FieldBooleanDetector: Get the list of original detectors.
getDetectorType() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the detector type.
getDeterminationMethod() - Method in class org.orekit.files.sinex.BiasDescription: Get the determination mode used to generate the bias results.
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.control.indirect.adjoint.CartesianAdjointDerivativesProvider: Getter for the dimension.
getDimension() - Method in class org.orekit.control.indirect.adjoint.FieldCartesianAdjointDerivativesProvider: Getter for the dimension.
getDimension() - Method in interface org.orekit.control.indirect.shooting.propagation.AdjointDynamicsProvider: Getter for adjoint dimension.
getDimension() - Method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProvider: Getter for adjoint dimension.
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 interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider: 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.
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.
getDirection(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the direction.
getDirection(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the thrust direction in S/C 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.common.PhaseBias: Get the signal phase discontinuity counter.
getDisplacements() - Method in class org.orekit.estimation.measurements.GroundStation: Get the displacement models.
getDistance() - Method in class org.orekit.bodies.LoxodromeArc: Compute the distance of the arc along the surface of the ellipsoid.
getDistanceThreshold() - Method in class org.orekit.propagation.events.FieldRelativeDistanceDetector: Get the relative distance threshold.
getDistanceThreshold() - Method in class org.orekit.propagation.events.RelativeDistanceDetector: Get the relative distance threshold.
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).
getDn() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get DN field.
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.OrbitPhysicalProperties: Get the other space objects this object is docked to.
getDoi() - Method in class org.orekit.files.rinex.section.RinexBaseHeader: Getter for the Digital Object Information.
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.
getDormandPrince54IntegratorSettings(double, double, ToleranceProvider) - Static method in class org.orekit.control.indirect.shooting.propagation.ShootingIntegrationSettingsFactory: Returns shooting integration settings according to the Dormand Prince 5(4) scheme.
getDormandPrince853IntegratorSettings(double, double, ToleranceProvider) - Static method in class org.orekit.control.indirect.shooting.propagation.ShootingIntegrationSettingsFactory: Returns shooting integration settings according to the Dormand Prince 8(53) scheme.
getDotOrbitDeltaAlongTrack() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection: Get the velocity of along-track orbit correction for broadcast ephemeris.
getDotOrbitDeltaCrossTrack() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection: Get the velocity of cross-track orbit correction for broadcast ephemeris.
getDotOrbitDeltaRadial() - Method in class org.orekit.gnss.metric.messages.common.OrbitCorrection: Get the velocity of radial orbit correction for broadcast ephemeris.
getDrag() - Method in class org.orekit.forces.Panel: Get drag coefficient.
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.adm.acm.AttitudePhysicalProperties: Get the drag coefficient.
getDragCoefficient() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: Get the nominal drag coefficient.
getDragCoefficient() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current DragCoefficientTerm value.
getDragCoefficient() - Method in class org.orekit.files.iirv.IIRVVector: Gets the drag coefficient term.
getDragConstantArea() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: 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.OrbitPhysicalProperties: Get the drag coefficient 1σ uncertainty.
getDrivers() - Method in class org.orekit.utils.ParameterDriversList: Get delegating drivers for all parameters.
getDrivers(double, Orbit, PositionAngleType) - Method in enum org.orekit.orbits.OrbitType: Get parameters drivers initialized from a reference orbit.
getDryMass() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties: Get the mass without propellant.
getDryMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: Get the mass without propellant.
getDsb() - Method in class org.orekit.files.sinex.SatelliteDifferentialSignalBias: Get the DSB data for the current satellite.
getDsb(SatelliteSystem) - Method in class org.orekit.files.sinex.StationDifferentialSignalBias: Get the DSB data for a given satellite system.
getDSDensityWrtState(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.drag.AbstractDragForceModel: Compute density and its derivatives.
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() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader.LineParameters: Get the DSTDTC parameter.
getDSTDTC(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData: Get the temperature change computed from Dst index.
getDSTDTC(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Get the temperature change computed from Dst index.
getDuration() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver: Get duration.
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.OrbitManeuver: 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.
getDut1() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage: Get the ΔUT₁.
getDUT1() - Method in class org.orekit.frames.EOPFittedModel: Get the fitted secular and harmonics model for DUT1/LOD.
getDut1Dot() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage: Get the ΔUT₁ first derivative.
getDut1DotDot() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage: Get the ΔUT₁ second derivative.
getDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: 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.OrbitManeuver: Get one σ angular off-nominal ΔV direction.
getDvMagSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: 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.
getDx() - Method in class org.orekit.frames.EOPFittedModel: Get the fitted secular and harmonics model for nutation x component.
getDy() - Method in class org.orekit.frames.EOPEntry: Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getDy() - Method in class org.orekit.frames.EOPFittedModel: Get the fitted secular and harmonics model for nutation y component.
getE() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements: Get the orbit eccentricity.
getE() - Method in class org.orekit.gnss.rflink.gps.SubFrame2: Get e.
getE() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac: Get 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.FieldGnssOrbitalElements: Get 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 class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Get 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.
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 interface org.orekit.utils.FieldTimeStampedCache: Get the earliest entry in this cache.
getEarliest() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the earliest entry in this cache.
getEarliest() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache: Get the earliest entry in this cache.
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.
getEarliestEpoch() - Method in class org.orekit.files.rinex.clock.RinexClock: Get earliest epoch from the clock data.
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.
getEarthOrientationParameters() - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get the Earth orientation parameters.
getEarthquakeDate() - Method in class org.orekit.models.earth.displacement.PsdCorrection: Get earthquake date.
getEarthTides() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get Enum YesNoUnknown that indicates if Earth and ocean tides are taken into account or not.
getEast() - Method in class org.orekit.bodies.FieldGeodeticPoint: Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.bodies.GeodeticPoint: Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.frames.TopocentricFrame: Get the east direction of topocentric frame, expressed in parent shape frame.
getEastLongitudeDegrees() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator: Get the computed satellite's east longitude.
getEastLongitudeDegrees() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator: Get the computed satellite's east longitude.
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.rinex.observation.RinexObservationHeader: Get the eccentricities of antenna center.
getEccentricities() - Method in class org.orekit.gnss.antenna.FrequencyPattern: Get the phase center eccentricities.
getEccentricities(RadioWave) - Method in class org.orekit.gnss.antenna.Antenna: Get the phase center eccentricities.
getEccentricities(AbsoluteDate) - Method in class org.orekit.files.sinex.Station: Get the station antenna eccentricities for the given epoch.
getEccentricitiesTimeSpanMap() - Method in class org.orekit.files.sinex.Station: Get the TimeSpanMap of site antenna eccentricities.
getEccentricity() - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the first eccentricity of the ellipsoid: e = sqrt(f * (2.0 - f)).
getEccentricitySquared() - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the first eccentricity squared of the ellipsoid: e^2 = f * (2.0 - f).
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.FieldGnssPropagator: 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.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.FieldGnssPropagator: Gets the Earth Centered Inertial frame used to propagate the orbit.
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.
getEclipseConditionsDetector() - Method in class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel: Retrieve detectors finding entries and exits in different eclipse zones.
getEclipseConditionsDetector() - Method in class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel: Retrieve detectors finding entries and exits in different eclipse zones.
getEclipseConditionsDetector() - Method in interface org.orekit.forces.radiation.LightFluxModel: Retrieve detectors finding entries and exits in different eclipse zones.
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.
getEDriver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Get the driver for the eccentricity.
getEffectName() - Method in interface org.orekit.estimation.measurements.EstimationModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.gnss.AbstractWindUp: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.AberrationModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockOnBoardRangeRateModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticJ2ClockModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.Bias: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersGroundReceiverBaseModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersInterSatellitesBaseModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersOneWayGNSSBaseModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.TDOAIonosphericDelayModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.TDOATroposphericDelayModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier: Get the name of the effect modifying the measurement.
getEffectName() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier: Get the name of the effect modifying the measurement.
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.adm.acm.AttitudeState: Get attitude elements.
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() - Method in class org.orekit.utils.FieldTrackingCoordinates: Get the elevation.
getElevation() - Method in class org.orekit.utils.TrackingCoordinates: Get the elevation.
getElevation(double) - Method in class org.orekit.utils.ElevationMask: Get the interpolated elevation for a given azimuth according to the mask.
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(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame: Get the elevation of a point with regards to the local point.
getElevation(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationExtremumDetector: Get the elevation value.
getElevation(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector: Get the elevation value.
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.
getEmitter() - Method in class org.orekit.estimation.measurements.gnss.AmbiguityDriver: Get emitter id.
getEmitterStation() - Method in class org.orekit.estimation.measurements.BistaticRange: Get the emitter ground station.
getEmitterStation() - Method in class org.orekit.estimation.measurements.BistaticRangeRate: Get the emitter ground station.
getEn() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS E_n Word.
getEncounterFrame() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Get encounter local orbital frame.
getEncounterFrame() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Get encounter local orbital frame.
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() - Method in class org.orekit.files.rinex.clock.RinexClock.ReferenceClock: Getter for the validity period end date.
getEndDate() - Method in class org.orekit.files.sinex.ParseInfo: Get end date.
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(GnssSignal) - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults: Return the end date at the given frequency.
getEndEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the ending epoch (UTC).
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination: Get the endpoints (i.e. frames A, B and their relationship).
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata: Get the endpoints (i.e. frames A, B and their relationship).
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get the endpoints (i.e. frames A, B and their relationship).
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity: Get the endpoints (i.e. frames A, B and their relationship).
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion: Get the endpoints (i.e. frames A, B and their relationship).
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler: Get the endpoints (i.e. frames A, B and their relationship).
getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Get the endpoints (i.e. frames A, B and their relationship).
getEndTime() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver: Get end time of actual maneuver, relative to t₀.
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.DataDictionary: Get a complete entry.
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.
getEntry(String) - Method in class org.orekit.utils.FieldDataDictionary: Get a complete entry.
getEnum(String) - Static method in enum org.orekit.files.ccsds.ndm.cdm.Maneuvrable: Get the enum entry corresponding to the given String.
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 interface org.orekit.frames.EOPBasedTransformProvider: Get the EOP history.
getEOPHistory() - Method in class org.orekit.frames.GTODProvider: Get the EOP history.
getEOPHistory() - Method in class org.orekit.time.UT1Scale: 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(IERSConventions, boolean) - Method in class org.orekit.frames.LazyLoadedFrames: Get Earth Orientation Parameters history.
getEOPHistory(IERSConventions, boolean, TimeScales) - Method in class org.orekit.frames.LazyLoadedEop: Get Earth Orientation Parameters history.
getEOPHistoryWithoutCachedTidalCorrection() - Method in class org.orekit.frames.EOPHistory: Get version of the instance that does not cache tidal correction.
getEopLoader(ITRFVersion) - Method in class org.orekit.files.sinex.Sinex: Get the parsed EOP data.
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.
getEphemeris(int) - Method in class org.orekit.files.sp3.SP3: Get an ephemeris.
getEphemeris(String) - Method in class org.orekit.files.sp3.SP3: Get an ephemeris.
getEphemerisData() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisMessage: Get the ephemeris data contain in the ephemeris message.
getEphemerisGenerator() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in interface org.orekit.propagation.FieldPropagator: Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisGenerator() - Method in interface org.orekit.propagation.Propagator: Set up an ephemeris generator that will monitor the propagation for building an ephemeris from it once completed.
getEphemerisNames() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for external ephemeris names for participants.
getEphemerisType() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Get the ephemeris type.
getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the type of ephemeris.
getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the type of ephemeris.
getEphemName() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the unique name of the external ephemeris used for OD.
getEpoch() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData: 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.rinex.clock.RinexClock.ClockDataLine: Get data line epoch.
getEpoch() - Method in class org.orekit.files.sinex.Station: Get the coordinates reference epoch.
getEpoch() - Method in class org.orekit.files.sp3.SP3Header: 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.models.earth.GeoMagneticField: Returns the epoch for this magnetic field model.
getEpoch() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements: Get the elements epoch.
getEpoch() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements: Get the elements epoch.
getEpoch(TimeScale) - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine: Get data line epoch.
getEpochDelayCorrection() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration: Get the epoch delay correction.
getEpochEigenInt() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get positional error ellipsoid 1σ intermediate eigenvalue at the epoch of OD.
getEpochEigenMaj() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get positional error ellipsoid 1σ major eigenvalue at the epoch of OD.
getEpochEigenMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get positional error ellipsoid 1σ minor eigenvalue at the epoch of OD.
getEpochEvent() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement: Get the indicator for the time event reference.
getEpochIdentifier() - Method in class org.orekit.files.ilrs.CRDHeader: Get the epoch identifier.
getEpochIgnition() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver: Get epoch ignition.
getEpochInterval() - Method in class org.orekit.files.sp3.SP3Header: 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.adm.acm.AcmMetadata: Get the epoch to which all relative times are referenced in data blocks.
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.
getEpochTime1s() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader: Get the Epoch Time 1s.
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.
getEpochToc() - Method in class org.orekit.propagation.analytical.gnss.data.FieldAbstractNavigationMessage: Getter for the time of clock epoch.
getEpsilon() - Method in class org.orekit.control.indirect.adjoint.cost.FieldPenalizedCartesianFuelCost: Getter for the penalty weight epsilon.
getEpsilon() - Method in class org.orekit.control.indirect.adjoint.cost.PenalizedCartesianFuelCost: Getter for the penalty weight epsilon.
getEpsilon() - Method in class org.orekit.propagation.conversion.averaging.converters.FixedPointOsculatingToAveragedConverter: Getter for the convergence threshold.
getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the equatorial radius of the body.
getEquatorialRadius() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder: Get the central body equatorial radius.
getEquatorialRadius() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter: Get the central body equatorial radius.
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.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.
getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the first component of the equinoctial eccentricity vector.
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.
getEquinoctialEx() - Method in class org.orekit.orbits.Orbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialExDot() - Method in class org.orekit.orbits.Orbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the second component of the equinoctial eccentricity vector.
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.
getEquinoctialEy() - Method in class org.orekit.orbits.Orbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEyDot() - Method in class org.orekit.orbits.Orbit: Get the second component of the equinoctial eccentricity vector derivative.
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.
getERD(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame4C: Get an Estimated Range Deviation.
getEstimate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the current corrected estimate.
getEstimate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: 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.AbstractKalmanEstimator: 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.SemiAnalyticalKalmanModel: Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the list of estimated measurements parameters.
getEstimatedMeasurementsWithoutDerivatives() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement: Get the underlying estimated measurements without derivatives.
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.
getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the list of estimated orbital 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.
getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: 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.
getEstimatedPropagator() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the propagator estimated with the values set in the propagator builder.
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.EstimatedMeasurementBase: Get the estimated value.
getEta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext: Get the eta value.
getEta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext: Get the eta 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.acm.AttitudeDetermination: Get the rotation order for Euler angles.
getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata: Get the rotation order for Euler angles.
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.
getEventDetectionSettings() - Method in class org.orekit.control.indirect.adjoint.cost.CartesianFuelCost: Getter for event detection settings.
getEventDetectionSettings() - Method in class org.orekit.control.indirect.adjoint.cost.FieldCartesianFuelCost: Getter for event detection settings.
getEventDetectionSettings() - Method in class org.orekit.control.indirect.adjoint.cost.FieldQuadraticPenaltyCartesianFuel: Getter for the event detection settings.
getEventDetectionSettings() - Method in class org.orekit.control.indirect.adjoint.cost.QuadraticPenaltyCartesianFuel: Getter for the event detection settings.
getEventDetectionSettings() - Method in class org.orekit.forces.radiation.AbstractSolarLightFluxModel: Getter for eclipse event detection settings used for eclipses.
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.
getEventDetectors() - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider: Get the discrete events related to the model.
getEventDetectors() - Method in interface org.orekit.attitudes.AttitudeProvider: Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.attitudes.AttitudesSequence
getEventDetectors() - Method in class org.orekit.attitudes.AttitudesSwitcher
getEventDetectors() - Method in class org.orekit.control.indirect.adjoint.cost.BoundedCartesianEnergy: Get the detectors needed for propagation.
getEventDetectors() - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost: Get the detectors needed for propagation.
getEventDetectors() - Method in class org.orekit.control.indirect.adjoint.cost.CartesianFuelCost: Get the detectors needed for propagation.
getEventDetectors() - Method in class org.orekit.control.indirect.adjoint.cost.QuadraticPenaltyCartesianFuel: Get the detectors needed for propagation.
getEventDetectors() - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergy: Get the detectors needed for propagation.
getEventDetectors() - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergyNeglectingMass: Get the detectors needed for propagation.
getEventDetectors() - Method in class org.orekit.forces.drag.TimeSpanDragForce: Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.empirical.AbstractParametricAcceleration: Get the discrete events related to the model.
getEventDetectors() - Method in interface org.orekit.forces.ForceModel: Get the discrete events related to the model.
getEventDetectors() - Method in interface org.orekit.forces.ForceModelModifier: Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.maneuvers.Maneuver: Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel: Get the discrete events related to the model.
getEventDetectors() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel: Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger: Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger: Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.forces.radiation.RadiationPressureModel: Get the discrete events related to the model.
getEventDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Get all the events detectors that have been added.
getEventDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Get all the events detectors that have been added.
getEventDetectors() - Method in interface org.orekit.propagation.events.EventDetectorsProvider: Get the discrete events related to the model.
getEventDetectors() - Method in interface org.orekit.propagation.FieldPropagator: Get all the events detectors that have been added.
getEventDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get all the events detectors that have been added.
getEventDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get all the events detectors that have been added.
getEventDetectors() - Method in interface org.orekit.propagation.Propagator: Get all the events detectors that have been added.
getEventDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the discrete events related to the model.
getEventDetectors() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Get the discrete events related to the model.
getEventDetectors(List<ParameterDriver>) - Method in interface org.orekit.attitudes.AttitudeProviderModifier: Get the discrete events related to the model from a list of ParameterDriver
getEventDetectors(List<ParameterDriver>) - Method in interface org.orekit.propagation.events.EventDetectorsProvider: Get the discrete events related to the model from a list of ParameterDriver
getEventFlag() - Method in class org.orekit.files.rinex.observation.ObservationDataSet: Get the event flag.
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.
getEvolution() - Method in class org.orekit.models.earth.displacement.PsdCorrection: Get time evolution.
getEvolution(double, RealVector[], MeasurementDecorator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
getEvolution(double, RealVector[], MeasurementDecorator) - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel
getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.KalmanModel
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.
getExhaustVelocity(double) - Static method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Method computing the effective exhaust velocity from the specific impulse.
getExponent() - Method in class org.orekit.utils.units.PowerTerm: Get the fractional exponent.
getExternalClockReference() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the external clock reference.
getExternalFrame() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints: 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.time.AbstractFieldTimeInterpolator: Get the extrapolation threshold.
getExtrapolationThreshold() - Method in class org.orekit.time.AbstractTimeInterpolator: Get the extrapolation threshold.
getExtrapolationThreshold() - Method in interface org.orekit.time.FieldTimeInterpolator: Get the extrapolation threshold.
getExtrapolationThreshold() - Method in interface org.orekit.time.TimeInterpolator: Get the extrapolation threshold.
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.
getF() - Method in class org.orekit.orbits.WalkerConstellation: Get the phasing parameter.
getF10() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters: Get the value of the instantaneous solar flux index (1e^-22*Watt/(m²*Hertz)).
getF10(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData: Get the value of the instantaneous solar flux index (1e^-22*Watt/(m²*Hertz)).
getF10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Get the value of the instantaneous solar flux index (1e^-22*Watt/(m²*Hertz)).
getF107() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters: Get the F10.0 flux.
getF107() - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickItu: Get solar flux.
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() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters: Get the value of the mean solar flux.
getF10B(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData: Get the value of the mean solar flux.
getF10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Get the value of the mean solar flux.
getFactoryKey() - Method in class org.orekit.frames.FactoryManagedFrame: Get the key of the frame within the factory.
getFallbackHostOrIPAddress() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Get the fallback host or IP address.
getFallbackPort() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Get the fallback port number.
getFDot() - Method in class org.orekit.data.DelaunayArguments: Get L - Ω where L is the mean longitude of the Moon time derivative.
getFDot() - Method in class org.orekit.data.FieldDelaunayArguments: Get L - Ω where L is the mean longitude of the Moon time derivative.
getField() - Method in class org.orekit.orbits.FieldOrbit: Getter for Field.
getField() - Method in class org.orekit.propagation.FieldAbstractPropagator: Field getter.
getField() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData: Get field.
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.
getField() - Method in class org.orekit.utils.FieldDataDictionary: Get the field to which elements belong.
getField(int) - Method in class org.orekit.gnss.metric.ntrip.Record: Get one field from the parsed sourcetable.
getField(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame: Get a field.
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
getFieldAcceleration(FieldAbsoluteDate<T>, T[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm: Compute the acceleration vector.
getFieldAcceleration(FieldAbsoluteDate<T>, T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm: Compute the acceleration vector.
getFieldAcceleration(FieldAbsoluteDate<T>, T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term: Compute the acceleration vector.
getFieldAcceleration(FieldAbsoluteDate<T>, T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointKeplerianTerm: Compute the acceleration vector.
getFieldAcceleration(FieldAbsoluteDate<T>, T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointSingleBodyTerm: Compute the acceleration vector.
getFieldAcceleration(FieldAbsoluteDate<T>, T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointThirdBodyTerm: Compute the acceleration vector.
getFieldAdjointVelocityNorm(T[]) - Method in class org.orekit.control.indirect.adjoint.cost.AbstractCartesianCost: Computes the Euclidean norm of the adjoint velocity vector.
getFieldAdjointVelocityNorm(T[]) - Method in class org.orekit.control.indirect.adjoint.cost.FieldAbstractCartesianCost: Computes the Euclidean norm of the adjoint velocity vector.
getFieldAuxiliaryElements() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldForceModelContext: Method to get the auxiliary elementsrelated to the ForceModelContext.
getFieldBodyPosition(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm: Get body's position.
getFieldDate() - Method in interface org.orekit.frames.FieldStaticTransform: Get the Field date.
getFieldDate() - Method in class org.orekit.frames.FieldTransform: Get the date.
getFieldDateDetector(Field<T>, TimeStamped...) - Method in interface org.orekit.propagation.events.EventDetectorsProvider: Method building dates' detector.
getFieldDensity(FieldSpacecraftState<T>) - Method in class org.orekit.forces.drag.AbstractDragForceModel: Evaluate the Field density.
getFieldEclipseConditionsDetector(Field<T>) - Method in class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel: Retrieve Field detectors finding entries and exits in different eclipse zones.
getFieldEclipseConditionsDetector(Field<T>) - Method in class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel: Retrieve Field detectors finding entries and exits in different eclipse zones.
getFieldEclipseConditionsDetector(Field<T>) - Method in interface org.orekit.forces.radiation.LightFluxModel: Retrieve Field detectors finding entries and exits in different eclipse zones.
getFieldEventDetectors(Field<S>) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger: Get the discrete events related to the model.
getFieldEventDetectors(Field<S>) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in interface org.orekit.attitudes.AttitudeProvider: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.attitudes.AttitudesSequence
getFieldEventDetectors(Field<T>) - Method in class org.orekit.attitudes.AttitudesSwitcher
getFieldEventDetectors(Field<T>) - Method in class org.orekit.control.indirect.adjoint.cost.FieldBoundedCartesianEnergy: Get the detectors needed for propagation.
getFieldEventDetectors(Field<T>) - Method in interface org.orekit.control.indirect.adjoint.cost.FieldCartesianCost: Get the detectors needed for propagation.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.control.indirect.adjoint.cost.FieldCartesianFuelCost: Get the detectors needed for propagation.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.control.indirect.adjoint.cost.FieldQuadraticPenaltyCartesianFuel: Get the detectors needed for propagation.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.control.indirect.adjoint.cost.FieldUnboundedCartesianEnergy: Get the detectors needed for propagation.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.drag.TimeSpanDragForce: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.empirical.AbstractParametricAcceleration: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in interface org.orekit.forces.ForceModel: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in interface org.orekit.forces.ForceModelModifier: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.Maneuver: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.forces.radiation.RadiationPressureModel: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in interface org.orekit.propagation.events.EventDetectorsProvider: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Get the discrete events related to the model.
getFieldEventDetectors(Field<T>, List<ParameterDriver>) - Method in interface org.orekit.attitudes.AttitudeProviderModifier: Get the discrete events related to the model from a list of ParameterDriver
getFieldEventDetectors(Field<T>, List<ParameterDriver>) - Method in interface org.orekit.propagation.events.EventDetectorsProvider: Get the discrete events related to the model from a list of ParameterDriver
getFieldHamiltonianContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm: Computes the contribution to the Hamiltonian.
getFieldHamiltonianContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in interface org.orekit.control.indirect.adjoint.CartesianAdjointEquationTerm: Computes the contribution to the Hamiltonian.
getFieldHamiltonianContribution(T[], T) - Method in interface org.orekit.control.indirect.adjoint.cost.FieldCartesianCost: Computes the Hamiltonian contribution to the cost function.
getFieldHamiltonianContribution(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.FieldCartesianFlightDurationCost: Computes the Hamiltonian contribution to the cost function.
getFieldHamiltonianContribution(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.FieldCartesianFuelCost: Computes the Hamiltonian contribution to the cost function.
getFieldHamiltonianContribution(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.FieldPenalizedCartesianFuelCost: Computes the Hamiltonian contribution to the cost function.
getFieldHamiltonianContribution(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.FieldUnboundedCartesianEnergyNeglectingMass: Computes the Hamiltonian contribution to the cost function.
getFieldImpulseProvider() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver: Getter for the impulse provider.
getFieldIntegratorBuilder(Field<T>) - Method in interface org.orekit.control.indirect.shooting.propagation.ShootingIntegrationSettings: Returns a Field ODE integrator builder based on an explicit Runge Kutta scheme.
getFieldNewtonianAcceleration(T[]) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNewtonianTerm: Compute the Newtonian acceleration.
getFieldNewtonianVelocityAdjointContribution(T[], T[]) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNewtonianTerm: Computes the generic term of a Newtonian attraction (central or not).
getFieldOther(Field<T>) - Method in class org.orekit.frames.encounter.AbstractEncounterLOF: Get the field version of other's position and velocity coordinates.
getFieldOther(Field<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF: Get other's position and velocity coordinates.
getFieldRatesContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm: Computes the contribution to the rates of the adjoint variables.
getFieldRatesContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointGravitationalTerm: Computes the contribution to the rates of the adjoint variables.
getFieldRatesContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in interface org.orekit.control.indirect.adjoint.CartesianAdjointEquationTerm: Computes the contribution to the rates of the adjoint variables.
getFieldRatesContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm: Computes the contribution to the rates of the adjoint variables.
getFieldsNumber() - Method in class org.orekit.gnss.metric.ntrip.Record: Get the number of fields.
getFieldStep(Field<T>) - Method in class org.orekit.propagation.conversion.AbstractFixedStepFieldIntegratorBuilder: Get "fielded" step size (s).
getFieldThrustAccelerationVector(T[], T) - Method in interface org.orekit.control.indirect.adjoint.cost.FieldCartesianCost: Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getFieldThrustAccelerationVector(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.FieldCartesianFlightDurationCost: Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getFieldThrustAccelerationVector(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.FieldCartesianFuelCost: Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getFieldThrustAccelerationVector(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.FieldLogarithmicBarrierCartesianFuel: Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getFieldThrustAccelerationVector(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.FieldQuadraticPenaltyCartesianFuel: Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getFieldThrustAccelerationVector(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.FieldUnboundedCartesianEnergyNeglectingMass: Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getFieldThrustDirection(T[]) - Method in class org.orekit.control.indirect.adjoint.cost.FieldPenalizedCartesianFuelCost: Computes the direction of thrust.
getFieldThrustForceNorm(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.FieldBoundedCartesianEnergy: Computes the Euclidean norm of the thrust force.
getFieldThrustForceNorm(T[], T) - Method in class org.orekit.control.indirect.adjoint.cost.FieldUnboundedCartesianEnergy: Computes the Euclidean norm of the thrust force.
getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements: Returns the magnetic field vector in Tesla.
getFiftiesEpoch() - Method in class org.orekit.time.AbstractTimeScales
getFiftiesEpoch() - Method in interface org.orekit.time.TimeScales: Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
getFiftiesEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
getFileDate() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters: Get the file date.
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.
getFileEpochEndTime() - Method in class org.orekit.files.sinex.AbstractSinex: Get the file epoch end time.
getFileEpochStartTime() - Method in class org.orekit.files.sinex.AbstractSinex: Get the file epoch start time.
getFileFormat() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser: Get the file format of the last message parsed.
getFileFormat() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser: Get the file format of the last message parsed.
getFileName() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the name of the file.
getFileType() - Method in class org.orekit.files.rinex.section.RinexBaseHeader: Get the file type.
getFilter() - Method in class org.orekit.files.sp3.SP3Header: Get the derivatives filter.
getFilter() - Method in class org.orekit.propagation.events.EventSlopeFilter: Deprecated.
since 13.0 (use getFilterType)
getFilter() - Method in class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator: Get Filter defining if only the state covariance value are used or if first or/and second Keplerian derivatives should be used.
getFilter() - Method in class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator: Get the filter for derivatives from the sample to use in interpolation.
getFilter() - Method in class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator: Get filter for derivatives from the sample to use in interpolation.
getFilter() - Method in class org.orekit.utils.TimeStampedAngularCoordinatesHermiteInterpolator: Get filter for derivatives from the sample to use in interpolation.
getFilter() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinatesHermiteInterpolator: Get filter for derivatives from the sample to use in interpolation.
getFilter() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinatesHermiteInterpolator: filter for derivatives from the sample to use in interpolation.
getFilter() - Method in class org.orekit.utils.TimeStampedPVCoordinatesHermiteInterpolator: Get filter for derivatives from the sample to use in interpolation.
getFilter(int) - Static method in enum org.orekit.utils.AngularDerivativesFilter: Get the filter corresponding to a maximum derivation order.
getFilter(int) - Static method in enum org.orekit.utils.CartesianDerivativesFilter: Get the filter corresponding to a maximum derivation order.
getFilteredDataMap() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother: Get the map of the filtered data.
getFilteredDataMap() - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother: Get the map of the filtered data.
getFilterFlag() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement: Get the filter flag.
getFilters() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder: Get the filters to apply to parse tokens.
getFiltersManager() - Method in class org.orekit.data.DataProvidersManager: Get the manager for filters.
getFilterType() - Method in class org.orekit.propagation.events.EventSlopeFilter: Get filter type.
getFilterType() - Method in class org.orekit.propagation.events.FieldEventSlopeFilter: Get filter type.
getFinalPoint() - Method in class org.orekit.bodies.LoxodromeArc: Get the final point of the arc.
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.
getFirst() - Method in class org.orekit.time.FieldTimeStampedPair: Get first time stamped value.
getFirst() - Method in class org.orekit.time.TimeStampedPair: Get first time stamped value.
getFirstFrequencyPhaseHistory() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter: Get the history of phase values of the first frequency.
getFirstKnownLeapSecond() - Method in class org.orekit.time.UTCScale: Get the date of the first known leap second.
getFirstNonNullSpan() - Method in class org.orekit.utils.TimeSpanMap: Get the first (earliest) span with non-null data.
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.TimeSpanEstimatedModel: 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.
getFitInterval() - Method in class org.orekit.gnss.rflink.gps.SubFrame2: Get fit interval.
getFitInterval() - Method in class org.orekit.propagation.analytical.gnss.data.FieldLegacyNavigationMessage: Getter for the fit interval.
getFitInterval() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage: Getter for the fit interval.
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.MultisatStepNormalizer: 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.MultisatStepNormalizer: 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.
getFlags() - Method in class org.orekit.files.rinex.navigation.IonosphereNequickGMessage: Get the disturbance flags.
getFlattening() - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the flattening of the body: f = (a-b)/a.
getFlattening() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder: Get the central body flattening.
getFlattening() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter: Get the central body flattening.
getFlowRate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the flow rate.
getFlowRate() - 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() - 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.AbstractConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(double[]) - 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.ScaledConstantThrustPropulsionModel: 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(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel: 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).
getFlowRate(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel: 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 class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel: 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(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the flow rate at given date.
getFlowRate(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(AbsoluteDate) - 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.AbstractConstantThrustPropulsionModel: Get the flow rate (kg/s).
getFlowRate(T[]) - 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.ScaledConstantThrustPropulsionModel: 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.
getFoF2() - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickParameters: Get F2 layer critical frequency.
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.
getForceModels() - Method in class org.orekit.control.indirect.shooting.propagation.ShootingPropagationSettings: Getter for the force models.
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.
getFormatter() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator: Used to format dates and doubles to string.
getFormatter() - Method in interface org.orekit.files.ccsds.utils.generation.Generator: Used to format dates and doubles to string.
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.files.rinex.clock.RinexClock: Getter for the format version.
getFormatVersion() - Method in class org.orekit.files.rinex.section.RinexBaseHeader: Getter for the format version.
getFormatVersionKey() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter: Get key for format version.
getFormatVersionKey() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter: Get key for format version.
getFormatVersionKey() - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter: Get key for 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() - Method in class org.orekit.bodies.FieldEllipse: Get the defining frame.
getFrame() - Method in class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity: Get frame in which angular velocities are specified.
getFrame() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Inertia: Get frame in which inertia is specified.
getFrame() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver: Get Coordinate system for the torque vector.
getFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).
getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory: Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata: 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.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.iirv.IIRVSegment: Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.iirv.IIRVVector: Returns the Frame associated with the IIRV vector based on its CoordinateSystemTerm.
getFrame() - Method in class org.orekit.files.iirv.terms.CoordinateSystemTerm: Returns the Frame specified within the IIRV using the default data context.
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.rinex.clock.RinexClock: Get the reference frame for the station positions.
getFrame() - Method in class org.orekit.files.sp3.SP3Ephemeris: Get the reference frame.
getFrame() - Method in class org.orekit.files.sp3.SP3Segment: Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
getFrame() - Method in class org.orekit.forces.gravity.J2OnlyPerturbation: Getter for frame.
getFrame() - Method in class org.orekit.frames.OrphanFrame: Get the associated frame.
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: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.gnss.FieldGnssPropagator: Get the frame in which the orbit is propagated.
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.intelsat.FieldIntelsatElevenElementsPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator: 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 class org.orekit.propagation.conversion.averaging.AbstractAveragedOrbitalState: Getter for the reference frame.
getFrame() - Method in interface org.orekit.propagation.conversion.averaging.AveragedOrbitalState: Getter for the reference frame.
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.FieldStateCovariance: Get the covariance 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.propagation.StateCovariance: Get the covariance 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.
getFrame(DataContext) - Method in class org.orekit.files.iirv.IIRVVector: Returns the Frame associated with the IIRV vector based on its CoordinateSystemTerm.
getFrame(DataContext) - Method in class org.orekit.files.iirv.terms.CoordinateSystemTerm: Returns the Frame specified within the IIRV.
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(FieldPVCoordinates<T>) - Method in enum org.orekit.frames.encounter.EncounterLOFType: Get encounter local orbital frame associated to this enum.
getFrame(IERSConventions, boolean, DataContext) - Method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame: Get the frame corresponding to the CCSDS constant.
getFrame(PVCoordinates) - Method in enum org.orekit.frames.encounter.EncounterLOFType: Get encounter local orbital frame associated to this enum.
getFrameA() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints: Get frame A.
getFrameAngvelFrame() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata: Get frame in which angular velocities are specified.
getFrameB() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints: Get frame B.
getFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata: Get epoch of reference frame, if not intrinsic to the definition of the reference frame.
getFrameName() - Method in class org.orekit.files.rinex.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.
getFreeCompsMap() - Method in class org.orekit.utils.AbstractMultipleShooting: Get the map of free state components.
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.
getFrequency() - Method in enum org.orekit.gnss.PredefinedGnssSignal: Get the value of the frequency in Hz.
getFrequency() - Method in interface org.orekit.gnss.RadioWave: Get the value of the frequency in Hz.
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.
getFromLatitude() - Method in class org.orekit.propagation.events.FieldLatitudeRangeCrossingDetector: Get the fixed latitude range to be crossed (radians), lower boundary.
getFromLatitude() - Method in class org.orekit.propagation.events.LatitudeRangeCrossingDetector: Get the fixed latitude range to be crossed (radians), lower boundary.
getFromLongitude() - Method in class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector: Get the fixed longitude range to be crossed (radians), lower boundary.
getFromLongitude() - Method in class org.orekit.propagation.events.LongitudeRangeCrossingDetector: Get the fixed longitude range to be crossed (radians), lower boundary.
getFrozenAttitudeProvider(AttitudeProvider) - Static method in interface org.orekit.attitudes.AttitudeProviderModifier: Wrap the input provider with a new one always returning attitudes with zero rotation rate and acceleration.
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() - Method in interface org.orekit.time.TimeScales: Dummy date at infinity in the future direction.
getFutureInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: 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() - Method in interface org.orekit.time.TimeScales: Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.
getGalileoEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
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.files.rinex.navigation.RinexNavigation: Get all the Galileo navigation messages contained in the file.
getGalileoNavigationMessages(String) - Method in class org.orekit.files.rinex.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() - 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.DSSTGravityContext: Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext: Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext: Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Get direction cosine γ for central body.
getGamma(LagrangianPoints) - Method in class org.orekit.bodies.CR3BPSystem: Get the position of the Lagrangian point in the CR3BP Rotating frame.
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.
getGeh() - Method in class org.orekit.models.earth.troposphere.AzimuthalGradientCoefficients: Get East hydrostatic coefficient.
getGeh() - Method in class org.orekit.models.earth.troposphere.FieldAzimuthalGradientCoefficients: Get East hydrostatic coefficient.
getGeneralEclipseAngles(FieldVector3D<T>, FieldVector3D<T>, T, FieldVector3D<T>, T) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Get the useful angles for eclipse computation.
getGeneralEclipseAngles(Vector3D, Vector3D, double, Vector3D, double) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Get the useful angles for eclipse computation.
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.
getGeneratedMeasurements() - Method in class org.orekit.estimation.measurements.generation.GatheringSubscriber: Get generated measurements.
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.
getGeocentricLatitudeDegrees() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator: Get the computed satellite's geocentric latitude.
getGeocentricLatitudeDegrees() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator: Get the computed satellite's geocentric latitude.
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 TimeStampedCache.getNeighbors(AbsoluteDate) method.
getGew() - Method in class org.orekit.models.earth.troposphere.AzimuthalGradientCoefficients: Get East wet coefficient.
getGew() - Method in class org.orekit.models.earth.troposphere.FieldAzimuthalGradientCoefficients: Get East wet coefficient.
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.
getGlonassChannels() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the list of GLONASS satellite/channel associations.
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.files.rinex.navigation.RinexNavigation: Get all the Glonass navigation messages contained in the file.
getGlonassNavigationMessages(String) - Method in class org.orekit.files.rinex.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 class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockOnBoardRangeRateModifier: Get gravitational constant for main body in signal path vicinity.
getGm() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get gravitational coefficient of attracting body.
getGM() - Method in interface org.orekit.bodies.CelestialBody: Get the attraction coefficient of the 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() - Method in class org.orekit.time.GLONASSDate: Get the Greenwich Mean Sidereal Time.
getGMST(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
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.
getGnh() - Method in class org.orekit.models.earth.troposphere.AzimuthalGradientCoefficients: Get North hydrostatic coefficient.
getGnh() - Method in class org.orekit.models.earth.troposphere.FieldAzimuthalGradientCoefficients: Get North hydrostatic coefficient.
getGnssIod() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData: Get the GNSS IOD.
getGnssIod() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionData: Get the GNSS IOD.
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.
getGnw() - Method in class org.orekit.models.earth.troposphere.AzimuthalGradientCoefficients: Get North wet coefficient.
getGnw() - Method in class org.orekit.models.earth.troposphere.FieldAzimuthalGradientCoefficients: Get North wet coefficient.
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.
getGPSCivilianNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get all the GPS civilian navigation messages contained in the file.
getGPSCivilianNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get the GPS civilian navigation messages for the given satellite Id.
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() - Method in interface org.orekit.time.TimeScales: Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
getGPSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: 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.
getGPSLegacyNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get all the GPS legacy navigation messages contained in the file.
getGPSLegacyNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get the GPS legacy navigation messages for the given satellite Id.
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.
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.SP3Header: Returns the GPS week as contained in the SP3 file.
getGradientCoefficients(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.troposphere.AzimuthalGradientProvider: Get azimuthal asymmetry gradients.
getGradientCoefficients(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ConstantAzimuthalGradientProvider: Get azimuthal asymmetry gradients.
getGradientCoefficients(FieldGeodeticPoint<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature: Get azimuthal asymmetry gradients.
getGradientCoefficients(GeodeticPoint, AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.AzimuthalGradientProvider: Get azimuthal asymmetry gradients.
getGradientCoefficients(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ConstantAzimuthalGradientProvider: Get azimuthal asymmetry gradients.
getGradientCoefficients(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature: Get azimuthal asymmetry gradients.
getGradientConverter() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester: Get the gradient converter related to the analytical orbit propagator.
getGradientDensityWrtState(AbsoluteDate, Frame, FieldVector3D<Gradient>) - Method in class org.orekit.forces.drag.AbstractDragForceModel: Compute density and its derivatives.
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.OrbitManeuverHistoryMetadata: Get the origin of gravitational assist.
getGravityDegree() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get degree of the gravity model.
getGravityDegree() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get degree of the gravity model.
getGravityFields() - Method in class org.orekit.data.CompositeDataContext
getGravityFields() - Method in interface org.orekit.data.DataContext: Get a factory constructing gravity fields based on the auxiliary data in this context.
getGravityFields() - Method in class org.orekit.data.ExceptionalDataContext
getGravityFields() - Method in class org.orekit.data.LazyLoadedDataContext
getGravityFields() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the instance of GravityFields that is called by the static methods of this class.
getGravityModel() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get gravity model name.
getGravityModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get gravity model name.
getGravityOrder() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get order of the gravity model.
getGravityOrder() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get order of the gravity model.
getGridPoints() - Method in class org.orekit.frames.InterpolatingTransformProvider: Get the number of interpolation grid points.
getGridPoints() - Method in class org.orekit.frames.ShiftingTransformProvider: Get the number of interpolation grid points.
getGridPoints(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.
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.
getGroundStationCoordinates(Frame) - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement: Get the station coordinates for a given frame.
getGroundStationPosition(Frame) - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement: Get the station position for a given frame.
getGroupDelayDifference() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Get group delay difference.
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(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) - Method in class org.orekit.frames.AbstractFrames
getGTOD(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames: 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.
getH1CrdString() - Method in class org.orekit.files.ilrs.CRDHeader: Get a string representation of the H1 in the CRD format.
getH2CrdString() - Method in class org.orekit.files.ilrs.CRDHeader: Get a string representation of the H2 in the CRD format.
getH3CrdString() - Method in class org.orekit.files.ilrs.CRDHeader: Get a string representation of the H3 in the CRD format.
getH4CrdString() - Method in class org.orekit.files.ilrs.CRDHeader: Get a string representation of the H4 in the CRD format.
getH5CrdString() - Method in class org.orekit.files.ilrs.CRDHeader: Get a string representation of the H5 in the CRD format.
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. rotation around +Y_ell).
getHalfApertureAlongY() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView: get the FOV half aperture angle for spreading along Y_ell (i.e. rotation around -X_ell).
getHaloOrbitalPeriod(double) - Method in class org.orekit.orbits.RichardsonExpansion: Return the orbital period of the Halo Orbit.
getHamiltonianContribution(double[], double) - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost: Computes the Hamiltonian contribution to the cost function.
getHamiltonianContribution(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.CartesianFlightDurationCost: Computes the Hamiltonian contribution to the cost function.
getHamiltonianContribution(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.CartesianFuelCost: Computes the Hamiltonian contribution to the cost function.
getHamiltonianContribution(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.PenalizedCartesianFuelCost: Computes the Hamiltonian contribution to the cost function.
getHamiltonianContribution(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergyNeglectingMass: Computes the Hamiltonian contribution to the cost function.
getHamiltonianContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm: Computes the contribution to the Hamiltonian.
getHamiltonianContribution(AbsoluteDate, double[], double[], Frame) - Method in interface org.orekit.control.indirect.adjoint.CartesianAdjointEquationTerm: Computes the contribution to the Hamiltonian.
getHandler() - Method in class org.orekit.control.indirect.adjoint.cost.ControlSwitchDetector
getHandler() - Method in class org.orekit.control.indirect.adjoint.cost.FieldControlSwitchDetector
getHandler() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver
getHandler() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Get the handler.
getHandler() - Method in class org.orekit.forces.maneuvers.trigger.FieldManeuverTriggerDetector
getHandler() - Method in class org.orekit.forces.maneuvers.trigger.ManeuverTriggerDetector
getHandler() - Method in class org.orekit.propagation.events.AbstractDetector: Get the handler.
getHandler() - Method in interface org.orekit.propagation.events.DetectorModifier: Get the handler.
getHandler() - Method in interface org.orekit.propagation.events.EventDetector: Get the handler.
getHandler() - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter: Get the handler.
getHandler() - Method in class org.orekit.propagation.events.EventShifter: Get the handler.
getHandler() - Method in class org.orekit.propagation.events.EventSlopeFilter: Get the handler.
getHandler() - Method in class org.orekit.propagation.events.FieldAbstractDetector: Get the handler.
getHandler() - Method in interface org.orekit.propagation.events.FieldDetectorModifier: Get the handler.
getHandler() - Method in interface org.orekit.propagation.events.FieldEventDetector: Get the handler.
getHandler() - Method in class org.orekit.propagation.events.FieldEventEnablingPredicateFilter: Get the handler.
getHandler() - Method in class org.orekit.propagation.events.FieldEventShifter
getHandler() - Method in class org.orekit.propagation.events.FieldEventSlopeFilter
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.
getHarvester() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: 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.
getHbr() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the object hard body radius.
getHdop() - Method in class org.orekit.gnss.DOP: Gets the horizontal dilution of precision.
getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent: Get the header.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser: Get file header to fill.
getHeader() - Method in class org.orekit.files.ilrs.CPF: Get the CPF file header.
getHeader() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the header of the current data block.
getHeader() - Method in class org.orekit.files.rinex.RinexFile: Get the header.
getHeader() - Method in class org.orekit.files.sp3.SP3: Get the header.
getHeader() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionMessage: Get the header.
getHeader() - Method in class org.orekit.gnss.metric.messages.ssr.SsrMessage: Get the header.
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.BeidouCivilianNavigationMessage: Getter for health.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouAlmanac: Gets the Health status.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for health.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGPSAlmanac: Gets the Health status.
getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.FieldQZSSAlmanac: 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.FieldGalileoAlmanac: Gets the E1-B/C signal 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.FieldGalileoAlmanac: Gets the E5a 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.FieldGalileoAlmanac: Gets the E5b signal health status.
getHealthE5b() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac: Gets the E5b signal health status.
getHealthFlags() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Get health flags.
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.
getHmE() - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickParameters: Get the E layer maximum density height.
getHmF1() - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickParameters: Get the F1 layer maximum density height.
getHmF2() - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickParameters: Get the F2 layer maximum density height.
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.
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.DSSTThirdBodyDynamicContext: Get hXXX = h * Χ³.
getHXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: 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.
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.attitudes.FieldInertiaAxis: Get the moment of inertia.
getI() - Method in class org.orekit.attitudes.InertiaAxis: Get the moment of inertia.
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.
getI0() - Method in class org.orekit.gnss.rflink.gps.SubFrame3: Get i₀.
getI0() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements: Get the inclination angle at reference time.
getI0() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Get the inclination angle at reference time.
getI0Driver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Get the driver for the inclination angle at reference time.
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.acm.AcmSatelliteEphemeris: Get the satellite ID.
getId() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination: Get identification number.
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.iirv.IIRVEphemerisFile.IIRVEphemeris: 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.SP3Ephemeris: Get the satellite ID.
getId() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris
getId() - Method in class org.orekit.gnss.metric.ntrip.StreamedMessage: Get message id.
getId() - Method in class org.orekit.gnss.rflink.gps.SubFrame: Get sub-frame id.
getID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver: Get maneuver identification number.
getIdentifier() - Method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter: Get the regular expression for identifying line.
getIdentity() - Static method in interface org.orekit.frames.KinematicTransform: Get the identity kinematic transform.
getIdentity() - Static method in interface org.orekit.frames.StaticTransform: Get the identity static transform.
getIdentity(Field<T>) - Static method in interface org.orekit.frames.FieldKinematicTransform: Get the identity kinematic transform.
getIdentity(Field<T>) - Static method in interface org.orekit.frames.FieldStaticTransform: Get the identity static transform.
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.gnss.rflink.gps.SubFrame3: Get dot(i).
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.GNSSOrbitalElementsDriversProvider: Get rate of inclination angle.
getIDotDriver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get the driver for 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
getIIRV() - Method in class org.orekit.files.iirv.IIRVEphemerisFile: Gets the IIRV message containing the ephemeris data.
getIIRV() - Method in class org.orekit.files.iirv.IIRVEphemerisFile.IIRVEphemeris: Gets the IIRVMessage containing the ephemeris data for this object's IIRVSegment.
getIIRVEphemeris() - Method in class org.orekit.files.iirv.IIRVEphemerisFile: Gets the IIRVEphemerisFile.IIRVEphemeris associated with this file.
getIIRVMessage() - Method in class org.orekit.files.iirv.IIRVSegment: Gets the IIRV message for this segment.
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.
getImpulse(FieldSpacecraftState<T>, boolean) - Method in interface org.orekit.forces.maneuvers.FieldImpulseProvider: Method returning the impulse to be applied (Field version).
getImpulse(SpacecraftState, boolean) - Method in interface org.orekit.forces.maneuvers.ImpulseProvider: Method returning the impulse to be applied.
getImpulseManeuvers() - Method in class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder: Protected getter for the impulse maneuvers.
getImpulseProvider() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Getter for the impulse provider.
getInclination() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the angle between the objects orbit plane and the orbit centers equatorial plane.
getInclination() - Method in class org.orekit.models.earth.GeoMagneticElements: Returns the inclination of the magnetic field in radians.
getIncludeMessageMetadataSetting() - Method in class org.orekit.files.iirv.StreamingIIRVFileWriter: Gets the setting for when message metadata terms appear in the created IIRV message.
getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter: Get the increasing events time shift.
getIncreasingTimeShift() - Method in class org.orekit.propagation.events.FieldEventShifter: Get the increasing events time shift.
getIndicator() - Method in enum org.orekit.files.ilrs.CRDHeader.DataType: Get the data type indicator.
getIndicator() - Method in enum org.orekit.files.ilrs.CRDHeader.RangeType: Get the range type indicator.
getIndices() - Method in class org.orekit.estimation.measurements.CommonParametersWithDerivatives: Get derivatives indices map.
getInertia() - Method in class org.orekit.attitudes.TorqueFree: Get the spacecraft inertia.
getInertiaAxis1() - Method in class org.orekit.attitudes.FieldInertia: Get inertia along first axis.
getInertiaAxis1() - Method in class org.orekit.attitudes.Inertia: Get inertia along first axis.
getInertiaAxis2() - Method in class org.orekit.attitudes.FieldInertia: Get inertia along second axis.
getInertiaAxis2() - Method in class org.orekit.attitudes.Inertia: Get inertia along second axis.
getInertiaAxis3() - Method in class org.orekit.attitudes.FieldInertia: Get inertia along third axis.
getInertiaAxis3() - Method in class org.orekit.attitudes.Inertia: Get inertia along third axis.
getInertiaBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData: Get the inertia logical block.
getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Get the inertial velocity increment of the maneuver.
getInertialFrame() - Method in class org.orekit.attitudes.LofOffset: Get the inertial frame.
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.
getInertialFrame() - Method in class org.orekit.frames.LocalMagneticFieldFrame: Get interlai frame.
getInertialFrame() - Method in class org.orekit.propagation.events.BetaAngleDetector: The inertial frame in which beta angle is computed.
getInertialFrame() - Method in class org.orekit.propagation.events.FieldBetaAngleDetector: The inertial frame in which beta angle is computed.
getInertiallyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody: Get an inertially oriented, body centered frame.
getInertiaMatrix() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties: Get the inertia matrix.
getInertiaMatrix() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Inertia: Get the inertia matrix.
getInertiaMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: Get the inertia matrix.
getInertiaReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties: Get reference frame for inertia.
getInitialAttitude() - Method in class org.orekit.attitudes.TorqueFree: Get the initial attitude.
getInitialCartesianState() - Method in class org.orekit.control.indirect.shooting.boundary.FixedTimeCartesianBoundaryStates: Getter for the initial Cartesian condition.
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: Get the initial flow rate.
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.
getInitialOrbit() - Method in class org.orekit.control.indirect.shooting.boundary.FixedTimeBoundaryOrbits: Getter for the initial condition.
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.control.indirect.shooting.ShootingBoundaryOutput: Getter for the initial state.
getInitialState() - Method in class org.orekit.files.general.EphemerisSegmentPropagator
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: Get the initial thrust vector.
getInitialWetMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: Get the total mass at beginning of life.
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.KalmanModel
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
getInnovation(MeasurementDecorator, RealVector, RealVector, RealMatrix) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
getInnovation(MeasurementDecorator, RealVector, RealVector, RealMatrix) - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel
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.
getIntegrationSettings() - Method in class org.orekit.control.indirect.shooting.propagation.ShootingPropagationSettings: Getter for the integration settings.
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 interface org.orekit.control.indirect.shooting.propagation.ShootingIntegrationSettings: Returns an ODE integrator builder based on an explicit Runge Kutta scheme.
getIntegratorBuilder() - Method in class org.orekit.propagation.conversion.AbstractIntegratedPropagatorBuilder: Getter for integrator builder.
getIntegratorName() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the integrator's name.
getIntegratorName() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get the integrator's name.
getIntegrityFlags() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for B1C integrity flags.
getIntegrityFlags() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for B1C integrity flags.
getIntegrityStatus() - Method in class org.orekit.gnss.rflink.gps.SubFrame: Get integrity status flag.
getIntelsatElevenElements() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator: Get the Intelsat's 11 elements used by the propagator.
getIntelsatElevenElements() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator: Get the Intelsat's 11 elements used by the propagator.
getInternationalDes() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the international designator for the object.
getInternationalDesignator() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata: Get the international designator for the object.
getInternationalDesignator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the international designator for the object.
getInterpMethodEOP() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the interpolation method for Earth Orientation Parameters.
getInterpMethodSW() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get the interpolation method for Space Weather data.
getInterpolatedPoint(double, double) - Method in class org.orekit.models.earth.tessellation.Tile: Get an interpolated point inside the tile.
getInterpolatedState(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Get the state at interpolated date.
getInterpolatedState(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator: Get the state at interpolated date.
getInterpolationDate() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData: Get interpolation date.
getInterpolationDate() - Method in class org.orekit.time.AbstractTimeInterpolator.InterpolationData: Get interpolation 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.
getInterpolationDegree() - Method in class org.orekit.frames.EOPHistory: Get interpolation degree.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory: Get the interpolation method to be used.
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.acm.AttitudeStateHistory: Get the number of samples to use in interpolation.
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.iirv.IIRVSegment: 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.SP3Ephemeris: Get the number of points to use for interpolation.
getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3Segment: Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
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(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(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.
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(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(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.
getInterval() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the observation interval in seconds.
getInterval() - Method in class org.orekit.models.earth.ionosphere.nequick.Segment: Get the integration step.
getIntervalNumber() - Method in class org.orekit.time.GLONASSDate: Get the number of the current four year interval.
getIntrackThrust() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get Enum YesNoUnknown that indicates if intrack thrust modeling was into account or not.
getInverse() - Method in interface org.orekit.frames.FieldKinematicTransform: Get the inverse transform of the instance.
getInverse() - Method in interface org.orekit.frames.FieldStaticTransform: Get the inverse transform of the instance.
getInverse() - Method in class org.orekit.frames.FieldTransform: Get the inverse transform of the instance.
getInverse() - Method in interface org.orekit.frames.KinematicTransform: Get the inverse transform of the instance.
getInverse() - Method in interface org.orekit.frames.StaticTransform: Get the inverse transform of the instance.
getInverse() - Method in class org.orekit.frames.Transform: Get the inverse transform of the instance.
getIOD() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGalileoAlmanac: Gets the Issue of Data (IOD).
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.gnss.rflink.gps.SubFrame1: Get IODC.
getIODC() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for the Issue Of Data Clock (IODC).
getIODC() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for the Issue Of Data Clock (IODC).
getIODC() - Method in class org.orekit.propagation.analytical.gnss.data.FieldLegacyNavigationMessage: Getter for the Issue Of Data Clock (IODC).
getIODC() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage: Getter for the Issue Of Data Clock (IODC).
getIODE() - Method in class org.orekit.gnss.rflink.gps.SubFrame2: Get Issue Of Data (ephemeris).
getIODE() - Method in class org.orekit.gnss.rflink.gps.SubFrame3: Get Issue Of Data (ephemeris).
getIODE() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for the Issue Of Data Ephemeris (IODE).
getIODE() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for the Issue Of Data Ephemeris (IODE).
getIODE() - Method in class org.orekit.propagation.analytical.gnss.data.FieldLegacyNavigationMessage: Getter for the Issue Of Data Ephemeris (IODE).
getIODE() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage: Getter for the Issue Of Data Ephemeris (IODE).
getIODEC() - Method in class org.orekit.propagation.analytical.gnss.data.FieldIRNSSNavigationMessage: Getter for the Issue Of Data Ephemeris and Clock (IODEC).
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.FieldGalileoNavigationMessage: Getter for the the Issue Of Data (IOD).
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.rtcm.correction.RtcmCorrectionHeader: Get the IOD SSR.
getIodSsr() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader: Get the IOD SSR.
getIonoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier: Get the ionospheric delay model.
getIonoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier: Get the ionospheric delay model.
getIonosphereFreeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory: Get the Ionosphere-Free combination of measurements.
getIonosphericCorrectionType() - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader: 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.files.rinex.navigation.RinexNavigation: Get all the IRNSS navigation messages contained in the file.
getIRNSSNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get the IRNSS navigation messages for the given satellite Id.
getIscB1CD() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for inter Signal Delay for B1 CD.
getIscB1CD() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for inter Signal Delay for B1 CD.
getIscB1CP() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for inter Signal Delay for B1 CP.
getIscB1CP() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for inter Signal Delay for B1 CP.
getIscB2AD() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for inter Signal Delay for B2 AD.
getIscB2AD() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for inter Signal Delay for B2 AD.
getIscL1CA() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Getter for inter Signal Delay for L1 C/A.
getIscL1CA() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Getter for inter Signal Delay for L1 C/A.
getIscL1CD() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Getter for inter Signal Delay for L1 CD.
getIscL1CD() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Getter for inter Signal Delay for L1 CD.
getIscL1CP() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Getter for inter Signal Delay for L1 CP.
getIscL1CP() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Getter for inter Signal Delay for L1 CP.
getIscL2C() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Getter for inter Signal Delay for L2 C.
getIscL2C() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Getter for inter Signal Delay for L2 C.
getIscL5I5() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Getter for inter Signal Delay for L5I.
getIscL5I5() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Getter for inter Signal Delay for L5I.
getIscL5Q5() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Getter for inter Signal Delay for L5Q.
getIscL5Q5() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Getter for inter Signal Delay for L5Q.
getIsp() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the specific impulse.
getIsp() - Method in class org.orekit.forces.maneuvers.FieldImpulseManeuver: 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).
getIsp(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the specific impulse at given date.
getIsp(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the specific impulse at given date.
getIteration() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase: Get the iteration number.
getIterationCount() - Method in class org.orekit.control.indirect.shooting.ShootingBoundaryOutput: Getter for 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.
getIterationsNb() - Method in class org.orekit.propagation.conversion.osc2mean.FixedPointConverter: Gets the number of iterations performed by the last conversion.
getIterationsNb() - Method in class org.orekit.propagation.conversion.osc2mean.LeastSquaresConverter: Gets the number of iterations performed by the last conversion.
getITRF(ITRFVersion, IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
getITRF(ITRFVersion, IERSConventions, boolean) - Method in interface org.orekit.frames.Frames: Get an specific International Terrestrial Reference Frame.
getITRF(ITRFVersion, IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get a specific International Terrestrial Reference Frame.
getITRF(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(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get an unspecified International Terrestrial Reference Frame.
getITRFEquinox(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
getITRFEquinox(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames: Get the equinox-based ITRF reference frame.
getITRFEquinox(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the equinox-based ITRF reference frame.
getITRFType() - Method in class org.orekit.frames.EOPEntry: Get the ITRF version this entry defines.
getITRFVersion() - Method in class org.orekit.frames.VersionedITRF: 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(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the ITRF version.
getJ2() - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term: Getter for J2.
getJ2(AbsoluteDate) - Method in class org.orekit.forces.gravity.J2OnlyPerturbation: Return J2 at requested date.
getJ2(FieldAbsoluteDate<T>) - Method in class org.orekit.forces.gravity.J2OnlyPerturbation: Return J2 at requested date (Field 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() - Method in interface org.orekit.time.TimeScales: J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
getJ2000Epoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
getJacobian(Orbit, PositionAngleType, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Compute the Jacobian of the orbit with respect to maneuver parameters.
getJacobian(CartesianDerivativesFilter, double[][]) - Method in class org.orekit.frames.Transform: Compute the Jacobian of the Transform.transformPVCoordinates(PVCoordinates) method of the transform.
getJacobian(CartesianDerivativesFilter, T[][]) - Method in class org.orekit.frames.FieldTransform: Compute the Jacobian of the FieldTransform.transformPVCoordinates(FieldPVCoordinates) 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.gnss.GNSSPropagator: 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 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(PositionAngleType, double[][]) - Method in class org.orekit.orbits.Orbit: Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtCartesian(PositionAngleType, T[][]) - Method in class org.orekit.orbits.FieldOrbit: Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtParameters(PositionAngleType, double[][]) - Method in class org.orekit.orbits.Orbit: Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJacobianWrtParameters(PositionAngleType, T[][]) - Method in class org.orekit.orbits.FieldOrbit: Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJavaEpoch() - Method in class org.orekit.time.AbstractTimeScales
getJavaEpoch() - Method in interface org.orekit.time.TimeScales: Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
getJavaEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
getJD() - Method in class org.orekit.time.AbsoluteDate: Return the given date as a Julian Date expressed in UTC.
getJD() - Method in class org.orekit.time.FieldAbsoluteDate: Return the given date as a Julian Date expressed in UTC.
getJD(TimeScale) - Method in class org.orekit.time.AbsoluteDate: Return the given date as a Julian Date expressed in given timescale.
getJD(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate: Return the given date as a Julian Date expressed in given timescale.
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.
getJulianEpoch() - Method in class org.orekit.time.AbstractTimeScales
getJulianEpoch() - Method in interface org.orekit.time.TimeScales: Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
getJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: 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.files.rinex.observation.GlonassSatelliteChannel: Get the channel frequency multiplier.
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.
getKalmanEstimation() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator: Get the provider for kalman filter estimations.
getKalmanEstimation() - Method in class org.orekit.estimation.sequential.KalmanEstimator: Get the provider for kalman filter estimations.
getKalmanEstimation() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator: Get the provider for kalman filter estimations.
getKalmanEstimation() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimator: Get the provider for kalman filter estimations.
getKalmanEstimation() - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimator: Get the provider for kalman filter estimations.
getKalmanFilter() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator: Get the Hipparchus filter.
getKalmanFilter() - Method in class org.orekit.estimation.sequential.KalmanEstimator: Get the Hipparchus filter.
getKalmanFilter() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator: Get the Hipparchus filter.
getKalmanFilter() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimator: Get the Hipparchus filter.
getKalmanFilter() - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimator: Get the Hipparchus filter.
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.
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.semianalytical.dsst.utilities.AuxiliaryElements: Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the Keplerian period.
getKey() - Method in enum org.orekit.files.rinex.clock.RinexClock.ClockDataType: Get the key for the system.
getKey() - Method in enum org.orekit.files.sp3.DataUsed: Get the key for the data used.
getKey() - Method in enum org.orekit.files.sp3.SP3FileType: Get the key for the file type.
getKey() - Method in enum org.orekit.gnss.SatelliteSystem: Get the key for the system.
getKey() - Method in enum org.orekit.gnss.TimeSystem: Get the 3 letters key of the time system.
getKey() - Method in class org.orekit.utils.DataDictionary.Entry: Get the entry key.
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.
getKey() - Method in class org.orekit.utils.FieldDataDictionary.Entry: Get the entry key.
getKinematicTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider: Get a transform for position and velocity, not acceleration.
getKinematicTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter: Get a transform for position and velocity, not acceleration.
getKinematicTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider: Get a transform for position and velocity, not acceleration.
getKinematicTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider: Get a transform for position and velocity, not acceleration.
getKinematicTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter: Get a transform for position and velocity, not acceleration.
getKinematicTransform(FieldAbsoluteDate<T>) - Method in interface org.orekit.frames.TransformProvider: Get a transform for position and velocity, not acceleration.
getKinematicTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame: Get the kinematic portion of the transform from the instance to another frame.
getKinematicTransformTo(Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.Frame: Get the kinematic portion of the transform from the instance to another frame.
getKlobucharAlpha() - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get the "alpha" ionospheric parameters.
getKlobucharBeta() - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get the "beta" ionospheric parameters.
getKlobucharMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get the ionosphere Klobuchar messages.
getKpSum() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters: Gets the sum of all eight Kp indices for the current entry.
getKurtosis() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the kurtosis of raw system delay values from the mean.
getKurtosis() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics: Get the session kurtosis from the mean of raw accepted time-of-flight values minus the trend function.
getKXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext: Get kXXX = h * Χ³.
getKXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: 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(PositionAngleType) - Method in class org.orekit.orbits.EquinoctialOrbit: Get the longitude argument.
getL(PositionAngleType) - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the longitude argument.
getL2PDataFlag() - Method in class org.orekit.gnss.rflink.gps.SubFrame1: Get L2 P data flag.
getLabel() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame: Get the frame label.
getLabel() - Method in enum org.orekit.files.rinex.section.RinexLabels: Get the first label.
getLabel(String) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils: Get the trimmed label from a header line.
getLagrangianPoint() - Method in class org.orekit.orbits.RichardsonExpansion: Get the considered lagrangian point.
getLambda() - Method in class org.orekit.models.earth.weather.FieldPressureTemperatureHumidity: Get water vapor decrease factor.
getLambda() - Method in class org.orekit.models.earth.weather.PressureTemperatureHumidity: Get water vapor decrease factor.
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.
getLaserRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Get laser configuration record related to the systemRecord.
getLaserType() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Get the laser type.
getLast() - Static method in enum org.orekit.frames.ITRFVersion: Get last supported ITRF version.
getLastDailyPredictedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader: Gets the day (at data start) of the last daily data entry.
getLastEstimations() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Get the last estimations performed.
getLastKnownLeapSecond() - Method in class org.orekit.time.UTCScale: Get the date of the last known leap second.
getLastNonNullSpan() - Method in class org.orekit.utils.TimeSpanMap: Get the last (latest) span with non-null data.
getLastObservedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader: Gets the day (at data start) of the last observed data entry.
getLastOccurrence() - Method in class org.orekit.propagation.events.handlers.FieldRecallLastOccurrence: Getter for last occurrence.
getLastOccurrence() - Method in class org.orekit.propagation.events.handlers.RecallLastOccurrence: Getter for last occurrence.
getLastSpan() - Method in class org.orekit.utils.TimeSpanMap: Get the last (latest) span.
getLastSystemRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration: Get the system configuration record.
getLastTransition() - Method in class org.orekit.utils.TimeSpanMap: Get the last (latest) transition.
getLatC() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements: Get the latitude oscillation-amplitude for the cosine term.
getLatC() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements: Get the latitude oscillation-amplitude for the cosine term.
getLatC1() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements: Get the rate of change of latitude, for the cosine term.
getLatC1() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements: Get the rate of change of latitude, for the cosine term.
getLatest() - Method in interface org.orekit.utils.FieldTimeStampedCache: Get the latest entry in this cache.
getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the latest entry in this cache.
getLatest() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache: Get the latest entry in this cache.
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.
getLatestEpoch() - Method in class org.orekit.files.rinex.clock.RinexClock: Get latest epoch from the clock data.
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.models.earth.ionosphere.nequick.Ray: Get the ray-perigee 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).
getLatS() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements: Get the latitude oscillation-amplitude for the sine term.
getLatS() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements: Get the latitude oscillation-amplitude for the sine term.
getLatS1() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements: Get the rate of change of latitude, for the sine term.
getLatS1() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements: Get the rate of change of latitude, for the sine term.
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.OdmCommonMetadata: 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.
getLaunchNumber(String) - Method in class org.orekit.files.ccsds.section.Metadata: 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.OdmCommonMetadata: 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.
getLaunchPiece(String) - Method in class org.orekit.files.ccsds.section.Metadata: Get the piece of launch.
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.OdmCommonMetadata: 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.
getLaunchYear(String) - Method in class org.orekit.files.ccsds.section.Metadata: Get the launch year.
getLayerAmplitudes() - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickParameters: Get the F2, F1 and E layer amplitudes.
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(PositionAngleType) - Method in class org.orekit.orbits.EquinoctialOrbit: Get the longitude argument derivative.
getLDot(PositionAngleType) - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the longitude argument derivative.
getLe() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the eccentric longitude.
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.
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() - Method in class org.orekit.time.UTCTAIOffset: Get the value of the leap at offset validity start.
getLeap(AbsoluteDate) - 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(AbsoluteDate) - Method in class org.orekit.time.UTCScale: 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(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale: Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale: Get the value of the previous leap.
getLeapSeconds() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the Number of leap seconds since 6-Jan-1980.
getLeapSecondsDayNum() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the respective leap second day number.
getLeapSecondsFuture() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the future or past leap seconds.
getLeapSecondsWeekNum() - Method in class org.orekit.files.rinex.observation.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.
getLicense() - Method in class org.orekit.files.rinex.section.RinexBaseHeader: Getter for the license of use.
getLiftRatio() - Method in class org.orekit.forces.Panel: Get drag lift ratio.
getLightFluxModel() - Method in class org.orekit.forces.radiation.RadiationPressureModel: Getter for light flux model.
getLightFluxVector(FieldSpacecraftState<T>) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel: Get the light flux vector in the state's frame.
getLightFluxVector(FieldSpacecraftState<T>) - Method in interface org.orekit.forces.radiation.LightFluxModel: Get the light flux vector in the state's frame.
getLightFluxVector(SpacecraftState) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel: Get the light flux vector in the state's frame.
getLightFluxVector(SpacecraftState) - Method in interface org.orekit.forces.radiation.LightFluxModel: Get the light flux vector in the state's frame.
getLightingRatio(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel: Get the lighting ratio ([0-1]).
getLightingRatio(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel: Get the lighting ratio ([0-1]).
getLightingRatio(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel: Get the lighting ratio ([0-1]).
getLightingRatio(Vector3D, Vector3D) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel: Get the lighting ratio ([0-1]).
getLightingRatio(Vector3D, Vector3D) - Method in class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel: Get the lighting ratio ([0-1]).
getLightingRatio(Vector3D, Vector3D) - Method in class org.orekit.forces.radiation.CylindricallyShadowedLightFluxModel: Get the lighting ratio ([0-1]).
getLightingRatio(FieldSpacecraftState<T>) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel: Get the lighting ratio ([0-1]).
getLightingRatio(FieldSpacecraftState<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get the lighting ratio ([0-1]).
getLightingRatio(SpacecraftState) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel: Get the lighting ratio ([0-1]).
getLightingRatio(SpacecraftState) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get the lighting ratio ([0-1]).
getLimbRadius() - Method in class org.orekit.utils.OccultationEngine.FieldOccultationAngles: Get limb radius in occulting/occulted plane.
getLimbRadius() - Method in class org.orekit.utils.OccultationEngine.OccultationAngles: Get limb radius in occulting/occulted plane.
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.
getLine2CheckSum() - Method in class org.orekit.files.iirv.IIRVVector: Gets the checksum value for line 2.
getLine3CheckSum() - Method in class org.orekit.files.iirv.IIRVVector: Gets the checksum term for line 3.
getLine4CheckSum() - Method in class org.orekit.files.iirv.IIRVVector: Gets the checksum value for line 4 term.
getLine5CheckSum() - Method in class org.orekit.files.iirv.IIRVVector: Gets the checksum term for line 5.
getLinearInterpolation(AbstractSolarActivityData.LocalSolarActivity, Function<L, Double>) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData: Performs a linear interpolation between two values The weights are computed from the time delta between previous date, current date, next date.
getLinearInterpolation(AbsoluteDate, Function<L, Double>) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData: Performs a linear interpolation between two values The weights are computed from the time delta between previous date, current date, next date.
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.files.rinex.section.RinexComment: Get the line number.
getListAppliedDCBS() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the applied differential code bias corrections.
getListAppliedDCBS() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the list of applied differential code bias corrections.
getListAppliedPCVS() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the applied phase center variations.
getListAppliedPCVS() - Method in class org.orekit.files.rinex.observation.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(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(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(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState, AuxiliaryElements) - 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(SpacecraftState, AuxiliaryElements) - 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.semianalytical.dsst.utilities.AuxiliaryElements: Get the mean longitude.
getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the mean longitude.
getLm0() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements: Get the mean longitude (East of Greenwich).
getLm0() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements: Get the mean longitude (East of Greenwich).
getLm1() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements: Get the drift rate.
getLm1() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements: Get the drift rate.
getLm2() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements: Get the drift acceleration.
getLm2() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements: Get the drift acceleration.
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
getLocalOffset() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithDerivatives: Get local clock offset.
getLocalOffset() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithoutDerivatives: Get local clock offset.
getLocalRate() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithDerivatives: Get local clock rate.
getLocalRate() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithoutDerivatives: Get local clock rate.
getLocalTimingId() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration: Get the local timing system configuration ID.
getLocation() - Method in class org.orekit.gnss.DOP: Gets the location with respect to the Earth where DOP was calculated.
getLod() - Method in class org.orekit.files.sinex.SinexEopEntry: Get the length of day.
getLOD() - Method in class org.orekit.frames.EOPEntry: Get the LoD (Length of Day) value.
getLOD(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the LoD (Length of Day) value.
getLOD(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory: Get the LoD (Length of Day) value.
getLof() - Method in class org.orekit.attitudes.LofOffset: Get the local orbital frame.
getLOF() - Method in class org.orekit.propagation.FieldStateCovariance: Get the covariance LOF type.
getLOF() - Method in class org.orekit.propagation.StateCovariance: Get the covariance LOF type.
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.
getLonC() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements: Get the longitude oscillation-amplitude for the cosine term.
getLonC() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements: Get the longitude oscillation-amplitude for the cosine term.
getLonC1() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements: Get the rate of change of longitude, for the cosine term.
getLonC1() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements: Get the rate of change of longitude, for the cosine term.
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.models.earth.ionosphere.nequick.Ray: Get the ray-perigee longitude.
getLongitude() - Method in class org.orekit.propagation.events.FieldLongitudeCrossingDetector: Get the fixed longitude to be crossed (radians).
getLongitude() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector: Get the fixed longitude to be crossed (radians).
getLonS() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements: Get the longitude oscillation-amplitude for the sine term.
getLonS() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements: Get the longitude oscillation-amplitude for the sine term.
getLonS1() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElements: Get the rate of change of longitude, for the sine term.
getLonS1() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElements: Get the rate of change of longitude, for the sine term.
getLossOfLockIndicator() - Method in class org.orekit.files.rinex.observation.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.CanonicalSaastamoinenModel: Get the low elevation threshold value for path delay computation.
getLowElevationThreshold() - Method in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel: 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.
getLowercaseOmega() - Method in class org.orekit.gnss.rflink.gps.SubFrame3: Get ω.
getLowercaseOmega() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac: Get ω.
getLowerLimit() - Method in class org.orekit.ssa.metrics.FieldProbabilityOfCollision: Get lower limit of the probability of collision value.
getLowerLimit() - Method in class org.orekit.ssa.metrics.ProbabilityOfCollision: Get lower limit of the probability of collision value.
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.
getLutherIntegratorSettings(double) - Static method in class org.orekit.control.indirect.shooting.propagation.ShootingIntegrationSettingsFactory: Returns shooting integration settings according to the Luther Runge Kutta scheme.
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.semianalytical.dsst.utilities.AuxiliaryElements: Get the true longitude.
getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the true longitude.
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.gnss.rflink.gps.SubFrame2: Get M₀.
getM0() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac: Get M₀.
getM0() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements: Get mean anomaly at reference time.
getM0() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Get mean anomaly at reference time.
getM0Driver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Get the driver for 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.
getM2(AbsoluteDate) - 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.DSSTThirdBodyDynamicContext: Get m2aoA = -2 * a / A.
getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Get m2aoA = -2 * a / A.
getM2Value() - Method in class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder: Get the value of the M2 parameter.
getMagneticField() - Method in class org.orekit.frames.LocalMagneticFieldFrame: Get geomagnetid field.
getMahalanobisDistance() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the Mahalanobis Distance.
getMainStateDerivativesIncrements() - Method in class org.orekit.propagation.integration.CombinedDerivatives: Get the derivatives increments related to the main state.
getMainStateDerivativesIncrements() - Method in class org.orekit.propagation.integration.FieldCombinedDerivatives: Get the derivatives increments related to the main state.
getMainStateEquations(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(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator: Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: 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).
getManagedAdditionalData() - Method in class org.orekit.propagation.AbstractPropagator: Get all the names of all managed additional data.
getManagedAdditionalData() - Method in class org.orekit.propagation.analytical.Ephemeris: Get all the names of all managed additional data.
getManagedAdditionalData() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get all the names of all managed data.
getManagedAdditionalData() - Method in interface org.orekit.propagation.FieldPropagator: Get all the names of all managed data.
getManagedAdditionalData() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get all the names of all managed additional data.
getManagedAdditionalData() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get all the names of all managed data.
getManagedAdditionalData() - Method in interface org.orekit.propagation.Propagator: Get all the names of all managed additional data.
getManBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get basis of this maneuver history data.
getManBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: 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.OrbitManeuverHistoryMetadata: Get maneuver elements of information.
getManDeviceID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get identifier of the device used for this maneuver.
getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData: Get a maneuver.
getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Get a maneuver.
getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData: Get a maneuver.
getManeuverable() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the ability of object to maneuver or not.
getManeuverBlocks() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData: Get maneuvers logical blocks.
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.OrbitManeuverHistory: 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.OrbitPhysicalProperties: 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.OrbitPhysicalProperties: Get the average number of orbit or attitude maneuvers per year.
getManeuverTriggers() - Method in class org.orekit.forces.maneuvers.Maneuver: Get the maneuver triggers.
getManeuverTriggersParameters(double[]) - Method in class org.orekit.forces.maneuvers.Maneuver: Extract maneuver triggers' parameters from the parameters' array called in by the ForceModel interface.
getManeuverTriggersParameters(T[]) - Method in class org.orekit.forces.maneuvers.Maneuver: Extract maneuver triggers' parameters from the parameters' array called in by the ForceModel interface.
getManFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get epoch of the maneuver reference frame.
getManID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: 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.OrbitManeuverHistoryMetadata: Get start time of next maneuver.
getManNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get identification number of next maneuver.
getManPredSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get prediction source on which this maneuver is based.
getManPrevEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get completion time of previous maneuver.
getManPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get identification number of previous maneuver.
getManPurpose() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver: Get purpose of maneuver.
getManPurpose() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get the purposes of the maneuver.
getManReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get reference frame of the maneuver.
getManufacturer() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: Get manufacturer name.
getManUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadata: Get maneuver elements of information units.
getMapFilters() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother: Get the map storing the filters for each observation type.
getMapFilters() - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother: Get the map storing the filters for each observation type.
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.EclipseDetector: Get the angular margin used for eclipse detection.
getMargin() - Method in class org.orekit.propagation.events.FieldEclipseDetector: Get the angular margin used for eclipse detection.
getMargin() - Method in class org.orekit.propagation.events.GeographicZoneDetector: Get the angular margin to apply (radians).
getMarkerName() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get name of the antenna marker.
getMarkerNumber() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get number of the antenna marker.
getMarkerType() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get type of the antenna marker.
getMars() - Method in interface org.orekit.bodies.CelestialBodies: Get the Mars singleton body.
getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Mars singleton body.
getMars() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
getMass() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the mass of the object.
getMass() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData: Get the mass.
getMass() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData: Get the mass.
getMass() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters: Get the spacecraft mass.
getMass() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current MassTerm value.
getMass() - Method in class org.orekit.files.iirv.IIRVVector: Gets the mass term.
getMass() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the mass.
getMass() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Get the initial mass.
getMass() - Method in class org.orekit.propagation.FieldSpacecraftState: Gets the current 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.
getMass(AbsoluteDate) - Method in class org.orekit.files.general.EphemerisSegmentPropagator
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(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.intelsat.IntelsatElevenElementsPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: 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(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.gnss.FieldGnssPropagator: Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator: Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Get the mass.
getMassDepletionDelay() - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate: Get the mass depletion effect processor.
getMassDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel: Get the mass derivative (i.e. flow rate in kg/s) during maneuver.
getMassDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the mass derivative (i.e. flow rate in kg/s) during maneuver.
getMassDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel: Get the mass derivative (i.e. flow rate in kg/s) during maneuver.
getMassDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel: Get the mass derivative (i.e. flow rate in kg/s) during maneuver.
getMassFlowRateFactor() - Method in class org.orekit.control.indirect.adjoint.cost.AbstractCartesianCost: Getter for mass flow rate factor.
getMassFlowRateFactor() - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost: Getter for mass flow rate factor.
getMassFlowRateFactor() - Method in class org.orekit.control.indirect.adjoint.cost.FieldAbstractCartesianCost: Getter for mass flow rate factor.
getMassFlowRateFactor() - Method in interface org.orekit.control.indirect.adjoint.cost.FieldCartesianCost: Getter for mass flow rate factor.
getMassFlowRateFactor() - Method in class org.orekit.control.indirect.adjoint.cost.FieldUnboundedCartesianEnergyNeglectingMass: Getter for mass flow rate factor.
getMassInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator: Get mass interpolator.
getMassInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator: Get mass interpolator.
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.adm.acm.AttitudeCovariance: Get the covariance matrix.
getMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovariance: Get the covariance matrix.
getMatrix() - Method in class org.orekit.propagation.FieldStateCovariance: Get the covariance matrix.
getMatrix() - Method in class org.orekit.propagation.StateCovariance: Get the covariance matrix.
getMatrixDecomposer() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator: Get the matrix decomposer.
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.DSSTThirdBodyStaticContext: Get the value of max power for a/R3 in the serie expansion.
getMaxAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: Get the maximum cross-sectional area for collision probability estimation purposes.
getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Get the maximal degree available in the last file parsed.
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.OceanTidesReader: Get the maximal order 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.EventDetectionSettings: Getter for adaptable interval.
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.FieldEventDetectionSettings: Getter for adaptable interval.
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.
getMaxCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get max collision probability.
getMaxCollisionProbabilityMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get max collision probability method.
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.files.general.EphemerisSegmentPropagator
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData: Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader: Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader: Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData: Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader: Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters: Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters: Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
getMaxDate() - Method in class org.orekit.propagation.analytical.Ephemeris: Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator: Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator: Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Get the last date of the range.
getMaxDate() - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider: 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.DSSTThirdBodyStaticContext: Get the value of max power for e in the serie expansion.
getMaxFreqF() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyStaticContext: Get the value of max frequency of F.
getMaximumIterationCount() - Method in class org.orekit.control.indirect.shooting.AbstractFixedInitialCartesianSingleShooting: Returns the maximum number of iterations.
getMaximumIterationCount() - Method in interface org.orekit.control.indirect.shooting.boundary.CartesianBoundaryConditionChecker: Returns the maximum number of iterations.
getMaximumIterationCount() - Method in class org.orekit.control.indirect.shooting.boundary.NormBasedCartesianConditionChecker: Returns the maximum number of iterations.
getMaximumIterationCount() - Method in class org.orekit.control.indirect.shooting.NewtonFixedBoundaryCartesianSingleShooting
getMaximumObsGap() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get maximum time between observations in the OD of the object.
getMaximumThrustMagnitude() - Method in class org.orekit.control.indirect.adjoint.cost.BoundedCartesianEnergy: Getter for maximum thrust magnitude.
getMaximumThrustMagnitude() - Method in class org.orekit.control.indirect.adjoint.cost.CartesianFlightDurationCost: Getter for maximum thrust magnitude.
getMaximumThrustMagnitude() - Method in class org.orekit.control.indirect.adjoint.cost.CartesianFuelCost: Getter for maximum thrust magnitude.
getMaximumThrustMagnitude() - Method in class org.orekit.control.indirect.adjoint.cost.FieldBoundedCartesianEnergy: Getter for maximum thrust magnitude.
getMaximumThrustMagnitude() - Method in class org.orekit.control.indirect.adjoint.cost.FieldCartesianFlightDurationCost: Getter for maximum thrust magnitude.
getMaximumThrustMagnitude() - Method in class org.orekit.control.indirect.adjoint.cost.FieldCartesianFuelCost: Getter for maximum thrust magnitude.
getMaximumThrustMagnitude() - Method in class org.orekit.control.indirect.adjoint.cost.FieldPenalizedCartesianFuelCost: Getter for maximum thrust magnitude.
getMaximumThrustMagnitude() - Method in class org.orekit.control.indirect.adjoint.cost.PenalizedCartesianFuelCost: Getter for maximum thrust magnitude.
getMaximumValidDateForObservation(ObservationType) - Method in class org.orekit.files.sinex.ObservableSpecificSignalBias: Get the maximum valid date for a given observation type.
getMaximumValidDateForObservationPair(ObservationType, ObservationType) - Method in class org.orekit.files.sinex.DifferentialSignalBias: Get the maximum valid date for a given observation pair.
getMaxIterationCount() - Method in class org.orekit.propagation.events.EventDetectionSettings: Getter for max iter.
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.FieldEventDetectionSettings: Getter for max iter.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.FieldEventDetector: Get maximal number of iterations in the event time search.
getMaxIterations() - Method in class org.orekit.propagation.conversion.averaging.converters.FixedPointOsculatingToAveragedConverter: Getter for the maximum number of iterations.
getMaxIterations() - Method in class org.orekit.propagation.conversion.osc2mean.FixedPointConverter: Gets maximum number of iterations.
getMaxIterations() - Method in class org.orekit.propagation.conversion.osc2mean.LeastSquaresConverter: Gets the maximum number of iterations.
getMaxNeighborsSize() - Method in interface org.orekit.utils.FieldTimeStampedCache: Get the fixed size of the lists returned by FieldTimeStampedCache.getNeighbors(FieldAbsoluteDate).
getMaxNeighborsSize() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the maximum size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate, int).
getMaxNeighborsSize() - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache: Get the fixed size of the lists returned by FieldTimeStampedCache.getNeighbors(FieldAbsoluteDate).
getMaxNeighborsSize() - Method in class org.orekit.utils.ImmutableTimeStampedCache: Get the maximum size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate, int).
getMaxNeighborsSize() - Method in interface org.orekit.utils.TimeStampedCache: Get the maximum size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate, int).
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.CommonPhysicalProperties: 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.
getMaxStep() - Method in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder: Getter for the maximum step.
getMaxStep() - Method in class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder: Getter for the maximum step.
getMaxThrust() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: 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.DSSTThirdBodyDynamicContext: Get mCo2AB = -C / 2AB.
getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: 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.
getMeanAnomalyDotWrtA() - Method in class org.orekit.orbits.FieldOrbit: Get the derivative of the mean anomaly with respect to the semi major axis.
getMeanAnomalyDotWrtA() - Method in class org.orekit.orbits.Orbit: Get the derivative of the mean anomaly with respect to the semi major axis.
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(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(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(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm: 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(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(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(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: 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(SpacecraftState, AuxiliaryElements, double[]) - 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(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm: 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(SpacecraftState, AuxiliaryElements, double[]) - 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(SpacecraftState, AuxiliaryElements, double[]) - 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.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.DSSTGravityContext: Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext: 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.FieldDSSTGravityContext: Get the Keplerian mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: 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.
getMeanMotion0() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGnssOrbitalElements: Get the computed mean motion n₀.
getMeanMotion0() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Get the computed mean motion n₀.
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.
getMeanTheory() - Method in class org.orekit.propagation.conversion.osc2mean.FixedPointConverter: Gets the theory defining the mean orbit.
getMeanTheory() - Method in class org.orekit.propagation.conversion.osc2mean.LeastSquaresConverter: Gets the theory defining the mean orbit.
getMeanTheory() - Method in interface org.orekit.propagation.conversion.osc2mean.OsculatingToMeanConverter: Gets the theory defining the mean orbit.
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.estimation.measurements.gnss.CombinedObservationData: Get the measurement type.
getMeasurementType() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Get the type of measurement.
getMeasurementType() - Method in interface org.orekit.gnss.ObservationType: Get the measurement type.
getMeasurementType() - Method in enum org.orekit.gnss.PredefinedObservationType: 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
getMergedFiles() - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader: Getter for the number of merged files.
getMessage() - Method in exception org.orekit.errors.OrekitException
getMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
getMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
getMessage() - Method in exception org.orekit.errors.OrekitInternalError
getMessage() - Method in exception org.orekit.errors.OrekitIOException
getMessage() - Method in exception org.orekit.errors.OrekitParseException
getMessage() - Method in class org.orekit.gnss.rflink.gps.SubFrame: Get telemetry message.
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(Locale) - Method in exception org.orekit.errors.OrekitIllegalArgumentException: Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalStateException: Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitInternalError: Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIOException: Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitParseException: Gets the message in a specified locale.
getMessageClass() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current MessageClassTerm value.
getMessageClass() - Method in class org.orekit.files.iirv.IIRVVector: Gets the message class term.
getMessageEnd() - Method in class org.orekit.files.iirv.IIRVVector: Gets the "ITERM" message end term.
getMessageFor() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmHeader: Get the spacecraft name for which the CDM is provided stored in MESSAGE_FOR key.
getMessageId() - Method in class org.orekit.files.ccsds.section.Header: Get the ID that uniquely identifies a message from a given originator.
getMessageID() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current MessageIDTerm value.
getMessageID() - Method in class org.orekit.files.iirv.IIRVVector: Gets the message ID term.
getMessageSource() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current MessageSourceTerm value.
getMessageSource() - Method in class org.orekit.files.iirv.IIRVVector: Gets the message source term.
getMessageStart() - Method in class org.orekit.files.iirv.IIRVVector: Gets the message start term.
getMessageType() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current MessageTypeTerm value.
getMessageType() - Method in class org.orekit.files.iirv.IIRVVector: Gets the message type term.
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.acm.Acm: Get the metadata from the single segment.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistory: Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory: Get metadata.
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.Ocm: Get the metadata from the single segment.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistory: Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistory: Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory: Get metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm: Get the file metadata.
getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Get the file metadata.
getMetadata() - Method in class org.orekit.files.ccsds.section.Segment: Get the segment metadata.
getMetadataObject1() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm: Get the file metadata.
getMetadataObject2() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm: Get the file metadata.
getMeteo(AbsoluteDate) - Method in class org.orekit.files.ilrs.CRD.Meteo: Get the meteorological parameters at a given date.
getMeteoData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the meteorological data for the data block.
getMeteorologicalId() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration: Get the meteorological configuration ID.
getMeteorologicalRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration: Get the meteorological record.
getMeteorologicalRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Get meteorological configuration record related to the systemRecord.
getMethod() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination: Get attitude determination method.
getMethod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get orbit determination method.
getMethod() - Method in enum org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType: Get probability of collision method.
getMethodType() - Method in enum org.orekit.files.ccsds.definitions.PocMethodType: Get a probability of collision computing method type based on the short term encounter model.
getMidpointIntegratorSettings(double) - Static method in class org.orekit.control.indirect.shooting.propagation.ShootingIntegrationSettingsFactory: Returns shooting integration settings according to the midpoint Runge Kutta scheme.
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.OrbitPhysicalProperties: Get the minimum cross-sectional area for collision probability estimation purposes.
getMinDate() - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
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.files.general.EphemerisSegmentPropagator
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData: Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader: Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.DtcDataLoader: Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData: Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader: Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters: Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters: Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
getMinDate() - Method in class org.orekit.propagation.analytical.Ephemeris: Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.BoundedPropagator: Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator: Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Get the first date of the range.
getMinDate() - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider: 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.
getMinGap() - Method in class org.orekit.propagation.events.DateDetector: Get the minimum gap between added dates.
getMinGap(TimeStamped...) - Static method in class org.orekit.propagation.events.intervals.DateDetectionAdaptableIntervalFactory: Compute min. gap between dated objects if applicable.
getMinimumValidDateForObservation(ObservationType) - Method in class org.orekit.files.sinex.ObservableSpecificSignalBias: Get the minimum valid date for a given observation type.
getMinimumValidDateForObservationPair(ObservationType, ObservationType) - Method in class org.orekit.files.sinex.DifferentialSignalBias: Get the minimum valid date for a given observation pair.
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.CommonPhysicalProperties: Get the minimum radar cross-section.
getMinStep() - Method in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder: Getter for the minimum step.
getMinStep() - Method in class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder: Getter for the minimum step.
getMinute() - Method in class org.orekit.time.TimeComponents: Get the minute number.
getMinutesFromUTC() - Method in class org.orekit.time.TimeComponents: Get the offset between the specified date and UTC.
getMinValue() - Method in class org.orekit.utils.ParameterDriver: Get minimum parameter value.
getMisc() - Method in class org.orekit.gnss.metric.ntrip.Record: Get miscellaneous information.
getMissDistance() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the norm of relative position vector at TCA.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder: Get the mission reference date or Mission Elapsed Time or Mission Relative Time time systems.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.adm.AdmParser: Get reference date for Mission Elapsed Time and Mission Relative Time time systems.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser: Get reference date for Mission Elapsed Time and Mission Relative Time time systems.
getMjd() - Method in class org.orekit.frames.EOPEntry: Get the entry date (modified julian day, 00h00 UTC scale).
getMJD() - Method in class org.orekit.time.AbsoluteDate: Return the given date as a Modified Julian Date expressed in UTC.
getMJD() - Method in class org.orekit.time.DateComponents: Get the modified julian day.
getMJD() - Method in class org.orekit.time.FieldAbsoluteDate: Return the given date as a Modified Julian Date expressed in UTC.
getMJD() - Method in class org.orekit.time.UTCTAIOffset: Get the date of the start of the leap as Modified Julian Day.
getMJD(TimeScale) - Method in class org.orekit.time.AbsoluteDate: Return the given date as a Modified Julian Date expressed in given timescale.
getMJD(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate: Return the given date as a Modified Julian Date expressed in given timescale.
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.FieldDSSTTesseralContext: Deprecated.
since 12.2 Use getMuoa() instead
getMOD(boolean) - Method in class org.orekit.frames.AbstractFrames
getMOD(boolean) - 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) - Method in class org.orekit.frames.AbstractFrames
getMOD(IERSConventions) - Method in interface org.orekit.frames.Frames: 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.
getModels() - Method in class org.orekit.time.AggregatedClockModel: Get the underlying models.
getModifiedJulianDay() - Method in class org.orekit.files.sp3.SP3Header: Returns the modified julian day for this SP3 file.
getModifiedJulianEpoch() - Method in class org.orekit.time.AbstractTimeScales
getModifiedJulianEpoch() - Method in interface org.orekit.time.TimeScales: Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
getModifiedJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: 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 class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder: 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.
getMomentumAlpha() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Get the right ascension of angular momentum vector (rad).
getMomentumDelta() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Get the declination of the angular momentum vector (rad).
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.control.indirect.adjoint.AbstractCartesianAdjointGravitationalTerm: Getter for the gravitational constant.
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.iirv.IIRVEphemerisFile.IIRVEphemeris: Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.iirv.IIRVSegment: 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.SP3Ephemeris: Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.sp3.SP3Segment: Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris
getMu() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
getMu() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.forces.gravity.J2OnlyPerturbation: Getter for mu.
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.FieldGnssOrbitalElements: Get the Earth's universal gravitational parameter.
getMu() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Get the Earth's universal gravitational parameter.
getMu() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the central attraction coefficient (µ - m³/s²) value.
getMu() - Method in interface org.orekit.propagation.conversion.averaging.AveragedOrbitalState: Getter for the central body's gravitational constant.
getMu() - Method in class org.orekit.propagation.conversion.averaging.SGP4OrbitalState: Getter for the central body's gravitational constant.
getMu() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Get the central attraction coefficient (µ - m³/s²) value.
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.FieldAbstractGaussianContributionContext: Get central attraction coefficient.
getMu(Field<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction: Get the central attraction coefficient μ.
getMu(AbsoluteDate) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Get the central attraction coefficient μ.
getMu(AbsoluteDate) - Method in class org.orekit.forces.gravity.NewtonianAttraction: Get the central attraction coefficient μ.
getMu(AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Get the central attraction coefficient μ at specific date.
getMU() - Method in class org.orekit.propagation.analytical.gnss.FieldGnssPropagator: Gets the Earth gravity coefficient used for GNSS propagation.
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.
getMultipleMessageIndicator() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader: Get the Multiple Message Indicator.
getMultiplexedStateIndex(int, int) - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement: Get the spacecraft state index in the multiplexed measurement.
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.DSSTGravityContext: Get μ / a.
getMuoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext: Get muoa = μ / a.
getMuoR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext: Get muoR3 = mu3 / R3.
getMuoR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: 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.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.
getNA() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS N^A Word.
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.control.indirect.adjoint.CartesianAdjointDerivativesProvider: Getter for the name.
getName() - Method in class org.orekit.control.indirect.adjoint.FieldCartesianAdjointDerivativesProvider: Getter for the name.
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.estimation.measurements.ObservableSatellite: Build a name for the satellite.
getName() - Method in class org.orekit.files.ccsds.definitions.BodyFacade: Get the CCSDS name for the body.
getName() - Method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame: Get the name of celestial body frame.
getName() - Method in class org.orekit.files.ccsds.definitions.FrameFacade: Get the CCSDS name for the frame.
getName() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade: Get the name of the method.
getName() - Method in class org.orekit.files.ccsds.definitions.PocMethodFacade: Get the name of the method.
getName() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken: Get the name of the block or entry.
getName() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the satellite target name.
getName() - Method in class org.orekit.files.rinex.clock.RinexClock.ClockDataLine: Getter for the receiver/satellite name.
getName() - Method in class org.orekit.files.sinex.AntennaKey: Get the antenna name.
getName() - Method in class org.orekit.files.sinex.ParseInfo: Get name of data source.
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 data.
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 data.
getName() - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate: Get the name of the additional data.
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 class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel: 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.encounter.DefaultEncounterLOF: Get name of the local orbital frame.
getName() - Method in class org.orekit.frames.encounter.ValsecchiEncounterFrame: Get name of the local orbital frame.
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 class org.orekit.frames.LocalMagneticFieldFrame: Get name of the local orbital frame.
getName() - Method in interface org.orekit.frames.LOF: Get name of the local orbital frame.
getName() - Method in enum org.orekit.frames.LOFType: Get name of the local orbital frame.
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 interface org.orekit.gnss.GnssSignal: Get the RINEX name for the frequency.
getName() - Method in interface org.orekit.gnss.ObservationType: Get the name of the observation type.
getName() - Method in enum org.orekit.gnss.PredefinedGnssSignal: Get the RINEX name for the frequency.
getName() - Method in enum org.orekit.gnss.PredefinedObservationType: Get the name of the observation type.
getName() - Method in class org.orekit.propagation.AbstractStateModifier: Get the name of the additional data.
getName() - Method in interface org.orekit.propagation.AdditionalDataProvider: Get the name of the additional data.
getName() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester: Get the name of the additional data.
getName() - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider: Get the name of the additional data.
getName() - Method in class org.orekit.propagation.analytical.gnss.FieldClockCorrectionsProvider: Get the name of the additional data.
getName() - Method in class org.orekit.propagation.FieldAbstractStateModifier: Get the name of the additional data.
getName() - Method in interface org.orekit.propagation.FieldAdditionalDataProvider: Get the name of the additional data.
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.FieldAdditionalDerivativesProvider: 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.StateCovarianceMatrixProvider: Get the name of the additional data.
getName() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod: Get name of the method.
getName() - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Get name of the method.
getName() - Method in class org.orekit.time.ClockTimeScale: Get the name time scale.
getName() - Method in class org.orekit.time.ConstantOffsetTimeScale: 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.SatelliteClockScale: 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.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 parameter driver general name.
getName() - Method in class org.orekit.utils.units.Unit: Get the name of the unit.
getName(double) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType: Get the type name for a given format version.
getNameSpan(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver: Get name of the parameter span for a specific date.
getNamesSpanMap() - Method in class org.orekit.utils.ParameterDriver: Get current name span map of the parameterDriver, cut in interval in accordance with value span map and validity period.
getNarrowLaneCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory: Get the Narrow-Lane combination of measurements.
getNavigationMessageType() - Method in class org.orekit.files.rinex.navigation.TypeSvMessage: Get navigation message type.
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.
getNbInterpolationPoints() - Method in class org.orekit.time.AbstractFieldTimeInterpolator: Get the number of interpolation points.
getNbInterpolationPoints() - Method in class org.orekit.time.AbstractTimeInterpolator: Get the number of interpolation points.
getNbInterpolationPoints() - Method in interface org.orekit.time.FieldTimeInterpolator: Get the number of interpolation points.
getNbInterpolationPoints() - Method in interface org.orekit.time.TimeInterpolator: Get the number of interpolation points.
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.
getNbObsPerSat() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get an unmodifiable view of the map of number of observations per satellites.
getNBodyPerturbations() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get n-body perturbation bodies.
getNBodyPerturbations() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get n-body perturbation bodies.
getNbOfValues() - Method in class org.orekit.utils.ParameterDriver: Get the number of values to estimate that is to say the number.
getNbParametersDriversValue() - Method in interface org.orekit.utils.ParameterDriversProvider: Get total number of spans for all the parameters driver.
getNbParams() - Method in class org.orekit.utils.ParameterDriversList: Get the number of parameters with different names.
getNbPoints() - Method in class org.orekit.models.earth.ionosphere.nequick.Segment: Get number of points.
getNbSat() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get number of satellites.
getNbSensorNoiseCovariance() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor: Get number of noise elements for sensor.
getNbSpecies() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients: Get the number of species.
getNbStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination: Get number of states for AdMethodType.EKF, AdMethodType.BATCH or AdMethodType.FILTER_SMOOTHER.
getNbStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata: Get the number of data states included (attitude components plus rates components).
getNbTides(int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients: Get the number of tides for one species.
getNbValuesToEstimate() - Method in class org.orekit.utils.ParameterDriversList: Get the number of values to estimate for parameters with different names.
getNdFilterValue() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement: Get the neutral density (ND) filter value.
getNeighborList() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData: Get neighbor list.
getNeighborList() - Method in class org.orekit.time.AbstractTimeInterpolator.InterpolationData: Get neighbor list.
getNeighbors(AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedCache: Get the entries surrounding a central date.
getNeighbors(AbsoluteDate, int) - Method in class org.orekit.frames.EOPHistory: Get the entries surrounding a central date.
getNeighbors(AbsoluteDate, int) - Method in class org.orekit.utils.GenericTimeStampedCache: Get the entries surrounding a central date.
getNeighbors(AbsoluteDate, int) - Method in class org.orekit.utils.ImmutableTimeStampedCache: Get the entries surrounding a central date.
getNeighbors(AbsoluteDate, int) - Method in interface org.orekit.utils.TimeStampedCache: Get the entries surrounding a central date.
getNeighbors(FieldAbsoluteDate<KK>) - Method in interface org.orekit.utils.FieldTimeStampedCache: Get the entries surrounding a central date.
getNeighbors(FieldAbsoluteDate<KK>, int) - Method in interface org.orekit.utils.FieldTimeStampedCache: Get the entries surrounding a central date.
getNeighbors(FieldAbsoluteDate<KK>, int) - Method in class org.orekit.utils.ImmutableFieldTimeStampedCache: Get the entries surrounding a central date.
getNeighborsSize() - Method in class org.orekit.utils.FieldSortedListTrimmer: Get size of the list returned from FieldSortedListTrimmer.getNeighborsSubList(FieldAbsoluteDate, List).
getNeighborsSize() - Method in class org.orekit.utils.SortedListTrimmer: Get size of the list returned from SortedListTrimmer.getNeighborsSubList(AbsoluteDate, List).
getNeighborsSubList(AbsoluteDate, List<T>) - Method in class org.orekit.utils.SortedListTrimmer: Get the entries surrounding a central date.
getNeighborsSubList(FieldAbsoluteDate<K>, List<T>) - Method in class org.orekit.utils.FieldSortedListTrimmer: Get the entries surrounding a central date.
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.files.rinex.navigation.RinexNavigation: Get the "alpha" ionospheric parameters.
getNequickGMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get the ionosphere Nequick-G messages.
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.
getNewtonianAcceleration(double[]) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNewtonianTerm: Compute the Newtonian acceleration.
getNewtonianVelocityAdjointContribution(double[], double[]) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNewtonianTerm: Computes the generic term of a Newtonian attraction (central or not).
getNextLeapEpoch() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata: Get the epoch of next leap second.
getNextLeapEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the epoch of next leap second.
getNextLeapTaimutc() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata: Get the difference (TAI – UTC) in seconds incorporated at epoch AcmMetadata.getNextLeapEpoch().
getNextLeapTaimutc() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the difference (TAI – UTC) in seconds incorporated at epoch OcmMetadata.getNextLeapEpoch().
getNextMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get Scheduled UTC epoch of the next CDM associated with the event identified by CONJUNCTION_ID.
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.
getNextParam() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.LocalSolarActivity
getNmF2() - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickParameters: Get the F2 layer maximum density.
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.
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.ilrs.ILRSHeader: Get the satellite NORAD ID (i.e.
getNoradID() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle: Get the NORAD Catalog Number ("Satellite Number").
getNormal(FieldSpacecraftState<T>) - Method in class org.orekit.forces.FixedPanel: Get panel normal in spacecraft frame.
getNormal(FieldSpacecraftState<T>) - Method in class org.orekit.forces.Panel: Get panel normal in spacecraft frame.
getNormal(FieldSpacecraftState<T>) - Method in class org.orekit.forces.PointingPanel: Get panel normal in spacecraft frame.
getNormal(FieldSpacecraftState<T>) - Method in class org.orekit.forces.SlewingPanel: Get panel normal in spacecraft frame.
getNormal(SpacecraftState) - Method in class org.orekit.forces.FixedPanel: Get panel normal in spacecraft frame.
getNormal(SpacecraftState) - Method in class org.orekit.forces.Panel: Get panel normal in spacecraft frame.
getNormal(SpacecraftState) - Method in class org.orekit.forces.PointingPanel: Get panel normal in spacecraft frame.
getNormal(SpacecraftState) - Method in class org.orekit.forces.SlewingPanel: Get panel 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.
getNormalizedC20(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider: Get the normalized coefficient of degree 2 and order 0 at a specific instance in time.
getNormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics: Get a spherical harmonic cosine coefficient.
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(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the gravity field coefficients provider from the first supported file.
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.
getNormalizedProvider(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Create a NormalizedSphericalHarmonicsProvider from an UnnormalizedSphericalHarmonicsProvider.
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.
getNormalizedValue(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver: Get normalized value at specific date.
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.
getnSteps() - Method in class org.orekit.propagation.conversion.AbstractLimitedVariableStepFieldIntegratorBuilder: Getter for number of steps.
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.files.rinex.clock.RinexClock: Get the number of different clock data types in the file.
getNumberOfConstraints() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter: Get the total number of constraints.
getNumberOfConstraints() - Method in class org.orekit.utils.AbstractMultipleShooting: Get the total number of constraints.
getNumberOfEpochs() - Method in class org.orekit.files.sp3.SP3Header: Returns the number of epochs contained in this orbit file.
getNumberOfFreeComponents() - Method in class org.orekit.utils.AbstractMultipleShooting: Get the number of free state components.
getNumberOfIonosphericLayers() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header: Get the number of ionospheric layers.
getNumberOfLeapSeconds() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the number of leap seconds.
getNumberOfLeapSeconds() - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader: Getter for the current number of leap seconds.
getNumberOfLeapSecondsGNSS() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the number of leap second for GNSS time scales.
getNumberOfPointsRecorded() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the number of data points recorded.
getNumberOfPointsUsed() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the number of data points used.
getNumberOfRawRanges() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement: Get the umber of raw ranges (after editing) compressed into the normal point.
getNumberOfReceivers() - Method in class org.orekit.files.rinex.clock.RinexClock: Get the number of receivers that are considered in the file.
getNumberOfSatellites() - Method in class org.orekit.files.rinex.clock.RinexClock: Get the number of satellites that are considered in the file.
getNumberOfSatellites() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionHeader: Get the number of satellites for the current IGM message.
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.files.rinex.clock.RinexClock.ClockDataLine: Getter for the number of values to follow.
getNumberSelectedMeasurementDrivers() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the number of estimated measurement parameters.
getNumberSelectedOrbitalDrivers() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the number of estimated orbital parameters.
getNumberSelectedPropagationDrivers() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the number of estimated propagation parameters.
getNutation() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Get the nutation angle of spin axis (rad).
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.
getNutationArguments(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.
getNutationVel() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized: Get the angular velocity of spin vector around angular momentum vector.
getNutLn() - Method in class org.orekit.files.sinex.SinexEopEntry: Get the nutation correction in longitude.
getNutOb() - Method in class org.orekit.files.sinex.SinexEopEntry: Get the nutation correction in obliquity.
getNutX() - Method in class org.orekit.files.sinex.SinexEopEntry: Get the nutation correction X.
getNutY() - Method in class org.orekit.files.sinex.SinexEopEntry: Get the nutation correction Y.
getObject() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the object name for which metadata are given.
getObjectDesignator() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata: Get the unique satellite identification designator for the object.
getObjectDesignator() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the object satellite catalog designator for which metadata are given.
getObjectDesignator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the unique satellite identification designator for the object.
getObjectID() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata: Get the spacecraft ID for which the attitude data are provided.
getObjectID() - Method in class org.orekit.files.ccsds.ndm.odm.OdmCommonMetadata: Get the spacecraft ID for which the orbit state is provided.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the function computing position/velocity at sample points.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter: Get the function computing position/velocity at sample points.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter: Get the function computing position/velocity at sample points.
getObjectName() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata: Get the spacecraft name for which the attitude data are provided.
getObjectName() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the spacecraft name for the object.
getObjectName() - Method in class org.orekit.files.ccsds.ndm.odm.OdmMetadata: Get the spacecraft name for which the orbit state is provided.
getObjectOrbitFromCdm(CdmRelativeMetadata, CdmData, CdmMetadata, DataContext) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod: Extract collision object spacecraft state from given Conjunction Data Message data.
getObjectStateCovarianceFromCdm(CdmRelativeMetadata, CdmData) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod: Get collision object state covariance from given Conjunction Data Message data.
getObjectType() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the type of object.
getObjectType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the type of object.
getOblateFlattening() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get central body oblate spheroid oblateness.
getObsAvailable() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters: Get the number of observations available for the OD of the object.
getObsAvailable() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get number of observations available within the actual OD span.
getObsBeforeNextMessage() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the flag indicating whether new tracking observations are anticipated prior to the issue of the next CDM associated with the event specified by CONJUNCTION_ID.
getObservationCode() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the observation code of the average phasecenter position w/r to antenna reference point.
getObservationData() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet: Get list of observation data.
getObservationData() - Method in class org.orekit.files.rinex.observation.ObservationDataSet: Get list of observation data.
getObservationDataSets() - Method in class org.orekit.files.rinex.observation.RinexObservation: Get an unmodifiable view of the observations.
getObservations() - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock: Get the list of Observations data lines.
getObservationSampling() - Method in class org.orekit.files.sinex.BiasDescription: Get the observation sampling interval used for data analysis.
getObservationTimeScale() - Method in enum org.orekit.gnss.SatelliteSystem: Get observation time scale for satellite system.
getObservationType() - Method in class org.orekit.files.rinex.observation.ObservationData: Get the observation type.
getObservedLineOfSight(Frame) - Method in class org.orekit.estimation.measurements.AngularAzEl: Calculate the Line Of Sight of the given measurement.
getObservedLineOfSight(Frame) - Method in class org.orekit.estimation.measurements.AngularRaDec: Calculate the Line Of Sight of the given measurement.
getObservedMeasurement() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase: 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.EstimatedMeasurementBase: Get the observed value.
getObserver() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator: Get the observer.
getObserver() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator: Get the observer.
getObserver() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the observer for Kalman Filter estimations.
getObserver() - Method in interface org.orekit.estimation.sequential.SemiAnalyticalProcess: Get the observer for Kalman Filter estimations.
getObserver() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimator: Get the observer.
getObserver() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: 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.files.rinex.observation.RinexObservationHeader: Get name of the observer.
getObservers() - Method in class org.orekit.utils.ParameterDriver: Get the observers for this driver.
getObsUsed() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters: Get the number of observations accepted for the OD of the object.
getObsUsed() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get number of observations accepted within the actual OD span.
getOccultationEngine() - Method in class org.orekit.propagation.events.EclipseDetector: Get the occultation engine.
getOccultationEngine() - Method in class org.orekit.propagation.events.FieldEclipseDetector: Get the occultation engine.
getOcculted() - Method in class org.orekit.utils.OccultationEngine: Getter for the occulted body.
getOccultedApparentRadius() - Method in class org.orekit.utils.OccultationEngine.FieldOccultationAngles: Get apparent radius of occulted body.
getOccultedApparentRadius() - Method in class org.orekit.utils.OccultationEngine.OccultationAngles: Get apparent radius of occulted body.
getOccultedBody() - Method in class org.orekit.forces.radiation.AbstractLightFluxModel: Getter for the occulted body's position provider.
getOccultedBodyPosition(AbsoluteDate, Frame) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel: Method computing the occulted body's position at a given date and frame.
getOccultedBodyPosition(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel: Method computing the occulted body's position at a given date and frame.
getOccultedRadius() - Method in class org.orekit.utils.OccultationEngine: Getter for the occultedRadius.
getOcculting() - Method in class org.orekit.utils.OccultationEngine: Getter for the occulting body.
getOccultingBodies() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel: Get all occulting bodies to consider.
getOccultingBodyRadius() - Method in class org.orekit.forces.radiation.AbstractSolarLightFluxModel: Getter for occulting body radius.
getOccultingBodyRadius() - Method in class org.orekit.propagation.events.CylindricalShadowEclipseDetector: Getter for occulting body radius.
getOccultingBodyRadius() - Method in class org.orekit.propagation.events.FieldCylindricalShadowEclipseDetector: Getter for occulting body radius.
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.
getOdEpoch() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters: Get the epoch of the orbit determination used for this message.
getOdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata: Get the Unique identifier of Orbit Data Message linked to this Attitude Data Message.
getOdmMsgLink() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the unique identifier of Orbit Data Message(s) that are linked (relevant) to this Conjunction Data Message.
getODParametersBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData: Get the OD parameters logical block.
getOebAreaAlongIntermediate() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties: Get the cross-sectional area of Optimally Enclosing Box when viewed along the intermediate OEB direction.
getOebAreaAlongMax() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties: Get the cross-sectional area of Optimally Enclosing Box when viewed along the maximum OEB direction.
getOebAreaAlongMin() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties: Get the cross-sectional area of Optimally Enclosing Box when viewed along the minimum OEB direction.
getOebIntermediate() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties: Get the intermediate physical dimension of the OEB.
getOebMax() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties: Get the maximum physical dimension of the OEB.
getOebMin() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties: Get the minimum physical dimension of the OEB.
getOebParentFrame() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties: Get the Optimally Enclosing Box parent reference frame.
getOebParentFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties: Get the Optimally Enclosing Box parent reference frame epoch.
getOebQ() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties: Get the quaternion defining Optimally Enclosing Box.
getOffset() - Method in class org.orekit.attitudes.LofOffset: Get the rotational offset.
getOffset() - Method in class org.orekit.time.ClockOffset: Get offset.
getOffset() - Method in class org.orekit.time.FieldClockOffset: Get offset.
getOffset() - Method in class org.orekit.time.OffsetModel: Offset at reference date in seconds (TAI minus UTC).
getOffset(AbsoluteDate) - Method in class org.orekit.estimation.measurements.QuadraticClockModel: Get the clock offset at date.
getOffset(AbsoluteDate) - Method in class org.orekit.time.AggregatedClockModel: Get the clock offset at date.
getOffset(AbsoluteDate) - Method in interface org.orekit.time.ClockModel: Get the clock offset at date.
getOffset(AbsoluteDate) - Method in class org.orekit.time.PerfectClockModel: Get the clock offset at date.
getOffset(AbsoluteDate) - Method in class org.orekit.time.SampledClockModel: Get the clock offset at date.
getOffset(AbsoluteDate) - 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.
getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.QuadraticClockModel: Get the clock offset at date.
getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.QuadraticFieldClockModel: Get the clock offset at date.
getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.time.AggregatedClockModel: Get the clock offset at date.
getOffset(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.ClockModel: Get the clock offset at date.
getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.time.PerfectClockModel: Get the clock offset at date.
getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.time.SampledClockModel: Get the clock offset at date.
getOffset(FieldAbsoluteDate<T>) - 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.
getOffsetGeodeticPoint(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.GroundStation: Get the geodetic point at the center of the offset frame.
getOffsetToInertial(Frame, AbsoluteDate, boolean) - 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.
getOffsetToInertialDownlink() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithDerivatives: Get transform between station and inertial frame.
getOffsetToInertialDownlink() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives: Get transform between station and inertial frame.
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.FieldGnssOrbitalElements: Get longitude of ascending node of orbit plane at weekly epoch.
getOmega0() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Get longitude of ascending node of orbit plane at weekly epoch.
getOmega0Driver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Get the driver for 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.gnss.rflink.gps.SubFrame3: Get dot(Ω).
getOmegaDot() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac: Get dot(Ω).
getOmegaDot() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get rate of right ascension.
getOmegaDotDriver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get the driver for the rate of right ascension.
getOne() - Method in class org.orekit.orbits.FieldOrbit: Getter for Field-valued one.
getOne() - Method in class org.orekit.time.AbstractFieldTimeInterpolator.InterpolationData: Get one.
getOneLetterCode() - Method in enum org.orekit.gnss.TimeSystem: Get the one letter code.
getOneWayDistance() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the one-way target distance (nominal).
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.DSSTGravityContext: ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext: Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext: Get ooAB = 1 / (A * B).
getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Get ooAB = 1 / (A * B).
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.FieldAbstractGaussianContributionContext: Get ooAB = 1 / (A * B).
getOoBpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext: Get ooBpo = 1 / (B + 1).
getOoBpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext: Get ooBpo = 1 / (B + 1).
getOoMU() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext: Get ooMu = 1 / mu.
getOoMU() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext: Get ooMu = 1 / mu.
getOON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext: Get 1 / (n² * a²).
getOON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext: Get 1 / (n² * a²).
getOpener() - Method in class org.orekit.data.DataSource: Get the data stream opener.
getOperator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the operator of the space object.
getOperator() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Get the institution/agency/company operating the caster.
getOperator() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord: Get the institution/agency/company operating the caster.
getOperatorContactPosition() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the contact position of the owner / operator of the object.
getOperatorEmail() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the email of the operator of the object.
getOperatorOrganization() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the contact organisation of the object.
getOperatorPhone() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the contact phone of the operator of the object.
getOpsStatus() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the operational status.
getOptimizer() - Method in class org.orekit.propagation.conversion.osc2mean.LeastSquaresConverter: Gets the optimizer.
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.orbits.WalkerConstellationSlot: Get the orbit.
getOrbit() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the current orbit.
getOrbit() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the orbit.
getOrbit() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the 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 propagation orbital elements.
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.
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.AbstractKalmanEstimator: Get the orbital parameters supported by this estimator.
getOrbitalPeriod() - Method in class org.orekit.orbits.CR3BPDifferentialCorrection: Get the orbital period of the required orbit.
getOrbitalPeriod() - Method in class org.orekit.orbits.LibrationOrbit: Return the orbital period of the libration orbit.
getOrbitCategory() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the orbit category.
getOrbitCenter() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the central body for object 1 and 2.
getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCombinedCorrectionData: Get the orbit correction data.
getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionData: Get the orbit correction data.
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.
getOrbitInterpolator() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator: Get orbit interpolator.
getOrbitInterpolator() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator: Get orbit interpolator.
getOrbitInterpolator() - Method in class org.orekit.propagation.SpacecraftStateInterpolator: Get orbit interpolator.
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.
getOrbitRadius() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator: Get the computed satellite's orbit.
getOrbitRadius() - Method in class org.orekit.propagation.analytical.intelsat.IntelsatElevenElementsPropagator: Get the computed satellite's orbit.
getOrbitType() - Method in class org.orekit.files.sp3.SP3Header: Returns the SP3OrbitType for this SP3 file.
getOrbitType() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester: Get the orbit type used for the matrix computation.
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.averaging.AveragedOrbitalState: Getter for the averaged orbit type.
getOrbitType() - Method in class org.orekit.propagation.conversion.averaging.BrouwerLyddaneOrbitalState: Getter for the averaged orbit type.
getOrbitType() - Method in class org.orekit.propagation.conversion.averaging.DSST6X0OrbitalState: Getter for the averaged orbit type.
getOrbitType() - Method in class org.orekit.propagation.conversion.averaging.EcksteinHechlerOrbitalState: Getter for the averaged orbit type.
getOrbitType() - Method in class org.orekit.propagation.conversion.averaging.SGP4OrbitalState: Getter for the averaged orbit type.
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.FieldStateCovariance: Get the covariance orbit 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 interface org.orekit.propagation.MatricesHarvester: Get the orbit type used for the matrix computation.
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.DSSTHarvester: Get the orbit type used for the matrix computation.
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.
getOrbitType() - Method in class org.orekit.propagation.StateCovariance: Get the covariance orbit type.
getOrbitTypeKey() - Method in class org.orekit.files.sp3.SP3Header: 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.FieldNegateDetector: Get the delegate event detector.
getOriginal() - Method in class org.orekit.propagation.events.NegateDetector: Get the delegate event detector.
getOriginalEstimatedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase: Get the original estimated value prior to any modification.
getOriginator() - Method in class org.orekit.files.ccsds.section.Header: Get the message originator.
getOriginatorAddress() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata: Get the address of Programmatic Point Of Contact at originator.
getOriginatorAddress() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the address of Programmatic Point Of Contact at originator.
getOriginatorEmail() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata: Get the email address of Programmatic Point Of Contact at originator.
getOriginatorEmail() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the email address of Programmatic Point Of Contact at originator.
getOriginatorPhone() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata: Get the phone number 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.adm.acm.AcmMetadata: Get the 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.adm.acm.AcmMetadata: Get the position of 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.
getOriginatorRoutingIndicator() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current OriginatorRoutingIndicatorTerm value.
getOriginatorRoutingIndicator() - Method in class org.orekit.files.iirv.IIRVVector: Gets the originator routing indicator term.
getOriginIdentification() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current OriginIdentificationTerm value.
getOriginIdentification() - Method in class org.orekit.files.iirv.IIRVVector: Gets the origin identification term.
getOriginIndicator() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement: Get the angle origin indicator.
getOriginOfValues() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement: Get the origin of values. 0=measure values 1=interpolated values
getOsb() - Method in class org.orekit.files.sinex.SatelliteObservableSpecificSignalBias: Get the OSB data for the current satellite.
getOsb(SatelliteSystem) - Method in class org.orekit.files.sinex.StationObservableSpecificSignalBias: Get the OSB data for a given satellite system.
getOsculatingCircularOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Get the osculating circular orbit from the EH model.
getOsculatingCircularOrbit(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Get the osculating circular orbit from the EH model.
getOther() - Method in class org.orekit.frames.encounter.AbstractEncounterLOF: Get the normal version of other's position and velocity coordinates.
getOther() - Method in interface org.orekit.frames.encounter.EncounterLOF: Get other's position and velocity coordinates.
getOtherAtTCA() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Get other's orbit at time of closest approach.
getOtherAtTCA() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Get other's orbit at time of closest approach.
getOtherCovariance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Get other's covariance.
getOtherCovariance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Get other's covariance.
getOutFrame() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator: Get output frame.
getOutLOF() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator: Get output local orbital frame.
getOutOrbitType() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator: Get output orbit type.
getOutPositionAngleType() - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator: Get output position angle type.
getOutputFrame() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator: Get output frame.
getOutputFrame() - Method in class org.orekit.propagation.SpacecraftStateInterpolator: Get output frame.
getOutputFrame() - Method in class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator: Get output frame for the interpolated instance.
getOutputFrame() - Method in class org.orekit.utils.FieldAbsolutePVCoordinatesHermiteInterpolator: Get output frame for the interpolated instance.
getOutputInertialFrame() - Method in class org.orekit.orbits.AbstractFieldOrbitInterpolator: Get output inertial frame.
getOutputInertialFrame() - Method in class org.orekit.orbits.AbstractOrbitInterpolator: Get output inertial frame.
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.orbits.WalkerConstellation: Get the number of orbital planes.
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.FieldGnssOrbitalElements: Get 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 class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Get 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.
getPaDriver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Get the driver for the argument of perigee.
getPanels() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Get the panels composing the body.
getParameterDerivatives(ParameterDriver) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the partial derivatives of the simulated measurement with respect to a parameter.
getParameterDerivatives(ParameterDriver, AbsoluteDate) - 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 interface org.orekit.utils.ParameterDriversProvider: Get parameter value from its name.
getParameters() - Method in class org.orekit.files.ccsds.ndm.odm.UserDefined: Get all user defined parameters.
getParameters() - Method in interface org.orekit.utils.ParameterDriversProvider: Get model parameters.
getParameters(Field<T>) - Method in interface org.orekit.utils.ParameterDriversProvider: Get model parameters.
getParameters(Field<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.utils.ParameterDriversProvider: Get model parameters.
getParameters(FieldSpacecraftState<Gradient>, ParameterDriversProvider) - Method in class org.orekit.propagation.integration.AbstractGradientConverter: Get the parametric model parameters, return gradient values for each span of each driver (several gradient values for each parameter).
getParameters(AbsoluteDate) - Method in interface org.orekit.utils.ParameterDriversProvider: Get model parameters.
getParametersAllValues() - Method in interface org.orekit.utils.ParameterDriversProvider: Get model parameters, return a list a all span values of all parameters.
getParametersAllValues(Field<T>) - Method in interface org.orekit.utils.ParameterDriversProvider: Get model parameters.
getParametersAtStateDate(FieldSpacecraftState<Gradient>, ParameterDriversProvider) - Method in class org.orekit.propagation.integration.AbstractGradientConverter: Get the parametric model parameters, return gradient values at state date for each driver (only 1 gradient value for each parameter).
getParametersDrivers() - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider: Get the drivers for parameters.
getParametersDrivers() - Method in interface org.orekit.attitudes.AttitudeProvider: Get the drivers for parameters.
getParametersDrivers() - Method in interface org.orekit.attitudes.AttitudeProviderModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.gnss.AbstractWindUp: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AberrationModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockOnBoardRangeRateModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier: Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.Bias: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesPhaseModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSPhaseModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSRangeModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersPhaseModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseCentersRangeModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesPhaseModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesRangeModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSPhaseModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockPhaseModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeRateModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesPhaseModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockInterSatellitesRangeModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSPhaseModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockOneWayGNSSRangeModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockPhaseModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticJ2ClockRangeModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TDOAIonosphericDelayModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TDOATroposphericDelayModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.drag.DragForce: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.drag.TimeSpanDragForce: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.ParametricAcceleration: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration: Get the drivers for parameters.
getParametersDrivers() - Method in interface org.orekit.forces.ForceModelModifier: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.AbstractBodyAttraction: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.DeSitterRelativity: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.J2OnlyPerturbation: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.LenseThirringRelativity: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.NewtonianAttraction: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.Relativity: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.inertia.InertialForces: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.Maneuver: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.ECOM2: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.RadiationPressureModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.AbstractVienna: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.AskneNordiusModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.CanonicalSaastamoinenModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ConstantTroposphericModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.EstimatedModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.iturp834.ITURP834PathDelay: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.MariniMurray: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ModifiedHopfieldModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator: Get the parameters driver for propagation model.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.gnss.FieldGnssPropagator: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.intelsat.FieldIntelsatElevenElementsPropagator: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.FieldTLE: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator: Get the drivers for parameters.
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 drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedForm: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Get the drivers for parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Get the drivers for parameters.
getParametersDrivers() - Method in interface org.orekit.utils.ParameterDriversProvider: Get the drivers for parameters.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester: Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester: Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester: Get the Jacobian with respect to propagation parameters.
getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester: Get the Jacobian with respect to propagation parameters.
getParameterSpacing() - Method in class org.orekit.files.sinex.BiasDescription: Get the parameter spacing interval between the bias value.
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.EstimatedMeasurementBase: 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() - Method in interface org.orekit.time.TimeScales: Dummy date at infinity in the past direction.
getPastInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: 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.
getPattern() - Method in class org.orekit.orbits.WalkerConstellation: Get the constellation pattern.
getPattern(RadioWave) - Method in class org.orekit.gnss.antenna.Antenna: Get a frequency pattern.
getPdop() - Method in class org.orekit.gnss.DOP: Gets the position dilution of precision.
getPeakMinusMean() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the system delay peak – mean value.
getPeakMinusMean() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics: Get the session peak – mean value.
getPendingEvent() - Method in class org.orekit.propagation.events.FieldEventState: Get PendingEvent.
getPeriapsisAltitude() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the distance of the closest point in the objects orbit above the equatorial radius of the central body.
getPeriapsisDetectionAdaptableInterval() - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory: Method providing a candidate AdaptableInterval for periapsis detection.
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.common.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.
getPhaseCenters(AbsoluteDate) - Method in class org.orekit.files.sinex.Station: Get the phase centers for the given epoch.
getPhaseCentersMap() - Method in class org.orekit.files.sinex.Station: Get the TimeSpanMap of phase centers.
getPhaseCenterSystem() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get satellite system for average phase center.
getPhaseCenterVariation(Vector3D) - Method in class org.orekit.gnss.antenna.FrequencyPattern: Get the value of the phase center variation in a signal direction.
getPhaseCenterVariation(RadioWave, Vector3D) - Method in class org.orekit.gnss.antenna.Antenna: Get the value of the phase center variation in a signal direction.
getPhaseCenterVariationFunction() - Method in class org.orekit.gnss.antenna.FrequencyPattern: Get the phase center variation function.
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.files.rinex.observation.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.AbstractKalmanEstimator: Get the "physical" estimated covariance matrix (i.e. not normalized)
getPhysicalEstimatedCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the "physical" estimated covariance matrix (i.e. not normalized)
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the "physical" estimated covariance matrix (i.e. not normalized)
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the "physical" estimated covariance matrix (i.e. not normalized)
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator: Get the "physical" estimated state (i.e. not normalized)
getPhysicalEstimatedState() - Method in interface org.orekit.estimation.sequential.KalmanEstimation: Get the "physical" estimated state (i.e. not normalized)
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the "physical" estimated state (i.e. not normalized)
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the "physical" estimated state (i.e. not normalized)
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.
getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the physical innovation covariance 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.
getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the physical Kalman gain 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).
getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the physical Jacobian of the measurement with respect to the state (H matrix).
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.
getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
getPhysicBlock() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData: Get physical properties logical block.
getPhysicBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData: Get physical properties logical block.
getPlane() - Method in class org.orekit.orbits.WalkerConstellationSlot: Get the plane index.
getPlaneSection(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.bodies.Ellipsoid: Compute the 2D ellipse at the intersection of the 3D ellipsoid and a plane.
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.bodies.Loxodrome: Get the geodetic point defining the loxodrome.
getPoint() - Method in class org.orekit.frames.TopocentricFrame: Get the surface point defining the origin of the frame.
getPoint(int) - Method in class org.orekit.models.earth.ionosphere.nequick.Segment: Get point along the ray.
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.orbits.FieldOrbit: Get the position in definition frame.
getPosition() - Method in class org.orekit.orbits.Orbit: Get the position in definition frame.
getPosition() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the position in orbit definition frame.
getPosition() - Method in class org.orekit.propagation.SpacecraftState: Get the position in orbit definition frame.
getPosition() - Method in class org.orekit.utils.FieldPVCoordinates: Gets the position.
getPosition() - Method in class org.orekit.utils.PVCoordinates: Gets the position.
getPosition(Frame) - Method in class org.orekit.orbits.FieldOrbit: Get the position in a specified frame.
getPosition(Frame) - Method in class org.orekit.orbits.Orbit: Get the position in a specified frame.
getPosition(Frame) - Method in class org.orekit.propagation.FieldSpacecraftState: Get the position in given output frame.
getPosition(Frame) - Method in class org.orekit.propagation.SpacecraftState: Get the position in given output frame.
getPosition(Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates: Get the position in a specified frame.
getPosition(Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates: Get the position in a specified frame.
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.bodies.AnalyticalSolarPositionProvider: Get the position of the body in the selected frame.
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.files.general.EphemerisSegmentPropagator
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame: Get the position of the body in the selected frame.
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.orbits.Orbit: Get the position of the body in the selected frame.
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
getPosition(AbsoluteDate, Frame) - Method in interface org.orekit.propagation.Propagator: Get the position of the body in the selected frame.
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.utils.ConstantPVCoordinatesProvider
getPosition(AbsoluteDate, Frame) - Method in class org.orekit.utils.FrameAdapter: Get the position of the body in the selected frame.
getPosition(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider: Get the position of the body in the selected frame.
getPosition(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.bodies.AnalyticalSolarPositionProvider: Get the position in the selected frame.
getPosition(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.orbits.FieldOrbit: Get the position of the body in the selected frame.
getPosition(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.propagation.FieldPropagator: Get the position of the body in the selected frame.
getPosition(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPositionProvider: Get the position in the selected frame.
getPosition(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider: Deprecated.

Get the position of the body in the selected frame.
getPosition(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.FieldPVCoordinatesProvider: Get the position of the body in the selected frame.
getPosition(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.utils.FrameAdapter: Get the position in the selected frame.
getPositionAccuracy() - Method in class org.orekit.files.sp3.SP3Coordinate: Get the position accuracy.
getPositionAdjointContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointGravitationalTerm: Computes the contribution to position adjoint derivatives.
getPositionAdjointContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm: Computes the contribution to position adjoint derivatives.
getPositionAdjointContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term: Computes the contribution to position adjoint derivatives.
getPositionAdjointContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointKeplerianTerm: Computes the contribution to position adjoint derivatives.
getPositionAdjointFieldContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointGravitationalTerm: Computes the contribution to position adjoint derivatives.
getPositionAdjointFieldContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm: Computes the contribution to position adjoint derivatives.
getPositionAdjointFieldContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term: Computes the contribution to position adjoint derivatives.
getPositionAdjointFieldContribution(FieldAbsoluteDate<T>, T[], T[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointKeplerianTerm: Computes the contribution to position adjoint derivatives.
getPositionAngleType() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise: Getter for the positionAngle.
getPositionAngleType() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester: Get the position angle used for the matrix computation.
getPositionAngleType() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getPositionAngleType() - Method in interface org.orekit.propagation.conversion.averaging.AveragedOrbitalState: Getter for the averaged position angle.
getPositionAngleType() - Method in class org.orekit.propagation.conversion.averaging.BrouwerLyddaneOrbitalState: Getter for the averaged position angle.
getPositionAngleType() - Method in class org.orekit.propagation.conversion.averaging.DSST6X0OrbitalState: Getter for the averaged position angle.
getPositionAngleType() - Method in class org.orekit.propagation.conversion.averaging.EcksteinHechlerOrbitalState: Getter for the averaged position angle.
getPositionAngleType() - Method in class org.orekit.propagation.conversion.averaging.SGP4OrbitalState: Getter for the averaged position angle.
getPositionAngleType() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getPositionAngleType() - Method in class org.orekit.propagation.events.PositionAngleDetector: Get the type of position angle.
getPositionAngleType() - Method in class org.orekit.propagation.FieldStateCovariance: Get the covariance angle type.
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 interface org.orekit.propagation.MatricesHarvester: Get the position angle used for the matrix computation.
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.DSSTHarvester: Get the position angle used for the matrix computation.
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.
getPositionAngleType() - Method in class org.orekit.propagation.StateCovariance: Get the covariance angle type.
getPositionScale() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the position scale.
getPositionVector() - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector: Get object Position Vector.
getPositionVector() - Method in class org.orekit.files.iirv.IIRVVector: Gets a position vector [x y z], represented as a Vector3D instance.
getPosVelBase() - Method in class org.orekit.files.sp3.SP3Header: Get the base for position/velocity accuracy.
getPotential(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel: Calculate spacecraft potential.
getPotential(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel: Calculate spacecraft potential.
getPreamble() - Method in class org.orekit.gnss.rflink.gps.SubFrame: Get telemetry preamble.
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 interface org.orekit.estimation.sequential.KalmanEstimation: Get the predicted measurement.
getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Get the predicted measurement.
getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: Get the predicted measurement.
getPredictedMeasurements(RealVector[], MeasurementDecorator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
getPredictedMeasurements(RealVector[], MeasurementDecorator) - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel
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.
getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel: 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.FieldPressureTemperature: Get pressure.
getPressure() - Method in class org.orekit.models.earth.weather.PressureTemperature: Get pressure.
getPressureTemperatureHumidity(AbsoluteDate) - Method in class org.orekit.estimation.measurements.GroundStation: Get the weather parameters.
getPressureTemperatureHumidity(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.GroundStation: Get the weather parameters.
getPrevId() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination: Get identification of previous orbit determination.
getPrevId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get identification of previous orbit determination.
getPrevID() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver: Get identification number of previous maneuver.
getPreviousMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the UTC epoch of the previous CDM issued for the event identified by CONJUNCTION_ID.
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.cdm.CdmRelativeMetadata: Get the ID of previous CDM issued for event identified by CONJUNCTION_ID.
getPreviousMessageID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the unique ID identifying previous message from a given originator.
getPreviousParam() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData.LocalSolarActivity
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.
getPrimary() - Method in class org.orekit.estimation.measurements.gnss.Dipole: Get the primary dipole vector.
getPrimaryObject() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector: Get the primaryObject, at the center of the proximity zone.
getPrimaryStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange: Get the primary ground station from which measurement is performed.
getPrimaryWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration: Get the primary wavelength.
getPrimeMeridianAngle(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole: Get the prime meridian angle.
getPrimeMeridianAngle(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole: Get the prime meridian angle.
getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get a driver allowing to add a prime meridian rotation rate.
getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to add a prime meridian rotation rate.
getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get a driver allowing to add a prime meridian rotation.
getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to add a prime meridian rotation.
getPrimeStation() - Method in class org.orekit.estimation.measurements.FDOA: Get the prime ground station, the one that gives the date of the measurement.
getPrimeStation() - Method in class org.orekit.estimation.measurements.TDOA: Get the prime ground station, the one that gives the date of the measurement.
getPrmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the Unique identifier of Pointing Request Message linked to this Orbit Data Message.
getPrn() - Method in class org.orekit.files.rinex.navigation.TypeSvMessage: Get satellite number.
getPRN() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac: Get the PRN code phase of the SV.
getPRN() - Method in class org.orekit.gnss.SatInSystem: Get the Pseudo Random Number of the satellite.
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.GNSSOrbitalElementsDriversProvider: Get the PRN number of the 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.estimation.measurements.gnss.CombinedObservationDataSet: 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.
getProbabilityOfCollisionMethodName() - Method in class org.orekit.ssa.metrics.FieldProbabilityOfCollision: Get name of the probability computing method with which this probability was computed.
getProbabilityOfCollisionMethodName() - Method in class org.orekit.ssa.metrics.ProbabilityOfCollision: Get name of the probability computing method with which this probability was computed.
getProcessingSoftwareName() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration: Get the processing software name.
getProcessingSoftwares() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Get the processing softwares.
getProcessingSoftwareVersion() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration: Get the processing software version.
getProcessingSoftwareVersions() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Get the processing software versions.
getProcessNoiseMatrix(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanModel
getProcessNoiseMatrix(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.UnscentedKalmanModel
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.files.rinex.AppliedDCBS: Get the program name used to apply DCBs.
getProgPCVS() - Method in class org.orekit.files.rinex.AppliedPCVS: Get the program name used to apply PCVs.
getProgramName() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the program name.
getProgramName() - Method in class org.orekit.files.rinex.section.RinexBaseHeader: Getter for the program name.
getPropagationFrame() - Method in class org.orekit.control.indirect.shooting.propagation.ShootingPropagationSettings: Getter for the propagation frame.
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.
getPropagationParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator: Get the propagator parameters supported by this estimator.
getPropagationParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise: Getter for the propagationParametersEvolution.
getPropagationSettings() - Method in class org.orekit.control.indirect.shooting.AbstractIndirectShooting: Getter for the propagation settings.
getPropagationType() - Method in class org.orekit.propagation.conversion.AbstractIntegratedPropagatorBuilder: Getter for the propagation type.
getPropagationType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the propagation type.
getPropagationType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get the propagation type.
getPropagator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get the orbit propagator used to generate this trajectory.
getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment: View this ephemeris segment as a propagator.
getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris: View this ephemeris as a propagator, combining data from all segments.
getPropagator() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris: View this ephemeris as a propagator, combining data from all segments.
getPropagator() - Method in class org.orekit.files.sp3.SP3Segment: View this ephemeris segment as a propagator.
getPropagator() - 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.
getPropagator() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac: Get the propagator corresponding to the navigation message.
getPropagator() - Method in class org.orekit.propagation.analytical.gnss.data.FieldAbstractAlmanac: Get the propagator corresponding to the navigation message.
getPropagator() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac: Get the propagator corresponding to the navigation message.
getPropagator() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Get the propagator corresponding to the navigation message.
getPropagator(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Get the propagator corresponding to the navigation message.
getPropagator(double, DataContext) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Get the propagator corresponding to the navigation message.
getPropagator(double, DataContext, AttitudeProvider, Frame, double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Get the propagator corresponding to the navigation message.
getPropagator(AttitudeProvider) - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment: View this ephemeris segment as a propagator.
getPropagator(AttitudeProvider) - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris: View this ephemeris as a propagator, combining data from all segments.
getPropagator(AttitudeProvider) - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris: View this ephemeris as a propagator, combining data from all segments.
getPropagator(AttitudeProvider) - Method in class org.orekit.files.sp3.SP3Segment: View this ephemeris segment as a propagator.
getPropagator(DataContext) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac: Get the propagator corresponding to the navigation message.
getPropagator(DataContext, AttitudeProvider, Frame, Frame, double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac: Get the propagator corresponding to the navigation message.
getPropagator(ObservableSatellite) - Method in class org.orekit.estimation.measurements.generation.Generator: Get a registered propagator.
getPropagator(Frames) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac: Get the propagator corresponding to the navigation message.
getPropagator(Frames) - Method in class org.orekit.propagation.analytical.gnss.data.FieldAbstractAlmanac: Get the propagator corresponding to the navigation message.
getPropagator(Frames) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Get the propagator corresponding to the navigation message.
getPropagator(Frames, AttitudeProvider, Frame, Frame, double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac: Get the propagator corresponding to the navigation message.
getPropagator(Frames, AttitudeProvider, Frame, Frame, double, double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage: Get the propagator corresponding to the navigation message.
getPropagator(Frames, AttitudeProvider, Frame, Frame, T) - Method in class org.orekit.propagation.analytical.gnss.data.FieldAbstractAlmanac: Get the propagator corresponding to the navigation message.
getPropagatorIndex() - Method in class org.orekit.estimation.measurements.ObservableSatellite: Get the index of the propagator related to this satellite.
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.
getPropagatorsMap() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator: Get the propagators map.
getPropulsionModel() - Method in class org.orekit.forces.maneuvers.Maneuver: Get the propulsion model.
getPropulsionModelParameters(double[]) - Method in class org.orekit.forces.maneuvers.Maneuver: Extract propulsion model parameters from the parameters' array called in by the ForceModel interface.
getPropulsionModelParameters(T[]) - Method in class org.orekit.forces.maneuvers.Maneuver: Extract propulsion model parameters from the parameters' array called in by the ForceModel interface.
getProvider() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Get the spherical harmonics provider.
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.SHAFormatReader: 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.
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.
getPsdTimeSpanMap() - Method in class org.orekit.files.sinex.Station: Get the TimeSpanMap of Post-Seismic Deformation.
getPth0Provider() - Method in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel: Get provider for atmospheric pressure, temperature and humidity at reference altitude.
getPulsations() - Method in class org.orekit.utils.SecularAndHarmonic: Get the pulsations of harmonic part.
getPulseEnergy() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration: Get the pulse energy.
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).
getPVAFilter() - Method in class org.orekit.orbits.FieldOrbitHermiteInterpolator: Get filter for derivatives from the sample to use in position-velocity-acceleration interpolation.
getPVAFilter() - Method in class org.orekit.orbits.OrbitHermiteInterpolator: Get filter for derivatives from the sample to use in position-velocity-acceleration interpolation.
getPVCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm: Get the position/velocity coordinates contained in the OPM.
getPVCoordinates() - Method in class org.orekit.files.iirv.IIRVVector: Gets the state vector as a PVCoordinates instance.
getPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit: Get the TimeStampedPVCoordinates in definition frame.
getPVCoordinates() - Method in class org.orekit.orbits.Orbit: Get the TimeStampedPVCoordinates in definition frame.
getPVCoordinates() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the TimeStampedFieldPVCoordinates in orbit definition frame.
getPVCoordinates() - Method in class org.orekit.propagation.SpacecraftState: Get the TimeStampedPVCoordinates in orbit definition frame.
getPVCoordinates() - Method in class org.orekit.utils.AbsolutePVCoordinates: Get the TimeStampedPVCoordinates.
getPVCoordinates() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates: Get the TimeStampedFieldPVCoordinates.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.FieldOrbit: Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.Orbit: Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.FieldSpacecraftState: Get the TimeStampedFieldPVCoordinates in given output frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.SpacecraftState: Get the TimeStampedPVCoordinates in given output frame.
getPVCoordinates(Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates: Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates: Get the TimeStampedFieldPVCoordinates in a specified frame.
getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the extrapolated position and velocity from an initial TLE.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.files.general.EphemerisSegmentPropagator
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame: Get the PVCoordinates of the topocentric frame origin in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.orbits.Orbit: 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 interface org.orekit.propagation.Propagator: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.InvalidPVProvider
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.ConstantPVCoordinatesProvider
getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.utils.ExtendedPositionProvider: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.FrameAdapter: Get the PVCoordinates 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.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.ShiftingPVCoordinatesProvider: Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.orbits.FieldOrbit: Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.propagation.FieldPropagator: Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator: Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPositionProvider: Get the position-velocity-acceleration in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider: Deprecated.

Get the FieldPVCoordinates of the body in the selected 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(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.utils.FieldShiftingPVCoordinatesProvider: Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.utils.FrameAdapter: Get the position-velocity-acceleration 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.
getPVCoordinatesProvider() - Method in class org.orekit.propagation.events.AlignmentDetector: Get the body to align.
getPVJacobian() - Method in interface org.orekit.frames.FieldKinematicTransform: Compute the Jacobian of the FieldKinematicTransform.transformOnlyPV(FieldPVCoordinates) (FieldPVCoordinates)} method of the transform.
getPVJacobian() - Method in interface org.orekit.frames.KinematicTransform: Compute the Jacobian of the KinematicTransform.transformOnlyPV(PVCoordinates) (PVCoordinates)} method of the transform.
getPvProvider() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: 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.
getQuadraticClockModel() - Method in class org.orekit.estimation.measurements.ObservableSatellite: Get a quadratic clock model valid at some date.
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.
getQZSSCivilianNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get all the QZSS navigation messages contained in the file.
getQZSSCivilianNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get the QZSS navigation messages for the given satellite Id.
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.
getQZSSLegacyNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get all the QZSS navigation messages contained in the file.
getQZSSLegacyNavigationMessages(String) - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get the QZSS navigation messages for the given satellite Id.
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.
getQzssToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data: Get the QZSS time of clock.
getR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyDynamicContext: Get the distance from center of mass of the central body to the 3rd body.
getR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyDynamicContext: Get the distance from center of mass of the central body to the 3rd body.
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.
getRaanDistribution() - Method in enum org.orekit.orbits.WalkerConstellation.Pattern: Get the RAAN distribution for the pattern.
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.
getRadiationSensitive() - Method in class org.orekit.forces.radiation.RadiationPressureModel: Getter for radiation sensitive object.
getRadiationSensitiveSpacecraft() - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Getter for radiation-sensitive spacecraft.
getRadioWave() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for radio wave.
getRadioWave() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for radio wave.
getRadioWaves() - Method in class org.orekit.gnss.antenna.Antenna: Get supported radio waves.
getRadius() - Method in class org.orekit.models.earth.ionosphere.nequick.Ray: Get the ray-perigee radius.
getRadomeCode() - Method in class org.orekit.files.sinex.AntennaKey: Get the radome code.
getRange() - Method in class org.orekit.utils.FieldTrackingCoordinates: Get the range.
getRange() - Method in class org.orekit.utils.TrackingCoordinates: Get the range.
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.
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.
getRange1() - Method in class org.orekit.estimation.iod.IodGooding: Get range for observation (1).
getRange2() - Method in class org.orekit.estimation.iod.IodGooding: Get range for observation (2).
getRange3() - Method in class org.orekit.estimation.iod.IodGooding: Get 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() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement: Get the range rate.
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.
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.
getRangeSupplementData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the range supplement data for the data block.
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() - Method in class org.orekit.time.ClockOffset: Get rate.
getRate() - Method in class org.orekit.time.FieldClockOffset: Get rate.
getRate(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide: Get the angular rate of the tide.
getRateElementsType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState: Get the type of the elements rates.
getRateProcessNoiseStdDev() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination: Get process noise standard deviation if AttitudeDetermination.rateStates is RateElementsType.ANGVEL.
getRatesContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm: Computes the contribution to the rates of the adjoint variables.
getRatesContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointGravitationalTerm: Computes the contribution to the rates of the adjoint variables.
getRatesContribution(AbsoluteDate, double[], double[], Frame) - Method in interface org.orekit.control.indirect.adjoint.CartesianAdjointEquationTerm: Computes the contribution to the rates of the adjoint variables.
getRatesContribution(AbsoluteDate, double[], double[], Frame) - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm: Computes the contribution to the rates of the adjoint variables.
getRateStates() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination: Get attitude rate states.
getRateType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata: Get attitude rate element set type.
getRatio() - Method in interface org.orekit.gnss.GnssSignal: Get the ratio f/f0, where f0 is the common frequency.
getRatio() - Method in enum org.orekit.gnss.PredefinedGnssSignal: 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.
getRawPosition(AbsoluteDate) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider: Get the position at date.
getRawPosition(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider: Get the position at date.
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.CommonPhysicalProperties: Get the typical (50th percentile) radar cross-section.
getRcvrClkOffset() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet: Get receiver clock offset.
getRcvrClkOffset() - Method in class org.orekit.files.rinex.observation.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.
getReceiveAmplitude() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement: Get the receive amplitude.
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.
getReceiver() - Method in class org.orekit.estimation.measurements.gnss.AmbiguityDriver: Get receiver id.
getReceiverIdentifier() - Method in class org.orekit.files.rinex.clock.RinexClock.Receiver: Getter for the receiver identifier.
getReceiverNumber() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the number of the receiver.
getReceivers() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the receivers.
getReceiversAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader: Get parsed receivers antennas.
getReceiverStation() - Method in class org.orekit.estimation.measurements.BistaticRange: Get the receiver ground station.
getReceiverStation() - Method in class org.orekit.estimation.measurements.BistaticRangeRate: Get the receiver ground station.
getReceiverType() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the type of the receiver.
getReceiverVersion() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the version of the receiver.
getRecH() - Method in class org.orekit.models.earth.ionosphere.nequick.Ray: Get receiver altitude.
getRecommendedOdSpan() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters: Get the recommended OD time span calculated for the object.
getRecommendedOdSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get time span of observation recommended for the OD of the object.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord: Get the type of record.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord: Get the type of record.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord: Get the type of record.
getRecordType() - Method in class org.orekit.gnss.metric.ntrip.Record: Get the type of record.
getReductionTheory() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations: Get reduction theory used for precession and nutation modeling.
getReferenceAtTCA() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Get reference's orbit at time of closest approach.
getReferenceAtTCA() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Get reference's orbit at time of closest approach.
getReferenceAttitude() - Method in class org.orekit.attitudes.FixedRate: Get the reference attitude.
getReferenceClocks() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the reference clocks.
getReferenceCovariance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Get reference's covariance.
getReferenceCovariance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Get reference's covariance.
getReferenceDate() - Method in class org.orekit.estimation.sequential.AbstractKalmanEstimator: Get the reference date.
getReferenceDate() - Method in class org.orekit.files.ccsds.definitions.TimeConverter: Get the reference date for relative dates (may be null if no relative dates are used).
getReferenceDate() - Method in class org.orekit.files.ccsds.utils.ContextBinding: Get initial date.
getReferenceDate() - Method in class org.orekit.files.rinex.navigation.TimeSystemCorrection: Getter for the reference date of the time system correction polynomial.
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.
getReferenceEpoch() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage: Get the reference epoch.
getReferenceEpoch() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage: Get the reference epoch.
getReferenceFrame() - Method in class org.orekit.attitudes.Attitude: Get the reference frame.
getReferenceFrame() - Method in class org.orekit.attitudes.AttitudeInterpolator: Get reference frame from which attitude is defined.
getReferenceFrame() - Method in class org.orekit.attitudes.FieldAttitude: Get the reference frame.
getReferenceFrame() - Method in class org.orekit.attitudes.FieldAttitudeInterpolator: Get reference frame from which attitude is defined.
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.acm.AttitudeStateHistory: Get the reference frame from which attitude is defined.
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.OdmCommonMetadata: 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.
getReferenceInertialFrame() - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm: Getter for reference frame.
getReferenceName() - Method in class org.orekit.files.rinex.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.
getReferenceRadius() - Method in class org.orekit.propagation.conversion.osc2mean.BrouwerLyddaneTheory: Gets reference radius of the central body (m).
getReferenceRadius() - Method in class org.orekit.propagation.conversion.osc2mean.DSSTTheory: Gets reference radius of the central body (m).
getReferenceRadius() - Method in class org.orekit.propagation.conversion.osc2mean.EcksteinHechlerTheory: Gets reference radius of the central body (m).
getReferenceRadius() - Method in interface org.orekit.propagation.conversion.osc2mean.MeanTheory: Gets reference radius of the central body (m).
getReferenceRadius() - Method in class org.orekit.propagation.conversion.osc2mean.TLETheory: Gets reference radius of the central body (m).
getReferenceTimeSystem() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage: Get the time system used as a reference to define a time system.
getReferenceTrajectories() - Method in class org.orekit.estimation.sequential.KalmanModel: Getter for the reference trajectories.
getReferenceValue() - Method in class org.orekit.utils.ParameterDriver: Get reference parameter value.
getRefFrame() - Method in class org.orekit.files.ccsds.definitions.ModifiedFrame: Get the CCSDS reference frame.
getRefFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the value of REF_FRAME as an Orekit Frame.
getRefFrame() - Method in class org.orekit.files.ilrs.CPFHeader: Get the reference frame.
getRefFrameId() - Method in class org.orekit.files.ilrs.CPFHeader: Get the reference frame identifier.
getReflectance() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties: Get the typical (50th percentile) coefficient of reflectance.
getReflection() - Method in class org.orekit.forces.Panel: Get radiation pressure specular reflection coefficient.
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.EarthStandardAtmosphereRefraction
getRefraction(double) - Method in class org.orekit.models.earth.ITURP834AtmosphericRefraction: Compute the refraction angle from the true (geometrical) elevation.
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.
getRegionCode() - Method in class org.orekit.files.rinex.navigation.IonosphereKlobucharMessage: Get the region code.
getRegistrationAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord: Get the web or mail address for registration.
getRelativeMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm: Get the file metadata.
getRelativeMetadata() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get the relative metadata following header, they are the common metadata for the CDM.
getRelativePosition() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the Object2’s position vector relative to Object1's at TCA in RTN frame, getX for R component, getY for T component, getZ for N component.
getRelativeSpeed() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the norm of relative velocity vector at TCA.
getRelativeVelocity() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the Object2’s velocity vector relative to Object1's at TCA in RTN frame, getX for R component, getY for T component, getZ for N component.
getRelaxationTime() - Method in class org.orekit.models.earth.displacement.PsdCorrection: Get relaxation time.
getRemainingDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: Get the total ΔV remaining for spacecraft.
getRemoteClock() - Method in class org.orekit.estimation.measurements.gnss.AbstractInterSatellitesMeasurement: Get emitting satellite clock provider.
getRemoteClock() - Method in class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement: Get emitting satellite clock provider.
getRemoteClock() - Method in class org.orekit.estimation.measurements.gnss.AbstractOneWayGNSSMeasurement: Get emitting satellite clock provider.
getRemoteClock(int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement: Get emitting satellite clock provider.
getRemoteOffset() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithDerivatives: Get remote clock offset.
getRemoteOffset() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithoutDerivatives: Get remote clock offset.
getRemotePV() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithDerivatives: Get remote satellite position/velocity.
getRemotePV() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithoutDerivatives: Get remote satellite position/velocity.
getRemotePV(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.AbstractInterSatellitesMeasurement: Get emitting satellite position/velocity provider.
getRemotePV(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement: Get emitting satellite position/velocity provider.
getRemotePV(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.AbstractOneWayGNSSMeasurement: Get emitting satellite position/velocity provider.
getRemotePV(SpacecraftState[], int) - Method in class org.orekit.estimation.measurements.gnss.AbstractInterSatellitesMeasurement: Get emitting satellite position/velocity provider.
getRemotePV(SpacecraftState[], int) - Method in class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement: Get emitting satellite position/velocity provider.
getRemotePV(SpacecraftState[], int) - Method in class org.orekit.estimation.measurements.gnss.AbstractOneWayGNSSMeasurement: Get emitting satellite position/velocity provider.
getRemoteRate() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithDerivatives: Get remote clock rate.
getRemoteRate() - Method in class org.orekit.estimation.measurements.gnss.OnBoardCommonParametersWithoutDerivatives: Get remote clock rate.
getrEq() - Method in class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term: Getter for central body equatorial radius.
getrEq() - Method in class org.orekit.forces.gravity.J2OnlyPerturbation: Getter for equatorial radius.
getReserved03() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A: Get the reserved field in word 3.
getReserved03() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B: Get the reserved field in word 3.
getReserved04() - Method in class org.orekit.gnss.rflink.gps.SubFrame1: Get the reserved field in word 4.
getReserved04() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A: Get the reserved field in word 4.
getReserved04() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B: Get the reserved field in word 4.
getReserved05() - Method in class org.orekit.gnss.rflink.gps.SubFrame1: Get the reserved field in word 5.
getReserved05() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A: Get the reserved field in word 5.
getReserved05() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B: Get the reserved field in word 5.
getReserved06() - Method in class org.orekit.gnss.rflink.gps.SubFrame1: Get the reserved field in word 6.
getReserved06() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A: Get the reserved field in word 6.
getReserved06() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B: Get the reserved field in word 6.
getReserved07() - Method in class org.orekit.gnss.rflink.gps.SubFrame1: Get the reserved field in word 7.
getReserved07() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A: Get the reserved field in word 7.
getReserved07() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B: Get the reserved field in word 7.
getReserved08() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A: Get the reserved field in word 8.
getReserved08() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B: Get the reserved field in word 8.
getReserved09() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B: Get the reserved field in word 9.
getReserved10() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A: Get the reserved field in word 10.
getReserved10() - Method in class org.orekit.gnss.rflink.gps.SubFrame4B: Get the reserved field in word 10.
getReserved10() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get reserved field in word 10.
getReserved10() - Method in class org.orekit.gnss.rflink.gps.SubFrame4E: Get the reserved field in word 10.
getReserved8() - Method in class org.orekit.gnss.rflink.gps.SubFrame4E: Get the reserved field in word 8.
getReservedA09() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A: Get the reserved field A in word 9.
getReservedA10() - Method in class org.orekit.gnss.rflink.gps.SubFrame5B: Get the reserved field A in word 10.
getReservedB09() - Method in class org.orekit.gnss.rflink.gps.SubFrame4A: Get the reserved field B in word 9.
getReservedB10() - Method in class org.orekit.gnss.rflink.gps.SubFrame5B: Get the reserved field B in word 10.
getResetAtEnd() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Getter for the resetting flag regarding initial state.
getResetAtEnd() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Getter for the resetting flag regarding initial state.
getResidualsAccepted() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters: Get the percentage of residuals accepted in the OD of the object (from 0 to 100).
getResults() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector: Get on all the results computed by the detector (e.g.: dates of cycle-slip).
getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the retrograde factor.
getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements: Get the retrograde factor.
getReturnRate() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the return rate.
getReturnRate() - Method in class org.orekit.files.ilrs.CRD.NptRangeMeasurement: Get the return rate.
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.
getRms() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the rms of raw system delay.
getRms() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics: Get the session RMS from the mean of raw accepted time-of-flight values minus the trend function.
getRms() - Method in class org.orekit.propagation.analytical.tle.generation.LeastSquaresTleGenerationAlgorithm: Get the Root Mean Square of the TLE estimation.
getRMS() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the Root Mean Square Deviation of the fitting.
getRMS() - Method in class org.orekit.propagation.conversion.osc2mean.LeastSquaresConverter: Gets the RMS for the last conversion.
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.DSSTGravityContext: Get roa = R / a.
getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTGravityContext: Get roa = R / a.
getRollOverCycle() - Method in enum org.orekit.time.GNSSDate.GNSSDateType: Get the number of week in one rollover cycle.
getRolloverReference() - Static method in class org.orekit.time.GNSSDate: Get the reference date ensuring continuity across GNSS week rollover.
getRollOverWeek(SatelliteSystem) - Static method in enum org.orekit.time.GNSSDate.GNSSDateType: Get the number of week in one rollover cycle for the given satellite system.
getRoot() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter: Get root element for XML files.
getRoot() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter: Get root element for XML files.
getRoot() - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter: Get root element for XML files.
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 interface org.orekit.frames.FieldStaticTransform: Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.frames.FieldTransform: Get the underlying elementary rotation.
getRotation() - Method in interface org.orekit.frames.StaticTransform: Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.frames.Transform: Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.utils.AngularCoordinates: Get the rotation.
getRotation() - Method in class org.orekit.utils.FieldAngularCoordinates: Get the rotation.
getRotationAcceleration() - Method in class org.orekit.attitudes.Attitude: Get the satellite rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.attitudes.FieldAttitude: Get the satellite rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.frames.FieldTransform: Get the second time derivative of the rotation.
getRotationAcceleration() - Method in class org.orekit.frames.Transform: Get the second time derivative of the rotation.
getRotationAcceleration() - Method in class org.orekit.utils.AngularCoordinates: Get the rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.utils.FieldAngularCoordinates: Get the rotation acceleration.
getRotationalAngleType() - Method in class org.orekit.files.ilrs.CPFHeader: Get the rotation angle type.
getRotationAngles() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler: Get the coordinates of the Euler angles.
getRotationRate() - Method in interface org.orekit.frames.FieldKinematicTransform: Get the first time derivative of the rotation.
getRotationRate() - Method in class org.orekit.frames.FieldTransform: Get the first time derivative of the rotation.
getRotationRate() - Method in interface org.orekit.frames.KinematicTransform: 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.
getRoundedTime(TimeUnit) - Method in class org.orekit.time.TimeOffset: Get the time in some unit.
getRoutingIndicator() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current RoutingIndicatorTerm value.
getRoutingIndicator() - Method in class org.orekit.files.iirv.IIRVVector: Gets the routing indicator term.
getRTNCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData: Get the covariance matrix logical block.
getRTNCovarianceMatrix() - Method in class org.orekit.files.ccsds.ndm.cdm.RTNCovariance: Get the RTN covariance matrix.
getRunByName() - Method in class org.orekit.files.rinex.section.RinexBaseHeader: Getter for the run/by name.
getS() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey: Get s.
getS1() - Method in class org.orekit.models.earth.ionosphere.nequick.Ray: Get the distance of the first point from the ray perigee.
getS10() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters: Get the EUV index (26-34 nm) scaled to F10.
getS10(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData: Get the EUV index (26-34 nm) scaled to F10.
getS10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Get the EUV index (26-34 nm) scaled to F10.
getS10B() - Method in class org.orekit.models.earth.atmosphere.data.SOLFSMYDataLoader.LineParameters: Get the EUV 81-day averaged centered index.
getS10B(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.JB2008SpaceEnvironmentData: Get the EUV 81-day averaged centered index.
getS10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters: Get the EUV 81-day averaged centered index.
getS2() - Method in class org.orekit.models.earth.ionosphere.nequick.Ray: Get the distance of the second point from the ray perigee.
getS2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTJ2SquaredClosedFormContext: Get the sine of the inclination to the power 2.
getS2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTJ2SquaredClosedFormContext: Get the sine of the inclination to the power 2.
getSample() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the states sample.
getSatConfiguration() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGPSAlmanac: Gets the satellite configuration.
getSatConfiguration() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Gets the satellite configuration.
getSatellite() - Method in class org.orekit.files.rinex.observation.GlonassSatelliteChannel: Get the satellite identifier.
getSatellite() - Method in class org.orekit.files.rinex.observation.ObservationDataSet: Get observed satellite.
getSatellite() - Method in class org.orekit.files.sinex.SatelliteDifferentialSignalBias: Return the satellite identifier.
getSatellite() - Method in class org.orekit.files.sinex.SatelliteObservableSpecificSignalBias: Return the satellite identifier.
getSatellite() - Method in class org.orekit.orbits.WalkerConstellationSlot: Get the satellite index in plane.
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(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.
getSatelliteID() - Method in class org.orekit.files.iirv.IIRVBuilder: Returns the satellite ID (set to the value of the VehicleIdCodeTerm).
getSatelliteID() - Method in class org.orekit.files.iirv.IIRVMessage: Returns the satellite ID (set to the value of the VehicleIdCodeTerm).
getSatelliteID() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionData: Get the satellite ID.
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.
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.
getSatelliteReferenceDatum() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmOrbitCorrectionHeader: Get the satellite reference datum.
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.generation.MeasurementBuilder: Get the satellites related to this measurement.
getSatellites() - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder: 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.acm.Acm: Get the loaded ephemeris for each satellite in the file.
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.iirv.IIRVEphemerisFile: 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.rinex.clock.RinexClock: Getter for the satellites.
getSatellites() - Method in class org.orekit.files.sp3.SP3
getSatellites() - Method in class org.orekit.files.stk.STKEphemerisFile: Get the loaded ephemeris for each satellite in the file.
getSatellitesAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader: Get parsed satellites antennas.
getSatellitesDsb() - Method in class org.orekit.files.sinex.SinexBias: Get the DSB data for satellites.
getSatellitesOsb() - Method in class org.orekit.files.sinex.SinexBias: Get the OSB data for satellites.
getSatellitesPhaseCenters() - Method in class org.orekit.files.sinex.Sinex: Get the parsed satellites phase centers.
getSatelliteSystem() - Method in class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet: Get Satellite System.
getSatelliteSystem() - Method in class org.orekit.files.rinex.AppliedDCBS: Get the satellite system.
getSatelliteSystem() - Method in class org.orekit.files.rinex.AppliedPCVS: Get the satellite system.
getSatelliteSystem() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the satellite system.
getSatelliteSystem() - Method in class org.orekit.files.rinex.observation.PhaseShiftCorrection: Get the Satellite System.
getSatelliteSystem() - Method in class org.orekit.files.rinex.section.RinexBaseHeader: Getter for the satellite system.
getSatelliteSystem() - Method in interface org.orekit.gnss.GnssSignal: Get the satellite system for which this frequency is defined.
getSatelliteSystem() - Method in class org.orekit.gnss.metric.messages.rtcm.correction.RtcmCorrectionMessage: Get the satellite system associated to the message.
getSatelliteSystem() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmMessage: Get the satellite system associated to the message.
getSatelliteSystem() - Method in enum org.orekit.gnss.PredefinedGnssSignal: Get the satellite system for which this frequency is defined.
getSatelliteSystem() - Method in enum org.orekit.time.GNSSDate.GNSSDateType: Get the satellite system.
getSatelliteType() - Method in class org.orekit.gnss.antenna.SatelliteAntenna: Get satellite type.
getSatelliteType() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for satellite type.
getSatelliteType() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for satellite type.
getSatH() - Method in class org.orekit.models.earth.ionosphere.nequick.Ray: Get satellite altitude.
getSatIds() - Method in class org.orekit.files.sp3.SP3Header: Get the satellite identifiers.
getSatInSystem() - Method in class org.orekit.gnss.antenna.SatelliteAntenna: Get satellite in system.
getSatsCorrected() - Method in class org.orekit.files.rinex.observation.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
getSbasId() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage: Get the SBAS Id.
getSBASNavigationMessages() - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get all the SBAS navigation messages contained in the file.
getSBASNavigationMessages(String) - Method in class org.orekit.files.rinex.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.estimation.sequential.AbstractKalmanEstimator: Get the parameter scaling factors.
getScale() - Method in class org.orekit.estimation.sequential.KalmanEstimator: Get the parameter scaling factors.
getScale() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator: Get the parameter scaling factors.
getScale() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel: Getter for the scale.
getScale() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimator: Get the parameter scaling factors.
getScale() - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimator: Get the parameter scaling factors.
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.
getScaleFactorCorrections(SatelliteSystem) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the list of scale factor correction.
getScalePositionDefects() - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting: Getter for scale of position defects.
getScales() - Method in class org.orekit.control.indirect.shooting.AbstractFixedInitialCartesianSingleShooting: Protected getter for the differentiation scales.
getScaleVelocityDefects() - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting: Getter for scale of velocity defects.
getScLat() - Method in class org.orekit.models.earth.ionosphere.nequick.Ray: Get the ray-perigee latitude sin/cos.
getSclkOffsetAtEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the spacecraft clock count at OcmMetadata.getEpochT0().
getSclkSecPerSISec() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the number of spacecraft clock seconds occurring during one SI second.
getScreenEntryTime() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the time in UTC when Object2 enters the screening volume.
getScreenExitTime() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the time in UTC when Object2 exits the screening volume.
getScreeningDataSource() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata: Get the source (or origin) of the specific orbital data for this object.
getScreenPcThreshold() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the collision probability screening threshold used to identify this conjunction.
getScreenType() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the type of screening to be used.
getScreenVolumeFrame() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the name of the Object1 centered reference frame in which the screening volume data are given.
getScreenVolumeRadius() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the screen volume radius.
getScreenVolumeShape() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the shape of the screening volume.
getScreenVolumeX() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the R or T (depending on if RTN or TVN is selected) component size of the screening volume in the corresponding frame.
getScreenVolumeY() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the T or V (depending on if RTN or TVN is selected) component size of the screening volume in the corresponding frame.
getScreenVolumeZ() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the N component size of the screening volume in the corresponding frame.
getSecInDay() - Method in class org.orekit.time.GLONASSDate: Get the number of seconds since N_a start.
getSecond() - Method in class org.orekit.time.FieldTimeStampedPair: Get second time stamped value.
getSecond() - Method in class org.orekit.time.TimeComponents: Get the seconds number.
getSecond() - Method in class org.orekit.time.TimeStampedPair: Get second time stamped value.
getSecondary() - Method in class org.orekit.bodies.CR3BPSystem: Get the secondary CelestialBody.
getSecondary() - Method in class org.orekit.estimation.measurements.gnss.Dipole: Get the secondary dipole vector.
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.
getSecondaryPVProvider() - Method in class org.orekit.propagation.events.ExtremumApproachDetector: Get the secondary position-velocity provider stored in this instance.
getSecondaryPVProvider() - Method in class org.orekit.propagation.events.FieldExtremumApproachDetector: Get the secondary position-velocity provider stored in this instance.
getSecondaryPVProvider() - Method in class org.orekit.propagation.events.FieldRelativeDistanceDetector: Get the secondary position-velocity provider stored in this instance.
getSecondaryPVProvider() - Method in class org.orekit.propagation.events.RelativeDistanceDetector: Get the secondary position-velocity provider stored in this instance.
getSecondaryStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange: Get the secondary ground station reflecting the signal.
getSecondFrequencyPhaseHistory() - Method in class org.orekit.estimation.measurements.filtering.DualFrequencyHatchFilter: Get the history of phase values of the second frequency.
getSeconds() - Method in class org.orekit.time.TimeOffset: Get the normalized seconds part of the time.
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.
getSecondsInWeek() - Method in class org.orekit.time.GNSSDate: Get the number of seconds since week start.
getSecondsOfWeek() - Method in class org.orekit.files.sp3.SP3Header: Returns the seconds of the GPS week as contained in the SP3 file.
getSecondStation() - Method in class org.orekit.estimation.measurements.FDOA: Get the second ground station, the one that gives the measurement.
getSecondStation() - Method in class org.orekit.estimation.measurements.TDOA: Get the second ground station, the one that gives the measurement.
getSecularDegree() - Method in class org.orekit.utils.SecularAndHarmonic: Get degree of polynomial secular part.
getSedr() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the amount of energy being removed from the object’s orbit by atmospheric drag.
getSedr() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get Specific Energy Dissipation Rate.
getSefiCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the Space Environment Fragmentation Impact probability.
getSefiCollisionProbabilityMethod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the Space Environment Fragmentation Impact probability method.
getSefiFragmentationModel() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the Space Environment Fragmentation Impact fragmentation model.
getSegment() - Method in class org.orekit.files.iirv.IIRVEphemerisFile.IIRVEphemeris: Get the IIRVSegment for this satellite.
getSegments() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmSatelliteEphemeris: Get the segments of the attitude ephemeris.
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.iirv.IIRVEphemerisFile.IIRVEphemeris: 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.SP3Ephemeris: Get the segments of the ephemeris.
getSegments() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris
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.
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.
getSensorFrequency() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor: Get frequency of sensor data for sensor.
getSensorNoiseCovariance() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor: Get standard deviation of sensor noise for sensor.
getSensorNumber() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor: Get number of the sensor.
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.
getSensorsUsed() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination: Get sensors used.
getSensorUsed() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor: Get sensor used.
getSeparation() - Method in class org.orekit.utils.OccultationEngine.FieldOccultationAngles: Get apparent separation between occulting and occulted directions.
getSeparation() - Method in class org.orekit.utils.OccultationEngine.OccultationAngles: Get apparent separation between occulting and occulted directions.
getSequenceNumber() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current SequenceNumberTerm value.
getSequenceNumber() - Method in class org.orekit.files.iirv.IIRVVector: Gets the sequence number term.
getSequenceNumber() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the ephemeris sequence number.
getSerialNumber() - Method in class org.orekit.files.sinex.AntennaKey: Get the serial number.
getSerialNumber() - Method in class org.orekit.gnss.antenna.ReceiverAntenna: Get the serial number.
getSessionStatisticsData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the session statistics data for the data block.
getSessionStatisticsRecord() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the default (the first if there are many records) SessionStat record.
getSessionStatisticsRecord(String) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock: Get the session statistics record related to the systemConfigurationId.
getSh() - Method in class org.orekit.models.earth.troposphere.FieldTroposphericDelay: Get slanted delay (m).
getSh() - Method in class org.orekit.models.earth.troposphere.TroposphericDelay: Get slanted delay (m).
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.
getShiftTypeIndicator() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the calibration shift type indicator.
getShootingPropagationSettings() - Method in class org.orekit.control.indirect.shooting.ShootingBoundaryOutput: Getter for the shooting propagation settings.
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.
getSig3EigVec3CovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData: Get the Sigma / Eigenvector covariance logical block.
getSigma() - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter: Get the current value of sigma.
getSigmaU() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination: Get rate random walk if AttitudeDetermination.rateStates is RateElementsType.GYRO_BIAS.
getSigmaV() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination: Get angle random walk if AttitudeDetermination.rateStates is RateElementsType.GYRO_BIAS.
getSign() - Method in class org.orekit.bodies.SexagesimalAngle: Get sign.
getSignal(SatelliteSystem) - Method in interface org.orekit.gnss.ObservationType: Get the signal for a specified satellite system.
getSignal(SatelliteSystem) - Method in enum org.orekit.gnss.PredefinedObservationType: Get the signal for a specified satellite system.
getSignalCode() - Method in interface org.orekit.gnss.ObservationType: Get the signal code.
getSignalCode() - Method in enum org.orekit.gnss.PredefinedObservationType: Get the signal code.
getSignalID() - Method in class org.orekit.gnss.metric.messages.common.CodeBias: Get the GNSS signal and tracking mode identifier.
getSignalID() - Method in class org.orekit.gnss.metric.messages.common.PhaseBias: Get the GNSS signal and tracking mode identifier.
getSignalStrength() - Method in class org.orekit.files.rinex.observation.ObservationData: Get the signal strength.
getSignalStrengthUnit() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the unit of the carrier to noise ratio observables.
getSignalWideLaneIntegerIndicator() - Method in class org.orekit.gnss.metric.messages.common.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.
getSineAz() - Method in class org.orekit.models.earth.ionosphere.nequick.Ray: Get the sine of azimuth of satellite as seen from ray-perigee.
getSinexCode() - Method in class org.orekit.gnss.antenna.Antenna: Get the sinex code of the antenna.
getSingleDateDetectionAdaptableInterval() - Static method in class org.orekit.propagation.events.intervals.DateDetectionAdaptableIntervalFactory: Return a candidate AdaptableInterval for single date detection.
getSingleDateDetectionFieldAdaptableInterval() - Static method in class org.orekit.propagation.events.intervals.DateDetectionAdaptableIntervalFactory: Return a candidate FieldAdaptableInterval for single date detection.
getSingularityThreshold() - Method in class org.orekit.control.indirect.shooting.NewtonFixedBoundaryCartesianSingleShooting: Getter for singularity threshold in LU decomposition.
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.FieldGalileoNavigationMessage: Getter for the signal in space accuracy (m).
getSisa() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage: Getter for the signal in space accuracy (m).
getSisaiOc1() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for Signal In Space Accuracy Index (clock drift accuracy).
getSisaiOc1() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for Signal In Space Accuracy Index (clock drift accuracy).
getSisaiOc2() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for Signal In Space Accuracy Index (clock drift rate accuracy).
getSisaiOc2() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for Signal In Space Accuracy Index (clock drift rate accuracy).
getSisaiOcb() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for Signal In Space Accuracy Index (radial and clock).
getSisaiOcb() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for Signal In Space Accuracy Index (radial and clock).
getSisaiOe() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for Signal In Space Accuracy Index (along track and across track).
getSisaiOe() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for Signal In Space Accuracy Index (along track and across track).
getSismai() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for Signal In Space Monitoring Accuracy Index.
getSismai() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for Signal In Space Monitoring Accuracy Index.
getSiteCode() - Method in class org.orekit.files.sinex.Station: Get the site code (station identifier).
getSiteCode() - Method in class org.orekit.files.sinex.StationDifferentialSignalBias: Get the site code (station identifier).
getSiteCode() - Method in class org.orekit.files.sinex.StationObservableSpecificSignalBias: 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.
getSkew() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the skew of raw system delay values from the mean.
getSkewness() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics: Get the session skewness from the mean of raw accepted time-of-flight values minus the trend function.
getSkimmingAltitude() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector: Get the skimming altitude.
getSlope() - Method in class org.orekit.time.OffsetModel: Offset slope in nanoseconds per UTC second (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.FieldGnssOrbitalElements: Get semi-major axis.
getSma() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Get 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.
getSmaDriver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements: Get semi-major axis.
getSmoothedData() - Method in class org.orekit.estimation.measurements.filtering.SmoothedObservationDataSet: Get the smoothed observation data.
getSnm() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data: Get the sine parameters of spherical harmonics expansion of degree N and order M.
getSnr() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement: Get the signal to noise ratio.
getSoftwareId() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Get the software configuration ID.
getSoftwareRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration: Get the software configuration record.
getSoftwareRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Get software configuration record related to the systemRecord.
getSolarRadArea() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters: Get the solar radiation pressure area.
getSolarRadCoeff() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters: Get the solar radiation pressure coefficient.
getSolarRadiationPressure() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMetadata: Get Enum YesNoUnknown that indicates if Solar Radiation Pressure is taken into account or not.
getSolarReflectivityCoefficient() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current SolarReflectivityCoefficientTerm value.
getSolarReflectivityCoefficient() - Method in class org.orekit.files.iirv.IIRVVector: Gets the solar reflectivity coefficient term.
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.ccsds.ndm.adm.acm.AttitudeDetermination: Get source of attitude estimate.
getSource() - Method in class org.orekit.files.ilrs.CPFHeader: Get the ephemeris source.
getSource() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGPSAlmanac: Gets the source of this GPS almanac.
getSource() - Method in class org.orekit.propagation.analytical.gnss.data.FieldQZSSAlmanac: Gets the source of this QZSS almanac.
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.files.rinex.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.files.rinex.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.AttitudeEndpoints: 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.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() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the calibration span.
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.
getSpareTerm() - Method in class org.orekit.files.iirv.IIRVVector: Gets the spare character term (ASCII space).
getSpatialFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the spatial filter.
getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser: Get the non-default token builders for special XML elements.
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.
getSplitSecond() - Method in class org.orekit.time.TimeComponents: Get the seconds number.
getSplitSecondsInLocalDay() - Method in class org.orekit.time.TimeComponents: Get the second number within the local day, without applying the offset from UTC.
getSplitSecondsInUTCDay() - Method in class org.orekit.time.TimeComponents: Get the second number within the UTC day, applying the offset from UTC.
getSplitSecondsInWeek() - Method in class org.orekit.time.GNSSDate: Get the number of seconds since week start.
getSqrtA() - Method in class org.orekit.gnss.rflink.gps.SubFrame2: Get √a.
getSqrtA() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac: Get √a.
getSqrtA() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Getter for Square Root of Semi-Major Axis (√m).
getSqrtA() - Method in class org.orekit.propagation.analytical.gnss.data.FieldAbstractNavigationMessage: Getter for Square Root of Semi-Major Axis (√m).
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.OrbitPhysicalProperties: Get the nominal SRP coefficient.
getSrpConstantArea() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: 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.OrbitPhysicalProperties: 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.rtcm.correction.RtcmCorrectionHeader: Get the SSR Provider ID.
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.rtcm.correction.RtcmCorrectionHeader: Get the SSR Solution 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.rtcm.correction.RtcmCorrectionHeader: Get the SSR Update Interval.
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() - Static method in class org.orekit.models.earth.troposphere.ModifiedSaastamoinenModel: Create a new Saastamoinen model using a standard atmosphere model.
getStandardModel(double, Unit) - Static method in class org.orekit.models.earth.troposphere.MendesPavlisModel: Create a new Mendes-Pavlis 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.acm.AcmSatelliteEphemeris: Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory: Get the start date of this ephemeris segment.
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.iirv.IIRVEphemerisFile.IIRVEphemeris: Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.iirv.IIRVSegment: Get the start date of this ephemeris segment.
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.SP3Ephemeris: Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.sp3.SP3Segment: Get the start date of this ephemeris segment.
getStart() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris
getStart() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
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.files.rinex.clock.RinexClock.ReferenceClock: Getter for the validity period start date.
getStartDate() - Method in class org.orekit.files.sinex.ParseInfo: Get start date.
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.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).
getStartScreenPeriod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the start time in UTC of the screening period for the conjunction assessment.
getStartTime() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata: Get the time of the earliest data contained in the OCM.
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.
getStartYear() - Method in class org.orekit.files.iirv.IIRVEphemerisFile: Gets the start year for this file.
getStartYear() - Method in class org.orekit.files.iirv.IIRVEphemerisFile.IIRVEphemeris: Gets the start year of the ephemeris data.
getStartYear() - Method in class org.orekit.files.iirv.IIRVSegment: Gets the start year for this segment.
getState() - Method in class org.orekit.estimation.measurements.CommonParametersWithDerivatives: Get spacecraft state.
getState() - Method in class org.orekit.estimation.measurements.CommonParametersWithoutDerivatives: Get spacecraft state.
getState() - Method in class org.orekit.estimation.sequential.PhysicalEstimatedState: Get the physical state.
getState() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent: Get the triggering state.
getState() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent: Get the triggering state.
getState() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event: Get the spacecraft's state at the event.
getState() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event: Get the spacecraft's state at the event.
getState(ParameterDriversProvider) - Method in class org.orekit.propagation.integration.AbstractGradientConverter: Get the state with the number of parameters consistent with parametric model.
getStateCovariance(SpacecraftState) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider: Get the state covariance in the same frame/local orbital frame, orbit type and position angle as the initial covariance.
getStateCovariance(SpacecraftState, Frame) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider: Get the state covariance expressed in a given frame.
getStateCovariance(SpacecraftState, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.StateCovarianceMatrixProvider: Get the state covariance expressed in a given orbit type.
getStateDerivatives(int) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the partial derivatives of the simulated measurement with respect to state Cartesian coordinates.
getStateInterpolator() - Method in class org.orekit.propagation.analytical.Ephemeris: Get state interpolator.
getStates() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase: 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 interface org.orekit.propagation.MatricesHarvester: Extract state transition matrix from state.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations: Method returning the State Transition Matrix.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester: Extract state transition matrix from state.
getStateType() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder: Get the type of the elements used to define the orbital state (mean or osculating).
getStateVectorBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData: Get the state vector logical block.
getStateVectorBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData: Get the state vector logical block.
getStaticInverse() - Method in interface org.orekit.frames.FieldStaticTransform: Get the inverse transform of the instance in static form (without rates).
getStaticInverse() - Method in interface org.orekit.frames.StaticTransform: Get the inverse transform of the instance in static form (without rates).
getStaticTransform(AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider: Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation: Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter: Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.L1TransformProvider: Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in class org.orekit.frames.ShiftingTransformProvider: Get a transform for only rotations and translations on the specified date.
getStaticTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider: Get a transform for only rotations and translations on the specified date.
getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get a transform for only rotations and translations on the specified date.
getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider: Get a transform for only rotations and translations on the specified date.
getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.HelmertTransformation: Get a transform for only rotations and translations on the specified date.
getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter: Get a transform for only rotations and translations on the specified date.
getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.L1TransformProvider: Get a transform for only rotations and translations on the specified date.
getStaticTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ShiftingTransformProvider: Get a transform for only rotations and translations on the specified date.
getStaticTransform(FieldAbsoluteDate<T>) - Method in interface org.orekit.frames.TransformProvider: Get a transform for only rotations and translations on the specified date.
getStaticTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame: Get the static portion of the transform from the instance to another frame.
getStaticTransformTo(Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.Frame: Get the static portion of the transform from the instance to another frame.
getStation() - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement: Get the ground station from which measurement is performed.
getStationClockAndDriftApplied() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Get the station clock offset and drift applied indicator.
getStationDownlink() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithDerivatives: Get station position in inertial frame at end of the downlink leg.
getStationDownlink() - Method in class org.orekit.estimation.measurements.GroundReceiverCommonParametersWithoutDerivatives: Get station position in inertial frame at end of the downlink leg.
getStationIdentifier() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the station identifier.
getStationInformation() - Method in class org.orekit.files.rinex.section.RinexBaseHeader: Getter for the station information.
getStationName() - Method in class org.orekit.files.ilrs.CRDHeader: Get the station name from official list.
getStationName() - Method in class org.orekit.files.rinex.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.Sinex: Get the parsed station data.
getStationsDsb() - Method in class org.orekit.files.sinex.SinexBias: Get the DSB data for stations.
getStationsOsb() - Method in class org.orekit.files.sinex.SinexBias: Get the OSB data for stations.
getStationUTCOffset() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration: Get the estimated station UTC offset.
getStatus() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase: Get the status.
getStatusFlags() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Get status flags.
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.
getStep() - Method in class org.orekit.propagation.conversion.AbstractFixedSingleStepIntegratorBuilder: Getter for the step size.
getStep() - Method in class org.orekit.propagation.conversion.AbstractFixedStepFieldIntegratorBuilder: Getter for the step size (s).
getSTKVersion() - Method in class org.orekit.files.stk.STKEphemerisFile: Returns the STK version string.
getStm(Orbit, double) - Static method in class org.orekit.propagation.StateCovariance: Get the state transition matrix considering Keplerian contribution only.
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.acm.AcmSatelliteEphemeris: Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory: Get the end date of this ephemeris segment.
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.iirv.IIRVEphemerisFile.IIRVEphemeris: Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.iirv.IIRVSegment: Get the end date of this ephemeris segment.
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.SP3Ephemeris: Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.sp3.SP3Segment: Get the end date of this ephemeris segment.
getStop() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemeris
getStop() - Method in class org.orekit.files.stk.STKEphemerisFile.STKEphemerisSegment
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.
getStopNumber() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement: Get the stop number.
getStopScreenPeriod() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the stop time in UTC of the screening period for the conjunction assessment.
getStopTime() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata: Get the time of the latest data contained in the OCM.
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(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.
getStream(T) - Method in class org.orekit.data.AbstractListCrawler: 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.
getSubInterpolators() - Method in class org.orekit.propagation.FieldSpacecraftStateInterpolator: Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.
getSubInterpolators() - Method in class org.orekit.propagation.SpacecraftStateInterpolator: Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.
getSubInterpolators() - Method in class org.orekit.time.AbstractFieldTimeInterpolator: Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.
getSubInterpolators() - Method in class org.orekit.time.AbstractTimeInterpolator: Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.
getSubInterpolators() - Method in interface org.orekit.time.FieldTimeInterpolator: Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.
getSubInterpolators() - Method in interface org.orekit.time.TimeInterpolator: Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.
getSumOfAllConstantDelays() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration: Get the sum of all constant delays (electronic, geometric, optical) that are not included in the time of flight measurements or time- variant or point angle-variant delays in the “42” record below (m, one way).
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.
getSun() - Method in class org.orekit.models.earth.atmosphere.AbstractSunInfluencedAtmosphere: Getter for Sun's position provider.
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.
getSunPosition(AbsoluteDate, Frame) - Method in class org.orekit.models.earth.atmosphere.AbstractSunInfluencedAtmosphere: Method returning the Sun's position vector.
getSunPosition(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.AbstractSunInfluencedAtmosphere: Method returning the Sun's position vector (Field version).
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.AbstractSolarActivityData: Get the supported names regular expression.
getSupportedNames() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
getSupportedNames() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
getSupportIdCode() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current SupportIdCodeTerm value.
getSupportIdCode() - Method in class org.orekit.files.iirv.IIRVVector: Gets the support ID code term.
getSurveyedTargetDistance() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration: Get the surveyed target distance.
getSurveyError() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration: Get the survey error.
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage: Getter for the user SV accuray (meters).
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Getter for the user SV accuray (meters).
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouLegacyNavigationMessage: Getter for the user SV accuray (meters).
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Getter for the user SV accuray (meters).
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.FieldLegacyNavigationMessage: Getter for the user SV accuray (meters).
getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage: 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.gnss.rflink.gps.SubFrame1: Get SV health.
getSvHealth() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac: Get SV health.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Getter for the satellite health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Getter for the satellite health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGalileoNavigationMessage: Getter for the SV health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.FieldIRNSSNavigationMessage: Getter for the satellite health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.FieldLegacyNavigationMessage: Getter for 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.IRNSSNavigationMessage: Getter for the satellite health status.
getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.LegacyNavigationMessage: Getter for the satellite health status.
getSvHealth(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame4E: Get the Sv health for a satellite.
getSvHealth(int) - Method in class org.orekit.gnss.rflink.gps.SubFrame5B: Get the SV Health for a satellite.
getSvId() - Method in class org.orekit.gnss.rflink.gps.SubFrame45: Get SV (page) ID.
getSVN() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGPSAlmanac: Gets the satellite "SVN" reference number.
getSVN() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac: Gets the satellite "SVN" reference number.
getSw() - Method in class org.orekit.models.earth.troposphere.FieldTroposphericDelay: Get wet slanted delay (m).
getSw() - Method in class org.orekit.models.earth.troposphere.TroposphericDelay: Get wet slanted delay (m).
getSwitches() - Method in class org.orekit.attitudes.AttitudesSequence: Gets a deep copy of the switches stored in this instance.
getSystem() - Method in class org.orekit.files.rinex.navigation.TypeSvMessage: Get satellite system.
getSystem() - Method in class org.orekit.gnss.SatInSystem: Get the system this satellite belongs to.
getSystem() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get satellite system.
getSystem(CelestialBody, CelestialBody, double) - Static method in class org.orekit.bodies.CR3BPFactory: Get the corresponding CR3BP System.
getSystemConfigurationId() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the system configuration id.
getSystemConfigurationId() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement: Get the system configuration id.
getSystemConfigurationId() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement: Get the system configuration id.
getSystemConfigurationId() - Method in class org.orekit.files.ilrs.CRD.SessionStatistics: Get system configuration id.
getSystemConfigurationIds() - Method in class org.orekit.files.ilrs.CRDConfiguration: Get a set of configuration ids.
getSystemConfigurationRecords() - Method in class org.orekit.files.ilrs.CRDConfiguration: Get a list of system configurations.
getSystemDelay() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the calibration system delay.
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.files.rinex.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.
getSystemRecord(String) - Method in class org.orekit.files.ilrs.CRDConfiguration: Get system configuration record.
getSystemTimeOffsets() - Method in class org.orekit.files.rinex.navigation.RinexNavigation: Get the system time offsets.
getT() - Method in class org.orekit.orbits.WalkerConstellation: Get the total number of satellites.
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.adm.acm.AcmMetadata: Get the difference (TAI – UTC) in seconds at epoch AcmMetadata.getEpochT0().
getTaimutcT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the difference (TAI – UTC) in seconds at epoch OcmMetadata.getEpochT0().
getTargetAttitude() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver: Get target attitude (if purpose is attitude adjustment).
getTargetClass() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the target class.
getTargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedFieldPVCoordinates<T>, Frame) - Method in class org.orekit.attitudes.GroundPointTarget: Get a target vector.
getTargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedFieldPVCoordinates<T>, Frame) - Method in interface org.orekit.attitudes.TargetProvider: Get a target vector.
getTargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedPVCoordinates, Frame) - Method in class org.orekit.attitudes.GroundPointTarget: Get a target vector.
getTargetDirection(ExtendedPositionProvider, OneAxisEllipsoid, TimeStampedPVCoordinates, Frame) - Method in interface org.orekit.attitudes.TargetProvider: Get a target vector.
getTargetLocation() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the target location.
getTargetMomentum() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver: Get target momentum (if purpose is momentum desaturation).
getTargetMomFrame() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver: Get reference frame for AttitudeManeuver.getTargetMomentum().
getTargetName() - Method in class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration: Get the target name or ID.
getTargetPosition(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing: Compute the target point position in specified frame.
getTargetPosition(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing: Compute the target point position in specified frame.
getTargetPosition(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointingAttitudeModifier: Compute the target point position in specified frame.
getTargetPosition(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing: Compute the target point position in specified frame.
getTargetPosition(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.NadirPointing: Compute the target point position in specified frame.
getTargetPosition(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TargetPointing: Compute the target point position in specified frame.
getTargetPosition(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing: Compute the target point position in specified frame.
getTargetPosition(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing: Compute the target point position in specified frame.
getTargetPosition(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointingAttitudeModifier: Compute the target point position in specified frame.
getTargetPosition(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing: Compute the target point position in specified frame.
getTargetPosition(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.NadirPointing: Compute the target point position in specified frame.
getTargetPosition(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TargetPointing: Compute the target point position 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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, 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.GroundPointingAttitudeModifier: 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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, 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.TargetPointing: Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, 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(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointingAttitudeModifier: 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(PVCoordinatesProvider, AbsoluteDate, 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.
getTargetPVViaInterpolation(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.NadirPointing: Compute target position-velocity-acceleration vector via interpolation (Field version).
getTargetPVViaInterpolation(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.NadirPointing: Compute target position-velocity-acceleration vector via interpolation.
getTargetSize() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the size of the target.
getTargetSpinRate() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver: Get target spin rate (if purpose is spin rate adjustment).
getTauC() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the GLONASS time scale correction to UTC time.
getTauD() - Method in class org.orekit.estimation.measurements.CommonParametersWithDerivatives: Get downlink delay.
getTauD() - Method in class org.orekit.estimation.measurements.CommonParametersWithoutDerivatives: Get downlink delay.
getTauGps() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data: Get the correction to GPS time relative to GLONASS time.
getTauMultiplier() - Method in class org.orekit.models.earth.displacement.Tide: Get the multiplier for the τ Doodson argument.
getTC() - Method in class org.orekit.data.DelaunayArguments: Get the offset in Julian centuries.
getTC() - Method in class org.orekit.data.FieldDelaunayArguments: Get the offset in Julian centuries.
getTca() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the date and time in UTC of the closest approach.
getTca() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition: Get the Time of Closest Approach.
getTca() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition: Get the Time of Closest Approach.
getTCB() - Method in class org.orekit.time.LazyLoadedTimeScales
getTCB() - Method in interface org.orekit.time.TimeScales: Get the Barycentric Coordinate Time scale.
getTCB() - Static method in class org.orekit.time.TimeScalesFactory: Get the Barycentric Coordinate Time scale.
getTCG() - Method in class org.orekit.time.LazyLoadedTimeScales
getTCG() - Method in interface org.orekit.time.TimeScales: Get the Geocentric Coordinate Time scale.
getTCG() - Static method in class org.orekit.time.TimeScalesFactory: Get the Geocentric Coordinate Time scale.
getTDB() - Method in class org.orekit.time.LazyLoadedTimeScales
getTDB() - Method in interface org.orekit.time.TimeScales: Get the Barycentric Dynamic Time scale.
getTDB() - Static method in class org.orekit.time.TimeScalesFactory: Get the Barycentric Dynamic Time scale.
getTdim() - Method in class org.orekit.bodies.CR3BPSystem: Get the CR3BP orbital period of m2 around m1.
getTdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the Unique identifier of Tracking Data Message linked to this Orbit Data Message.
getTdop() - Method in class org.orekit.gnss.DOP: Gets the time dilution of precision.
getTechAddress() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the address of Technical Point Of Contact at originator.
getTechEmail() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the email address of Technical Point Of Contact at originator.
getTechOrg() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the creating agency or operator.
getTechPhone() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the phone number of Technical Point Of Contact at originator.
getTechPOC() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the Technical Point Of Contact at originator.
getTechPosition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the position of Technical Point Of Contact at originator.
getTEME() - Method in class org.orekit.frames.AbstractFrames
getTEME() - Method in interface org.orekit.frames.Frames: Get the TEME reference frame.
getTEME() - Static method in class org.orekit.frames.FramesFactory: Get the TEME reference frame.
getTemperature() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement: Get the surface temperature.
getTemperature() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Get the local temperature at the evaluation location.
getTemperature() - Method in class org.orekit.models.earth.weather.FieldPressureTemperature: Get temperature.
getTemperature() - Method in class org.orekit.models.earth.weather.PressureTemperature: Get temperature.
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.
getTerminalCartesianState() - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting: Getter for the target terminal Cartesian state vector.
getTerminalCartesianState() - Method in class org.orekit.control.indirect.shooting.boundary.FixedTimeCartesianBoundaryStates: Getter for the terminal Cartesian condition.
getTerminalOrbit() - Method in class org.orekit.control.indirect.shooting.boundary.FixedTimeBoundaryOrbits: Getter for the terminal condition.
getTerminalState() - Method in class org.orekit.control.indirect.shooting.ShootingBoundaryOutput: Getter for the terminal state.
getText() - Method in class org.orekit.files.rinex.section.RinexComment: Get the text.
getTFirstObs() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get the time of First observation record.
getTGD() - Method in class org.orekit.gnss.rflink.gps.SubFrame1: Get the TGD.
getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Get the estimated group delay differential TGD for L1-L2 correction.
getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCommonGnssData: Get the estimated group delay differential TGD for L1-L2 correction.
getTGD() - Method in interface org.orekit.propagation.analytical.gnss.data.FieldGNSSClockElements: Get the estimated group delay differential TGD for L1-L2 correction.
getTGD() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements: Get the estimated group delay differential TGD for L1-L2 correction.
getTGD1() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage: Getter for the estimated group delay differential TGD1 for B1I signal.
getTGD1() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouLegacyNavigationMessage: Getter for the estimated group delay differential TGD1 for B1I signal.
getTGD2() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage: Getter for the estimated group delay differential TGD for B2I signal.
getTGD2() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouLegacyNavigationMessage: Getter for the estimated group delay differential TGD for B2I signal.
getTgdB1Cp() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for B1/B3 Group Delay Differential (s).
getTgdB1Cp() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for B1/B3 Group Delay Differential (s).
getTgdB2ap() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for B2 AP Group Delay Differential (s).
getTgdB2ap() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for B2 AP Group Delay Differential (s).
getTgdB2bI() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage: Getter for B2B_i / B3I Group Delay Differential (s).
getTgdB2bI() - Method in class org.orekit.propagation.analytical.gnss.data.FieldBeidouCivilianNavigationMessage: Getter for B2B_i / B3I Group Delay Differential (s).
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.
getTheoryName() - Method in class org.orekit.propagation.conversion.osc2mean.BrouwerLyddaneTheory: Gets the name of the theory used for osculating to mean conversion.
getTheoryName() - Method in class org.orekit.propagation.conversion.osc2mean.DSSTTheory: Gets the name of the theory used for osculating to mean conversion.
getTheoryName() - Method in class org.orekit.propagation.conversion.osc2mean.EcksteinHechlerTheory: Gets the name of the theory used for osculating to mean conversion.
getTheoryName() - Method in interface org.orekit.propagation.conversion.osc2mean.MeanTheory: Gets the name of the theory used for osculating to mean conversion.
getTheoryName() - Method in class org.orekit.propagation.conversion.osc2mean.TLETheory: Gets the name of the theory used for osculating to mean conversion.
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.ITURP834AtmosphericRefraction: Get the station elevation angle under free-space propagation .
getThetaMin() - Method in class org.orekit.models.earth.ITURP834AtmosphericRefraction: 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() - 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.CssiSpaceWeatherData: Get the value of the 3 hours geomagnetic index.
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.conversion.osc2mean.FixedPointConverter: Gets convergence threshold.
getThreshold() - Method in class org.orekit.propagation.conversion.osc2mean.LeastSquaresConverter: Gets the convergence threshold.
getThreshold() - Method in class org.orekit.propagation.events.EventDetectionSettings: Getter for threshold.
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.FieldEventDetectionSettings: Getter for threshold.
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.OrbitManeuver: Get thrust.
getThrustAcceleration() - Method in class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters: Get the object’s acceleration due to in-track thrust used to propagate the state vector and covariance to TCA.
getThrustAccelerationVector(double[], double) - Method in interface org.orekit.control.indirect.adjoint.cost.CartesianCost: Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getThrustAccelerationVector(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.CartesianFlightDurationCost: Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getThrustAccelerationVector(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.CartesianFuelCost: Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getThrustAccelerationVector(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.LogarithmicBarrierCartesianFuel: Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getThrustAccelerationVector(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.QuadraticPenaltyCartesianFuel: Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getThrustAccelerationVector(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergyNeglectingMass: Computes the thrust acceleration vector in propagation frame from the adjoint variables and the mass.
getThrustDirection(double[]) - Method in class org.orekit.control.indirect.adjoint.cost.PenalizedCartesianFuelCost: Computes the direction of thrust.
getThrustDirectionSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: Get one σ angular off-nominal thrust direction.
getThrustEfficiency() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: Get thrust efficiency η.
getThrustForceNorm(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.BoundedCartesianEnergy: Computes the Euclidean norm of the thrust force.
getThrustForceNorm(double[], double) - Method in class org.orekit.control.indirect.adjoint.cost.UnboundedCartesianEnergy: Computes the Euclidean norm of the thrust force.
getThrustInterpolation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: Get interpolation mode between current and next thrust line.
getThrustIsp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: Get thrust specific impulse.
getThrustMagnitude() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the thrust magnitude.
getThrustMagnitude() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the thrust magnitude (N).
getThrustMagnitude(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the thrust magnitude.
getThrustMagnitude(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the thrust magnitude (N) at given date.
getThrustMagnitudeSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuver: 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() - 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() - 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.AbstractConstantThrustPropulsionModel: 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(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel: 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(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel: 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).
getThrustVector(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.ProfileThrustPropulsionModel: 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 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.ProfileThrustPropulsionModel: 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(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the thrust vector (N) in S/C frame.
getThrustVector(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel: Get the thrust vector in spacecraft frame (N).
getThrustVector(AbsoluteDate, double) - Method in class org.orekit.forces.maneuvers.propulsion.PolynomialThrustSegment: Get thrust vector at a specified date.
getThrustVector(AbsoluteDate, double) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustVectorProvider: Get thrust vector at a specified date.
getThrustVector(FieldAbsoluteDate<T>, T) - Method in class org.orekit.forces.maneuvers.propulsion.PolynomialThrustSegment: Get thrust vector at a specified date.
getThrustVector(FieldAbsoluteDate<T>, T) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustVectorProvider: Get thrust vector at a specified date.
getThrustVector(T[]) - 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.BasicConstantThrustPropulsionModel: 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).
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.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 class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get 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.
getTimeBiasApplied() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement: Get the time bias applied.
getTimeConverter() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter: Get the current time converter.
getTimeConverter() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter: Get the current time converter.
getTimeDriver() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get the driver for reference time of the GNSS orbit as a duration from week start.
getTimeLastObsEnd() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters: Get the start of a time interval (UTC) that contains the time of the last accepted observation.
getTimeLastObsStart() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters: Get the start of a time interval (UTC) that contains the time of the last accepted observation.
getTimeOfFlight() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement: Get the time-of-flight.
getTimeOffset() - Method in class org.orekit.estimation.measurements.EstimatedMeasurementBase: Get the time offset from first state date to measurement date.
getTimeParameter(AbsoluteDate, AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.AbstractTimeInterpolator: Get the time parameter which lies between [0:1] by normalizing the difference between interpolating time and previous date by the Δt between tabulated values.
getTimeParameter(FieldAbsoluteDate<KK>, FieldAbsoluteDate<KK>, FieldAbsoluteDate<KK>) - Method in class org.orekit.time.AbstractFieldTimeInterpolator: Get the time parameter which lies between [0:1] by normalizing the difference between interpolating time and previous date by the Δt between tabulated values.
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.files.rinex.clock.RinexClock: Getter for the data time scale.
getTimeScale(TimeScales) - Method in enum org.orekit.gnss.ObservationTimeScale: Get 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.files.sinex.AbstractSinex: Get the time scales.
getTimeScales() - Method in class org.orekit.files.sinex.AbstractSinexParser: Get the time scales.
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() - Method in class org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElementsDriversProvider: Get known time scales.
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.
getTimeStampedPVCoordinates(int) - Method in class org.orekit.files.iirv.IIRVVector: Gets the state vector and time data as a TimeStampedPVCoordinates instance.
getTimeSystem() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata: Get the Time System that: for CDM, is used for relative metadata, metadata, OD parameters, state vector.
getTimeSystem() - Method in class org.orekit.files.ccsds.section.Metadata: Get the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.
getTimeSystem() - Method in class org.orekit.files.ccsds.utils.ContextBinding: Get the time system.
getTimeSystem() - Method in class org.orekit.files.rinex.clock.RinexClock: Getter for the file time system.
getTimeSystem() - Method in class org.orekit.files.sinex.BiasDescription: Get the time system for DSB data.
getTimeSystem() - Method in class org.orekit.files.sp3.SP3Header: Returns the TimeSystem used to time-stamp position entries.
getTimeSystemCorrectionA0() - Method in class org.orekit.files.rinex.navigation.TimeSystemCorrection: Getter for the A0 coefficient of the time system correction.
getTimeSystemCorrectionA1() - Method in class org.orekit.files.rinex.navigation.TimeSystemCorrection: Getter for the A1 coefficient of the time system correction.
getTimeSystemCorrections() - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader: Getter for the time system corrections contained in the file header.
getTimeSystemCorrectionType() - Method in class org.orekit.files.rinex.navigation.TimeSystemCorrection: Getter for the time system correction type.
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.
getTimingRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Get timing system configuration record related to the systemRecord.
getTIRF(IERSConventions) - 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) - Static method in class org.orekit.frames.FramesFactory: Get the TIRF reference frame, ignoring tidal effects.
getTIRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
getTIRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames: Get the TIRF reference frame.
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.files.rinex.observation.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.
getTm() - Method in class org.orekit.models.earth.weather.FieldPressureTemperatureHumidity: Get mean temperature weighted with water vapor pressure.
getTm() - Method in class org.orekit.models.earth.weather.PressureTemperatureHumidity: Get mean temperature weighted with water vapor pressure.
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.
getTOA() - Method in class org.orekit.gnss.rflink.gps.SubFrame5B: Get Time of Almanac.
getToaA() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac: Get Time Of Almanac.
getToc() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData: Get the time of clock.
getToc() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCommonGnssData: Get the time of clock.
getToc() - Method in interface org.orekit.propagation.analytical.gnss.data.FieldGNSSClockElements: Get the time of clock.
getToc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements: Get the time of clock.
getToc() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements: Gets the clock correction reference time toc.
getTOC() - Method in class org.orekit.gnss.rflink.gps.SubFrame1: Get the TOC.
getTOD(boolean) - Method in class org.orekit.frames.AbstractFrames
getTOD(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) - Method in class org.orekit.frames.AbstractFrames
getTOD(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames: Get the TOD reference frame.
getTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the TOD reference frame.
getToe() - Method in class org.orekit.gnss.rflink.gps.SubFrame2: Get Time Of Ephemeris.
getToLatitude() - Method in class org.orekit.propagation.events.FieldLatitudeRangeCrossingDetector: Get the fixed latitude range to be crossed (radians), upper boundary.
getToLatitude() - Method in class org.orekit.propagation.events.LatitudeRangeCrossingDetector: Get the fixed latitude range to be crossed (radians), upper boundary.
getToleranceProvider() - Method in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder: Getter for the integration tolerance provider.
getTolerances(FieldVector3D<T>, FieldVector3D<T>) - Method in interface org.orekit.propagation.CartesianToleranceProvider: Retrieve the integration tolerances given reference position and velocity Field vectors.
getTolerances(Vector3D, Vector3D) - Method in interface org.orekit.propagation.CartesianToleranceProvider: Retrieve the integration tolerances given reference position and velocity vectors.
getTolerances(CartesianOrbit) - Method in interface org.orekit.propagation.CartesianToleranceProvider: Retrieve the integration tolerances given a reference Cartesian orbit.
getTolerances(FieldCartesianOrbit<T>) - Method in interface org.orekit.propagation.CartesianToleranceProvider: Retrieve the integration tolerances given a reference Cartesian orbit.
getTolerances(FieldOrbit<T>, OrbitType) - Method in interface org.orekit.propagation.ToleranceProvider: Retrieve the integration tolerances given a reference Field orbit.
getTolerances(FieldOrbit<T>, OrbitType, PositionAngleType) - Method in interface org.orekit.propagation.ToleranceProvider: Retrieve the integration tolerances given a reference Field orbit.
getTolerances(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder: Computes tolerances.
getTolerances(Orbit, OrbitType) - Method in interface org.orekit.propagation.ToleranceProvider: Retrieve the integration tolerances given a reference orbit.
getTolerances(Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder: Computes tolerances.
getTolerances(Orbit, OrbitType, PositionAngleType) - Method in interface org.orekit.propagation.ToleranceProvider: Retrieve the integration tolerances given a reference orbit.
getTolerances(AbsolutePVCoordinates) - Method in interface org.orekit.propagation.CartesianToleranceProvider: Retrieve the integration tolerances given a reference absolute position-velocity vector.
getTolerances(AbsolutePVCoordinates) - Method in class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder: Computes tolerances.
getTolerances(FieldAbsolutePVCoordinates<T>) - Method in interface org.orekit.propagation.CartesianToleranceProvider: Retrieve the integration tolerances given a reference absolute position-velocity vector.
getTolerances(FieldAbsolutePVCoordinates<T>) - Method in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder: Computes tolerances.
getToLongitude() - Method in class org.orekit.propagation.events.FieldLongitudeRangeCrossingDetector: Get the fixed longitude range to be crossed (radians), upper boundary.
getToLongitude() - Method in class org.orekit.propagation.events.LongitudeRangeCrossingDetector: Get the fixed longitude range to be crossed (radians), upper boundary.
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.
getTopocentricFrame() - Method in class org.orekit.propagation.events.FieldElevationExtremumDetector: Returns the topocentric frame centered on ground point.
getTopocentricPosition(FieldTrackingCoordinates<T>) - Static method in class org.orekit.frames.TopocentricFrame: Get the topocentric position from FieldTrackingCoordinates.
getTopocentricPosition(TrackingCoordinates) - Static method in class org.orekit.frames.TopocentricFrame: Get the topocentric position from TrackingCoordinates.
getTorque() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver: Get the torque vector (N.m).
getTot() - Method in class org.orekit.gnss.rflink.gps.SubFrame4D: Get TOT field.
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).
getTotalNumberOfDataLines() - Method in class org.orekit.files.rinex.clock.RinexClock: Get the total number of complete data lines in the file.
getTow() - Method in class org.orekit.gnss.rflink.gps.SubFrame: Get Time Of Week of next 12 second message.
getTrackId() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata: Getter for the tracking data identifier.
getTrackingCoordinates(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame: Get the tracking coordinates of a point with regards to the local point.
getTrackingCoordinates(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame: Get the tracking coordinates of a point with regards to the local point.
getTrackingSoftwares() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Get the tracking softwares.
getTrackingSoftwareVersions() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration: Get the tracking software versions.
getTracksAvailable() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters: Get the number of sensor tracks available for the OD of the object.
getTracksAvailable() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get number of sensors tracks available for the OD within the actual OD span.
getTracksUsed() - Method in class org.orekit.files.ccsds.ndm.cdm.ODParameters: Get the number of sensor tracks used for the OD of the object.
getTracksUsed() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination: Get number of sensors tracks accepted for the OD within the actual OD span.
getTrajBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get basis of this trajectory state time history data.
getTrajBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata: Get identification number of the orbit determination or simulation upon which this trajectory is based.
getTrajectoryBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData: Get trajectory state histories logical blocks.
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.
getTransferType() - Method in class org.orekit.files.iirv.IIRVVector: Gets the transfer type term.
getTransform(FrameFacade, FrameFacade, Frame, AbsoluteDate, PVCoordinatesProvider) - Static method in class org.orekit.files.ccsds.definitions.FrameFacade: Get the transform between CCSDS frames.
getTransform(AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.EclipticProvider
getTransform(AbsoluteDate) - Method in class org.orekit.frames.FixedTransformProvider: Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider: Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation: Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.InterpolatingTransformProvider: Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter: Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.L1TransformProvider: Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.ShiftingTransformProvider: Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider: Get the Transform 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(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EclipticProvider
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.FixedTransformProvider: Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider: Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.HelmertTransformation: Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.InterpolatingTransformProvider: Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter: Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.L1TransformProvider: Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ShiftingTransformProvider: Get the FieldTransform 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.
getTransitionDates() - Method in class org.orekit.utils.ParameterDriver: Get the dates of the transitions TimeSpanMap.
getTransitions() - Method in class org.orekit.utils.FieldTimeSpanMap: Get an unmodifiable view of the sorted transitions.
getTransitPV() - Method in class org.orekit.estimation.measurements.CommonParametersWithDerivatives: Get transit position/velocity.
getTransitPV() - Method in class org.orekit.estimation.measurements.CommonParametersWithoutDerivatives: Get transit position/velocity.
getTransitState() - Method in class org.orekit.estimation.measurements.CommonParametersWithDerivatives: Get transit state.
getTransitState() - Method in class org.orekit.estimation.measurements.CommonParametersWithoutDerivatives: Get transit state.
getTranslation() - Method in interface org.orekit.frames.FieldStaticTransform: Get the underlying elementary translation.
getTranslation() - Method in class org.orekit.frames.FieldTransform: Get the underlying elementary translation.
getTranslation() - Method in interface org.orekit.frames.StaticTransform: Get the underlying elementary translation.
getTranslation() - Method in class org.orekit.frames.Transform: Get the underlying elementary translation.
getTransmissionOfSpectralFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration: Get the percentage of transmission of spectral filter.
getTransmissionTime() - Method in class org.orekit.files.rinex.navigation.EarthOrientationParameterMessage: Get the message transmission time.
getTransmissionTime() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage: Get the message transmission time.
getTransmissionTime() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage: Getter for transmission time.
getTransmissionTime() - Method in class org.orekit.propagation.analytical.gnss.data.FieldAbstractNavigationMessage: Getter for transmission time.
getTransmitAmplitude() - Method in class org.orekit.files.ilrs.CRD.FrRangeMeasurement: Get the transmit amplitude.
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.
getTransmitTime() - Method in class org.orekit.files.rinex.navigation.IonosphereBaseMessage: Get the transmit time.
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.
getTransponderRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration: Get transponder configuration record related to the systemRecord.
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.FieldImpulseManeuver: Get the triggering event.
getTrigger() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Get the triggering event.
getTriggeredIncreasing() - Method in enum org.orekit.propagation.events.FilterType: Get the increasing status of triggered events.
getTropoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier: Get the tropospheric delay model.
getTropoModel() - Method in class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier: Get the tropospheric delay model.
getTroposphericModel(AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel: Get the EstimatedModel model valid at a date.
getTroposphericRefractionCorrection() - Method in class org.orekit.files.ilrs.CRD.RangeSupplement: Get the tropospheric refraction correction.
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.
getTwoDigitsRinexPRN() - Method in class org.orekit.gnss.SatInSystem: Get a 2-digits Pseudo Random Number for RINEX files.
getTwoLettersCode() - Method in enum org.orekit.gnss.TimeSystem: Get the two letters code.
getTypAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalProperties: Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.
getType() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade: Get the method type.
getType() - Method in class org.orekit.files.ccsds.definitions.PocMethodFacade: Get the method type.
getType() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovariance: Get the type of the elements.
getType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovariance: 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.SP3Header: Returns the 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.
getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005: Get type of the method.
getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999: Get type of the method.
getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max: Get type of the method.
getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997: Get type of the method.
getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015: Get type of the method.
getType() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005: Get type of the method.
getType() - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod: Get type of the method.
getTypeCode() - Method in class org.orekit.gnss.metric.messages.ParsedMessage: Get the code for the message type.
getTypeIndicator() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the calibration type indicator.
getTypeObs() - Method in class org.orekit.files.rinex.observation.PhaseShiftCorrection: Get the Carrier Phase Observation Code.
getTypeObs() - Method in class org.orekit.files.rinex.observation.RinexObservationHeader: Get an unmodifiable view of the map of observation types.
getTypeOfData() - Method in class org.orekit.files.ilrs.CRD.Calibration: Get the type of data.
getTypesObsScaled() - Method in class org.orekit.files.rinex.observation.ScaleFactorCorrection: Get the list of Observation Types scaled.
getU() - Method in class org.orekit.bodies.Ellipse: Get the unit vector along the major axis.
getU() - Method in class org.orekit.bodies.FieldEllipse: 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.GroundPointingAttitudeModifier: Getter for underlying ground pointing law.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.SpinStabilized: Get the underlying attitude provider.
getUnderlyingModel() - Method in interface org.orekit.forces.ForceModelModifier: Get the underlying force model.
getUnderlyingModel() - Method in class org.orekit.forces.gravity.OceanTides
getUnderlyingModel() - Method in class org.orekit.forces.gravity.SolidTides
getUnderlyingStateIndex(int, int) - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement: Get the spacecraft state index in the underlying measurement.
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.ndm.adm.acm.AttitudeCovarianceType: Get the elements units.
getUnits() - Method in enum org.orekit.files.ccsds.ndm.adm.acm.AttitudeElementsType: Get the elements units.
getUnits() - Method in enum org.orekit.files.ccsds.ndm.adm.acm.RateElementsType: Get the elements units.
getUnits() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType: 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.
getUnnormalizedC20(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider: Get the un-normalized coefficient of degree 2 and order 0 at a specific instance in time.
getUnnormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics: Get a spherical harmonic cosine coefficient.
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(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the gravity field coefficients provider from the first supported file.
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.
getUnnormalizedProvider(NormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Create an UnnormalizedSphericalHarmonicsProvider from a NormalizedSphericalHarmonicsProvider.
getUnnormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics: Get a spherical harmonic sine coefficient.
getUnoccultedFluxVector(FieldVector3D<T>) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel: Get the light flux vector, not considering any shadowing effect.
getUnoccultedFluxVector(FieldVector3D<T>) - Method in class org.orekit.forces.radiation.AbstractSolarLightFluxModel: Get the light flux vector, not considering any shadowing effect.
getUnoccultedFluxVector(Vector3D) - Method in class org.orekit.forces.radiation.AbstractLightFluxModel: Get the light flux vector, not considering any shadowing effect.
getUnoccultedFluxVector(Vector3D) - Method in class org.orekit.forces.radiation.AbstractSolarLightFluxModel: Get the light flux vector, not considering any shadowing effect.
getUpdateInterval() - Method in class org.orekit.gnss.metric.messages.common.SsrUpdateInterval: Get the update interval.
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.
getUppercaseOmega0() - Method in class org.orekit.gnss.rflink.gps.SubFrame3: Get Ω₀.
getUppercaseOmega0() - Method in class org.orekit.gnss.rflink.gps.SubFrameAlmanac: Get Ω₀.
getUpperLimit() - Method in class org.orekit.ssa.metrics.FieldProbabilityOfCollision: Get upper limit of the probability of collision value.
getUpperLimit() - Method in class org.orekit.ssa.metrics.ProbabilityOfCollision: Get upper limit of the probability of collision value.
getURA() - Method in class org.orekit.propagation.analytical.gnss.data.FieldGPSAlmanac: Gets the average URA number.
getURA() - Method in class org.orekit.propagation.analytical.gnss.data.FieldIRNSSNavigationMessage: Getter for the user range accuray (meters).
getURA() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage: Getter for the user range accuray (meters).
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).
getUraiEd() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Getter for Elevation-Dependent User Range Accuracy.
getUraiEd() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Getter for Elevation-Dependent User Range Accuracy.
getUraIndex() - Method in class org.orekit.gnss.rflink.gps.SubFrame1: Get URA index.
getUraiNed0() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Getter for term 0 of Non-Elevation-Dependent User Range Accuracy.
getUraiNed0() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Getter for term 0 of Non-Elevation-Dependent User Range Accuracy.
getUraiNed1() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Getter for term 1 of Non-Elevation-Dependent User Range Accuracy.
getUraiNed1() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Getter for term 1 of Non-Elevation-Dependent User Range Accuracy.
getUraiNed2() - Method in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage: Getter for term 2 of Non-Elevation-Dependent User Range Accuracy.
getUraiNed2() - Method in class org.orekit.propagation.analytical.gnss.data.FieldCivilianNavigationMessage: Getter for term 2 of Non-Elevation-Dependent User Range Accuracy.
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.estimation.measurements.gnss.CombinedObservationData: Get the list of observation data used to perform the combination of measurements.
getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmData: Get user defined parameters logical block.
getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmData: Get the user defined logical block.
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.
getUserDefinedParameters() - Method in class org.orekit.files.ccsds.ndm.cdm.Cdm: Get user defined parameters.
getUT1(EOPHistory) - Method in class org.orekit.time.AbstractTimeScales: Get the Universal Time 1 scale.
getUT1(EOPHistory) - Method in class org.orekit.time.LazyLoadedTimeScales: Get the Universal Time 1 scale.
getUT1(EOPHistory) - Static method in class org.orekit.time.TimeScalesFactory: 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(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.
getUt1MinusUtc() - Method in class org.orekit.files.sinex.SinexEopEntry: Get the UT1-UTC offset.
getUT1MinusUTC() - Method in class org.orekit.frames.EOPEntry: Get the UT1-UTC value.
getUT1MinusUTC(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the UT1-UTC value.
getUT1MinusUTC(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory: Get the UT1-UTC value.
getUt1mutcT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata: Get the difference (UT1 – UTC) in seconds at epoch OcmMetadata.getEpochT0().
getUtc() - Method in class org.orekit.frames.AbstractEopLoader: Get the UTC time scale.
getUtc() - Method in class org.orekit.models.earth.ionosphere.nequick.NeQuickModel: Get 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.models.earth.atmosphere.data.AbstractSolarActivityData: Get the UTC timescale.
getUTC() - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader: Get the UTC timescale.
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.
getUtcId() - Method in class org.orekit.files.rinex.navigation.SystemTimeOffsetMessage: Get the UTC Id.
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.
getV() - Method in class org.orekit.bodies.FieldEllipse: 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.
getValidityEnd() - Method in class org.orekit.estimation.measurements.QuadraticClockModel: Get validity end.
getValidityEnd() - Method in class org.orekit.time.AggregatedClockModel: Get validity end.
getValidityEnd() - Method in interface org.orekit.time.ClockModel: Get validity end.
getValidityEnd() - Method in class org.orekit.time.PerfectClockModel: Get validity end.
getValidityEnd() - Method in class org.orekit.time.SampledClockModel: Get validity end.
getValidityStart() - Method in class org.orekit.estimation.measurements.QuadraticClockModel: Get validity start.
getValidityStart() - Method in class org.orekit.time.AggregatedClockModel: Get validity start.
getValidityStart() - Method in interface org.orekit.time.ClockModel: Get validity start.
getValidityStart() - Method in class org.orekit.time.PerfectClockModel: Get validity start.
getValidityStart() - Method in class org.orekit.time.SampledClockModel: Get validity start.
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.measurements.gnss.CombinedObservationData: Get the combined observed value.
getValue() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
getValue() - Method in enum org.orekit.files.ccsds.ndm.cdm.Maneuvrable: Get the String representation of the enum.
getValue() - Method in class org.orekit.files.rinex.observation.ObservationData: Get the observed value.
getValue() - Method in class org.orekit.ssa.metrics.FieldProbabilityOfCollision: Get value of the probability of collision.
getValue() - Method in class org.orekit.ssa.metrics.ProbabilityOfCollision: Get value of the probability of collision.
getValue() - Method in class org.orekit.time.TimeStampedDouble: Get value.
getValue() - Method in class org.orekit.time.TimeStampedField: Get value.
getValue() - Method in class org.orekit.utils.DataDictionary.Entry: Get the value.
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.FieldDataDictionary.Entry: Get the value.
getValue() - Method in class org.orekit.utils.ParameterDriver: Get current parameter 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) - 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, 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(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, 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, Map<String, Integer>) - Method in class org.orekit.utils.ParameterDriver: Get the value as a gradient at special date.
getValue(int, Map<String, Integer>, AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver: Get the value as a gradient at special date.
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(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver: Get current parameter value at specific date, depending on isContinuousEstimation value, the value returned will be obtained by step estimation or continuous estimation.
getValueAndDerivative(int, int, int, double) - 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.
getValueContinuousEstimation(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver: Get current parameter value at specific date with continuous estimation.
getValues() - Method in class org.orekit.utils.ParameterDriver: Get all values of the valueSpanMap in the chronological order.
getValueSpanMap() - Method in class org.orekit.utils.ParameterDriver: Get value time span map for parameterDriver.
getValuesSamples() - Method in class org.orekit.utils.InterpolationTableLoader: Returns a copy of the values samples for the interpolation function.
getValueStepEstimation(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver: Get current parameter value at specific date with step estimation.
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.
getVectorEpoch() - Method in class org.orekit.files.iirv.IIRVVector: Gets the vector epoch term.
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.
getVectors() - Method in class org.orekit.files.iirv.IIRVMessage: Gets the list of sequential IIRVVector instances contained within the overall IIRV message.
getVectorStrings(IIRVMessage.IncludeMessageMetadata) - Method in class org.orekit.files.iirv.IIRVMessage: Converts the IIRVVectors contained in the message file into a list of their String representations.
getVectorType() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current VectorTypeTerm value.
getVectorType() - Method in class org.orekit.files.iirv.IIRVVector: Gets the vector type term.
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.
getVehicleIdCode() - Method in class org.orekit.files.iirv.IIRVBuilder: Gets the current VehicleIdCodeTerm value.
getVehicleIdCode() - Method in class org.orekit.files.iirv.IIRVVector: Gets the vehicle ID code term.
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 interface org.orekit.frames.FieldKinematicTransform: Get the first time derivative of the translation.
getVelocity() - Method in class org.orekit.frames.FieldTransform: Get the first time derivative of the translation.
getVelocity() - Method in interface org.orekit.frames.KinematicTransform: 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() - Method in class org.orekit.utils.FieldPVCoordinates: Gets the velocity.
getVelocity() - Method in class org.orekit.utils.PVCoordinates: Gets the velocity.
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.
getVelocityAccuracy() - Method in class org.orekit.files.sp3.SP3Coordinate: Get the velocity accuracy.
getVelocityVector() - Method in class org.orekit.files.ccsds.ndm.cdm.StateVector: Get object Velocity Vector.
getVelocityVector() - Method in class org.orekit.files.iirv.IIRVVector: Gets a velocity vector [vx vy vz], represented as a Vector3D instance.
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.ccsds.ndm.cdm.CdmMessageWriter: Get current format version.
getVersion() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter: Get current format version.
getVersion() - Method in interface org.orekit.files.ccsds.utils.generation.MessageWriter: Get current format version.
getVersion() - Method in class org.orekit.files.ilrs.ILRSHeader: Get the format version.
getVersion() - Method in class org.orekit.files.sp3.SP3Header: Get the file 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.CommonPhysicalProperties: Get the typical (50th percentile) visual magnitude.
getVmApparent() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties: Get the typical (50th percentile) apparent visual magnitude.
getVmApparentMax() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties: Get the maximum apparent visual magnitude.
getVmApparentMin() - Method in class org.orekit.files.ccsds.ndm.CommonPhysicalProperties: 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.