Index (ORbit Extrapolation KIT 9.1 API)

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

A

a - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: final semi major axis.
a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: a.
A - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: A = sqrt(μ * a).
a0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: original recovered semi major axis.
AbsoluteDate - Class in org.orekit.time: This class represents a specific instant in time.
AbsoluteDate() - Constructor for class org.orekit.time.AbsoluteDate: Create an instance with a default value (AbsoluteDate.J2000_EPOCH).
AbsoluteDate(String, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location (parsed from a string) in a time scale.
AbsoluteDate(DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(DateComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(int, int, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(int, Month, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(Date, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from a location in a time scale.
AbsoluteDate(AbsoluteDate, double) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from an elapsed duration since to another instant.
AbsoluteDate(AbsoluteDate, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate: Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.
ABSORPTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive: Parameter name for absorption coefficient.
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.
AbstractDetector<T extends EventDetector> - Class in org.orekit.propagation.events: Common parts shared by several orbital events finders.
AbstractDetector(double, double, int, EventHandler<? super T>) - Constructor for class org.orekit.propagation.events.AbstractDetector: Build a new instance.
AbstractForceModel - Class in org.orekit.forces: Base class for force models.
AbstractForceModel() - Constructor for class org.orekit.forces.AbstractForceModel
AbstractGaussianContribution - Class in org.orekit.propagation.semianalytical.dsst.forces: Common handling of DSSTForceModel methods for Gaussian contributions to DSST propagation.
AbstractGaussianContribution(String, double, ForceModel) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Build a new instance.
AbstractIntegratedPropagator - Class in org.orekit.propagation.integration: Common handling of Propagator methods for both numerical and semi-analytical propagators.
AbstractIntegratedPropagator(ODEIntegrator, boolean) - 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).
AbstractMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements: Abstract class handling measurements boilerplate.
AbstractMeasurement(AbsoluteDate, double, double, double, List<Integer>, ParameterDriver...) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement: Simple constructor for mono-dimensional measurements.
AbstractMeasurement(AbsoluteDate, double[], double[], double[], List<Integer>, ParameterDriver...) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement: Simple constructor, for multi-dimensional measurements.
AbstractParametricAcceleration - Class in org.orekit.forces: This class implements a parametric acceleration.
AbstractParametricAcceleration(Vector3D, boolean, AttitudeProvider) - Constructor for class org.orekit.forces.AbstractParametricAcceleration: Simple constructor.
AbstractPropagator - Class in org.orekit.propagation: Common handling of Propagator methods for analytical propagators.
AbstractPropagator() - Constructor for class org.orekit.propagation.AbstractPropagator: Build a new instance.
AbstractPropagatorBuilder - Class in org.orekit.propagation.conversion: Base class for propagator builders.
AbstractPropagatorBuilder(Orbit, PositionAngle, double, boolean) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Build a new instance.
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.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.AbstractParametricAcceleration: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.AbstractParametricAcceleration: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.DragForce: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.DragForce: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in interface org.orekit.forces.ForceModel: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.ForceModel: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.OceanTides: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.OceanTides: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.Relativity: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.Relativity: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SolidTides: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SolidTides: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Compute acceleration.
acceptStep(OrekitStepInterpolator, AbsoluteDate, double) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Accept a step, triggering events and step handlers.
acceptStep(FieldAbstractAnalyticalPropagator<T>.FieldBasicStepInterpolator, FieldAbsoluteDate<T>, double) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Accept a step, triggering events and step handlers.
AdamsBashforthIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for AdamsBashforthIntegrator.
AdamsBashforthIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder: Build a new instance.
AdamsMoultonIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for AdamsMoultonIntegrator.
AdamsMoultonIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder: Build a new instance.
AdapterPropagator - Class in org.orekit.propagation.analytical: Orbit propagator that adapts an underlying propagator, adding differential effects.
AdapterPropagator(Propagator) - Constructor for class org.orekit.propagation.analytical.AdapterPropagator: Build a propagator from an underlying reference propagator.
AdapterPropagator.DifferentialEffect - Interface in org.orekit.propagation.analytical: Interface for orbit differential effects.
add(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepHandlerMultiplexer: Add a step handler.
add(OrekitStepHandler) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer: Add a step handler.
add(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix: Add the argument matrix with the current matrix.
add(ParameterDriver) - Method in class org.orekit.utils.ParameterDriversList: Add a driver.
addAdditionalEquations(AdditionalEquations) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Add a set of user-specified equations to be integrated along with the orbit propagation.
addAdditionalEquations(FieldAdditionalEquations<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Add a set of user-specified equations to be integrated along with the orbit propagation.
addAdditionalState(String, T...) - Method in class org.orekit.propagation.FieldSpacecraftState: Add an additional state.
addAdditionalState(String, double...) - Method in class org.orekit.propagation.SpacecraftState: Add an additional state.
addAdditionalStateProvider(AdditionalStateProvider) - Method in class org.orekit.propagation.AbstractPropagator: Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator: Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in interface org.orekit.propagation.FieldPropagator: Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(AdditionalStateProvider) - Method in interface org.orekit.propagation.Propagator: Add a set of user-specified state parameters to be computed along with the orbit propagation.
addCelestialBodyLoader(String, CelestialBodyLoader) - Static method in class org.orekit.bodies.CelestialBodyFactory: 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.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in interface org.orekit.forces.ForceModel: Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in interface org.orekit.forces.ForceModel: Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.NewtonianAttraction: Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction: Compute the contribution of the force model to the perturbing acceleration.
addContribution(BodiesElements, double[][], double[][]) - Method in class org.orekit.forces.gravity.potential.OceanTidesWave: Add the contribution of the wave to Stokes coefficients.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Compute the contribution of the force model to the perturbing acceleration.
addDefaultCelestialBodyLoader(String) - Static method in class org.orekit.bodies.CelestialBodyFactory: Add the default loaders for all predefined celestial bodies.
addDefaultCelestialBodyLoader(String, String) - Static method in class org.orekit.bodies.CelestialBodyFactory: Add the default loaders for celestial bodies.
addDefaultEOP1980HistoryLoaders(String, String, String, String, String) - Static method in class org.orekit.frames.FramesFactory: Add the default loaders EOP history (IAU 1980 precession/nutation).
addDefaultEOP2000HistoryLoaders(String, String, String, String, String) - Static method in class org.orekit.frames.FramesFactory: Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).
addDefaultOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: 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.
addDefaultProviders() - Method in class org.orekit.data.DataProvidersManager: Add the default providers configuration.
addDefaultUTCTAIOffsetsLoaders() - Static method in class org.orekit.time.TimeScalesFactory: Add the default loaders for UTC-TAI offsets history files (both IERS and USNO).
addEffect(AdapterPropagator.DifferentialEffect) - Method in class org.orekit.propagation.analytical.AdapterPropagator: Add a differential effect.
addEOPHistoryLoader(IERSConventions, EOPHistoryLoader) - Static method in class org.orekit.frames.FramesFactory: Add a loader for Earth Orientation Parameters history.
addEventDate(AbsoluteDate) - Method in class org.orekit.propagation.events.DateDetector: Add an event date.
addEventDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldDateDetector: Add an event date.
addEventDetector(T) - Method in class org.orekit.propagation.AbstractPropagator: Add an event detector.
addEventDetector(T) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Add an event detector.
addEventDetector(D) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Add an event detector.
addEventDetector(D) - Method in class org.orekit.propagation.FieldAbstractPropagator: Add an event detector.
addEventDetector(D) - Method in interface org.orekit.propagation.FieldPropagator: Add an event detector.
addEventDetector(EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Add an event detector.
addEventDetector(D) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Add an event detector.
addEventDetector(T) - Method in interface org.orekit.propagation.Propagator: Add an event detector.
addForceModel(ForceModel) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Add a force model to the global perturbation model.
addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Add a force model to the global perturbation model.
addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Add a force model.
addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Add a force model to the global perturbation model.
addGridPoint(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient: Add a point to the interpolation grid.
AdditionalEquations - Interface in org.orekit.propagation.integration: This interface allows users to add their own differential equations to a numerical propagator.
AdditionalStateProvider - Interface in org.orekit.propagation: This interface represents providers for additional state data beyond SpacecraftState.
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CartesianOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CircularOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.EquinoctialOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, T[]) - Method in class org.orekit.orbits.FieldCartesianOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, T[]) - Method in class org.orekit.orbits.FieldCircularOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, T[]) - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, T[]) - Method in class org.orekit.orbits.FieldKeplerianOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, T[]) - Method in class org.orekit.orbits.FieldOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.KeplerianOrbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.Orbit: Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(double) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations: Add the contribution of the Kepler evolution.
addKeplerContribution(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations: Add the contribution of the Kepler evolution.
addMassDerivative(T) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations: Add the contribution of the flow rate (dm/dt).
addMassDerivative(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations: Add the contribution of the flow rate (dm/dt).
addMeasurement(ObservedMeasurement<?>) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Add a measurement.
addModifier(EstimationModifier<T>) - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Add a modifier.
addModifier(EstimationModifier<T>) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Add a modifier.
addNewSegment(List<SpacecraftState>) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris: Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
addNewSegment(List<SpacecraftState>, int) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris: Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
addNewSegment(List<SpacecraftState>, CelestialBody, int) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris: Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
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(TDMFile.Observation) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock: Adds an observation data line.
addObservation(String, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock: Adds an observation data line.
addObservationComment(String) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock: Add an observation data line comment.
addObservationsBlock() - Method in class org.orekit.files.ccsds.TDMFile: Add a block to the list of observations blocks.
addObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver: Add an observer for this driver.
addOceanTidesReader(OceanTidesReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Add a reader for ocean tides.
addOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates: Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates: Add an offset from the instance.
addOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates: Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates: Add an offset from the instance.
addParticipant(int, String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Adds a participant to the list.
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.
addProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager: Add a data provider to the supported list.
addReceiveDelay(int, double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Adds a receive delay to the list.
addSatellite(String) - Method in class org.orekit.files.general.OrekitEphemerisFile: Adds a new satellite to this object.
addSatellite(String) - Method in class org.orekit.files.sp3.SP3File: Add a new satellite with a given identifier to the list of stored satellites.
addSupportedParameter(ParameterDriver) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Add a supported parameter.
addSwitchingCondition(AttitudeProvider, AttitudeProvider, T, boolean, boolean, double, AngularDerivativesFilter, AttitudesSequence.SwitchHandler) - Method in class org.orekit.attitudes.AttitudesSequence: Add a switching condition between two attitude providers.
addTransmitDelay(int, double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Adds a transmit delay to the list.
addUTCTAIOffsetsLoader(UTCTAIOffsetsLoader) - Static method in class org.orekit.time.TimeScalesFactory: Add a loader for UTC-TAI offsets history files.
addValidAfter(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap: Add an entry valid after a limit date.
addValidAfter(T, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap: Add an entry valid after a limit date.
addValidBefore(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap: Add an entry valid before a limit date.
addValidBefore(T, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap: Add an entry valid before a limit date.
addWaveCoefficients(int, int, int, double, double, double, double, int, String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Add parsed coefficients.
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.
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.
AlignmentDetector - Class in org.orekit.propagation.events: Finder for satellite/body alignment events in orbital plane.
AlignmentDetector(Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector: Build a new alignment detector.
AlignmentDetector(double, Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector: Build a new alignment detector.
alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.AlongTrackAiming: Find the along tile direction for tessellation at specified point.
alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.ConstantAzimuthAiming: Find the along tile direction for tessellation at specified point.
alongTileDirection(Vector3D, GeodeticPoint) - Method in interface org.orekit.models.earth.tessellation.TileAiming: Find the along tile direction for tessellation at specified point.
AlongTrackAiming - Class in org.orekit.models.earth.tessellation: Class used to orient tiles along an orbit track.
AlongTrackAiming(OneAxisEllipsoid, Orbit, boolean) - Constructor for class org.orekit.models.earth.tessellation.AlongTrackAiming: Simple constructor.
AltitudeDetector - Class in org.orekit.propagation.events: Finder for satellite altitude crossing events.
AltitudeDetector(double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector: Build a new altitude detector.
AltitudeDetector(double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector: Build a new altitude detector.
AltitudeDetector(double, double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector: Build a new altitude detector.
andCombine(EventDetector...) - Static method in class org.orekit.propagation.events.BooleanDetector: Create a new event detector that is the logical AND of the given event detectors.
andCombine(Collection<? extends EventDetector>) - Static method in class org.orekit.propagation.events.BooleanDetector: Create a new event detector that is the logical AND of the given event detectors.
AngularAzEl - Class in org.orekit.estimation.measurements: Class modeling an Azimuth-Elevation measurement from a ground station.
AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[]) - Constructor for class org.orekit.estimation.measurements.AngularAzEl: Simple constructor.
AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[], int) - Constructor for class org.orekit.estimation.measurements.AngularAzEl: Simple constructor.
AngularCoordinates - Class in org.orekit.utils: Simple container for rotation/rotation rate/rotation acceleration triplets.
AngularCoordinates() - Constructor for class org.orekit.utils.AngularCoordinates: Simple constructor.
AngularCoordinates(Rotation, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates: Builds a rotation/rotation rate pair.
AngularCoordinates(Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates: Builds a rotation/rotation rate/rotation acceleration triplet.
AngularCoordinates(PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.AngularCoordinates: Build the rotation that transforms a pair of pv coordinates into another one.
AngularCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.AngularCoordinates: Build one of the rotations that transform one pv coordinates into another one.
AngularCoordinates(FieldRotation<DerivativeStructure>) - Constructor for class org.orekit.utils.AngularCoordinates: Builds a AngularCoordinates from a FieldRotation<DerivativeStructure>.
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) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier: Constructor.
AngularRaDec - Class in org.orekit.estimation.measurements: Class modeling an Right Ascension - Declination measurement from a ground point (station, telescope).
AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[]) - Constructor for class org.orekit.estimation.measurements.AngularRaDec: Simple constructor.
AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], int) - Constructor for class org.orekit.estimation.measurements.AngularRaDec: Simple constructor.
AngularRadioRefractionModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical angular measurement with ionospheric radio refractive index.
AngularRadioRefractionModifier(AtmosphericRefractionModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier: Constructor.
AngularSeparationDetector - Class in org.orekit.propagation.events: Detects when spacecraft comes close to a moving beacon, as seen from a moving observer.
AngularSeparationDetector(PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationDetector: Build a new angular separation detector.
AngularTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers: Class modifying theoretical angular measurement with tropospheric delay.
AngularTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier: Constructor.
apply(Orbit) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Compute the effect of the maneuver on an orbit.
apply(SpacecraftState) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Compute the effect of the maneuver on a spacecraft state.
apply(SpacecraftState) - Method in interface org.orekit.propagation.analytical.AdapterPropagator.DifferentialEffect: Apply the effect to a spacecraft state.
apply(Orbit) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect: Compute the effect of the maneuver on an orbit.
apply(SpacecraftState) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect: Apply the effect to a spacecraft state.
applyTo(PVCoordinates) - Method in class org.orekit.utils.AngularCoordinates: Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.AngularCoordinates: Apply the rotation to a pv coordinates.
applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates: Apply the rotation to a pv coordinates.
applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates: Apply the rotation to a pv coordinates.
applyTo(PVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates: Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates: Apply the rotation to a pv coordinates.
applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates: Apply the rotation to a pv coordinates.
applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates: Apply the rotation to a pv coordinates.
approximateAsPolynomialOnly(int, AbsoluteDate, int, int, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic: Approximate an already fitted model to polynomial only terms.
ApsideDetector - Class in org.orekit.propagation.events: Finder for apside crossing events.
ApsideDetector(Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector: Build a new instance.
ApsideDetector(double, Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector: Build a new instance.
ARC_SECONDS_TO_RADIANS - Static variable in interface org.orekit.utils.Constants: Conversion factor from arc seconds to radians: 2*PI/(360*60*60).
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.forces.drag.atmosphere: Interface for atmospheric models.
AtmosphericRefractionModel - Interface in org.orekit.models: Defines an refraction model that can be used to correct for the apparent position of an object due to atmospheric effects.
ATOMIC_NITROGEN - Static variable in class org.orekit.forces.drag.atmosphere.DTM2000: Identifier for atomic nitrogen.
ATOMIC_OXYGEN - Static variable in class org.orekit.forces.drag.atmosphere.DTM2000: Identifier for atomic oxygen.
attachTo(Frame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame: Attach the instance (and all its children down to leafs) to the main tree.
attachTo(Frame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame: Attach the instance (and all its children down to leafs) to the main tree.
Attitude - Class in org.orekit.attitudes: This class handles attitude definition at a given date.
Attitude(Frame, TimeStampedAngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude: Creates a new instance.
Attitude(AbsoluteDate, Frame, AngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude: Creates a new instance.
Attitude(AbsoluteDate, Frame, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.Attitude: Creates a new instance.
AttitudeProvider - Interface in org.orekit.attitudes: This interface represents an attitude provider model set.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder: Sets the attitude provider.
AttitudeProviderModifier - Interface in org.orekit.attitudes: This interface represents an attitude provider that modifies/wraps another underlying provider.
AttitudesSequence - Class in org.orekit.attitudes: This classes manages a sequence of different attitude providers that are activated in turn according to switching events.
AttitudesSequence() - Constructor for class org.orekit.attitudes.AttitudesSequence: Constructor for an initially empty sequence.
AttitudesSequence.SwitchHandler - Interface in org.orekit.attitudes: Interface for attitude switch notifications.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.ThirdBodyAttraction: Suffix for parameter name for attraction coefficient enabling Jacobian processing.
AuxiliaryElements - Class in org.orekit.propagation.semianalytical.dsst.utilities: Container class for common parameters used by all DSST forces.
AuxiliaryElements(Orbit, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Simple constructor.

B

B - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: B = sqrt(1 - h² - k²).
B_STAR - Static variable in class org.orekit.propagation.conversion.TLEPropagatorBuilder: Parameter name for B* coefficient.
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.Ephemeris
basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Propagate an orbit without any fancy features.
basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Propagate an orbit without any fancy features.
BatchLSEstimator - Class in org.orekit.estimation.leastsquares: Least squares estimator for orbit determination.
BatchLSEstimator(LeastSquaresOptimizer, NumericalPropagatorBuilder...) - Constructor for class org.orekit.estimation.leastsquares.BatchLSEstimator: Simple constructor.
BatchLSObserver - Interface in org.orekit.estimation.leastsquares: Observer for batch least squares estimator iterations.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Method called just before integration.
beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Method called just before integration.
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.TLEPropagator: sqrt (1 - e2).
beta02 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: 1 - e2.
Bias<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers: Class modeling a measurement bias.
Bias(String[], double[], double[], double[], double[]) - Constructor for class org.orekit.estimation.measurements.modifiers.Bias: Simple constructor.
BodiesElements - Class in org.orekit.data: Elements of the bodies having an effect on nutation.
BodiesElements(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.BodiesElements: Simple constructor.
BodyCenterPointing - Class in org.orekit.attitudes: This class handles body center pointing attitude provider.
BodyCenterPointing(Frame, Ellipsoid) - Constructor for class org.orekit.attitudes.BodyCenterPointing: Creates new instance.
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.
BoundedPropagator - Interface in org.orekit.propagation: This interface is intended for ephemerides valid only during a time range.
BoxAndSolarArraySpacecraft - Class in org.orekit.forces: Class representing the features of a classical satellite with a convex body shape and rotating flat solar arrays.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft: Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft: Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft: Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft: Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft: Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft: Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft: Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft: Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft.Facet - Class in org.orekit.forces: Class representing a single facet of a convex spacecraft body.
build() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder: Finalizes the build.
Builder(GPSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder: Initializes the builder.
buildIdentityMatrix2() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities: Build the identity matrix of order 2.
buildIdentityMatrix4() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities: Build the identity matrix of order 4.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.EulerIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GillIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.LutherIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.MidpointIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in interface org.orekit.propagation.conversion.ODEIntegratorBuilder: Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder: Build a first order integrator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder: Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder: Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Build a propagator.
buildPropagator(double[]) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder: Build a propagator.
buildRow(int, int, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Build a coefficients row.
buildSimpleZone(double, double[]...) - Static method in class org.orekit.models.earth.tessellation.EllipsoidTessellator: Build a simple zone (connected zone without holes).
buildSimpleZone(double, GeodeticPoint...) - Static method in class org.orekit.models.earth.tessellation.EllipsoidTessellator: Build a simple zone (connected zone without holes).
buildTriangularArray(int, int, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Build a coefficients triangular array.
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).

C

C - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: C = 1 + p² + q².
c1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: C1 from SPTRCK #3.
c2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: C2 from SPTRCK #3.
c4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: C4 from SPTRCK #3.
CachedNormalizedSphericalHarmonicsProvider - Class in org.orekit.forces.gravity.potential: Caching wrapper for NormalizedSphericalHarmonicsProvider.
CachedNormalizedSphericalHarmonicsProvider(NormalizedSphericalHarmonicsProvider, double, int, int, double, double) - Constructor for class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Simple constructor.
calculateField(double, double, double) - Method in class org.orekit.models.earth.GeoMagneticField: Calculate the magnetic field at the specified geodetic point identified by latitude, longitude and altitude.
canAdd(int, int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Check if coefficients can be added.
CartesianDerivativesFilter - Enum in org.orekit.utils: Enumerate for selecting which derivatives to use in TimeStampedPVCoordinates and TimeStampedFieldPVCoordinates interpolation.
CartesianOrbit - Class in org.orekit.orbits: This class holds Cartesian orbital parameters.
CartesianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CartesianOrbit: Constructor from Cartesian parameters.
CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CartesianOrbit: Constructor from Cartesian parameters.
CartesianOrbit(Orbit) - Constructor for class org.orekit.orbits.CartesianOrbit: Constructor from any kind of orbital parameters.
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_OEM_VERS - Static variable in class org.orekit.files.ccsds.OEMWriter: Version number implemented.
CCSDS_OEM_VERS - Static variable in class org.orekit.files.ccsds.StreamingOemWriter: Version number implemented.
CCSDSFrame - Enum in org.orekit.files.ccsds: Frames used in CCSDS Orbit Data Messages.
CcsdsModifiedFrame - Class in org.orekit.files.ccsds: A reference frame created from the REF_FRAME and CENTER_NAME is a CCSDS OPM, OMM, or OEM file.
CcsdsTimeScale - Enum in org.orekit.files.ccsds: The set of time scales defined in Annex A of the ODM CCSDS standard 502.0-B-2.
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.
CelestialBodyLoader - Interface in org.orekit.bodies: Interface for loading celestial bodies.
CelestialBodyPointed - Class in org.orekit.attitudes: This class handles a celestial body pointed attitude provider.
CelestialBodyPointed(Frame, PVCoordinatesProvider, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.CelestialBodyPointed: Creates new instance.
CenterName - Enum in org.orekit.files.ccsds: 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.
checkEOPContinuity(double) - Method in class org.orekit.frames.EOPHistory: Check Earth orientation parameters continuity.
checkTimeSystems() - Method in class org.orekit.files.ccsds.TDMFile: Check that, according to the CCSDS standard, every ObservationsBlock has the same time system.
ChronologicalComparator - Class in org.orekit.time: Comparator for TimeStamped instance.
ChronologicalComparator() - Constructor for class org.orekit.time.ChronologicalComparator: Simple constructor.
CircularFieldOfViewDetector - Class in org.orekit.propagation.events: Finder for target entry/exit events with respect to a satellite sensor Field Of View.
CircularFieldOfViewDetector(double, PVCoordinatesProvider, Vector3D, double) - Constructor for class org.orekit.propagation.events.CircularFieldOfViewDetector: Build a new instance.
CircularOrbit - Class in org.orekit.orbits: This class handles circular orbital parameters.
CircularOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit: Creates a new instance.
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit: Creates a new instance.
CircularOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CircularOrbit: Constructor from Cartesian parameters.
CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit: Constructor from Cartesian parameters.
CircularOrbit(Orbit) - Constructor for class org.orekit.orbits.CircularOrbit: Constructor from any kind of orbital parameters.
circularToPosition(T, T, T, T, T, T, double) - Static method in class org.orekit.orbits.FieldCircularOrbit: Compute position from circular parameters.
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.
ClassicalRungeKuttaIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for ClassicalRungeKuttaIntegrator.
ClassicalRungeKuttaIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder: Build a new instance.
ClasspathCrawler - Class in org.orekit.data: Provider for data files stored as resources in the classpath.
ClasspathCrawler(String...) - Constructor for class org.orekit.data.ClasspathCrawler: Build a data classpath crawler.
ClasspathCrawler(ClassLoader, String...) - Constructor for class org.orekit.data.ClasspathCrawler: Build a data classpath crawler.
clear() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue: Clear all stored events.
clearCelestialBodyCache(String) - Static method in class org.orekit.bodies.CelestialBodyFactory: Clear the specified celestial body from the internal cache.
clearCelestialBodyCache() - Static method in class org.orekit.bodies.CelestialBodyFactory: Clear all loaded celestial bodies.
clearCelestialBodyLoaders(String) - Static method in class org.orekit.bodies.CelestialBodyFactory: Clear loaders for one celestial body.
clearCelestialBodyLoaders() - Static method in class org.orekit.bodies.CelestialBodyFactory: Clear loaders for all celestial bodies.
clearEOPHistoryLoaders() - Static method in class org.orekit.frames.FramesFactory: Clear loaders for Earth Orientation Parameters history.
clearEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator: Remove all events detectors.
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 class org.orekit.propagation.FieldAbstractPropagator: 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.
clearHistory() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient: Clear the recorded values from the interpolation grid.
clearLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager: Clear the set of data file names that have been loaded.
clearLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger: Clear the logged events.
clearLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger: Clear the logged events.
clearOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Clear ocean tides readers.
clearPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Clear gravity field readers.
clearProviders() - Method in class org.orekit.data.DataProvidersManager: Remove all data providers.
clearUTCTAIOffsetsLoaders() - Static method in class org.orekit.time.TimeScalesFactory: Clear loaders for UTC-TAI offsets history files.
co2AB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: C / (2 * A * B) .
coef - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: coef for SGP C3 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.
compare(TimeStamped, TimeStamped) - Method in class org.orekit.time.ChronologicalComparator: Compare two time-stamped instances.
compareTo(CoefficientsFactory.NSKey) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
compareTo(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate: Compare the instance with another date.
compareTo(DateComponents) - Method in class org.orekit.time.DateComponents
compareTo(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents
compareTo(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate: Compare the instance with another date.
compareTo(TimeComponents) - Method in class org.orekit.time.TimeComponents
compile(PoissonSeries...) - Static method in class org.orekit.data.PoissonSeries: Join several nutation series, for fast simultaneous evaluation.
complainIfNotSupported(String) - Method in class org.orekit.forces.AbstractForceModel: Complain if a parameter is not supported.
compute(AbsoluteDate, List<Propagator>) - Method in class org.orekit.gnss.DOPComputer: Compute the DOP at a given date for a set of GNSS spacecrafts.
computeDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations: Compute differential equations for main state.
computeDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.propagation.integration.AdditionalEquations: Compute the derivatives related to the additional state parameters.
computeDerivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations: Compute differential equations for main state.
computeDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations: Compute the derivatives related to the additional state parameters.
computeDerivatives(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Compute the derivatives related to the additional state parameters.
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).
computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear: Compute the values for the first four coefficients and their derivatives by means of series.
computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear: Compute the initial values (see Collins, 4-255, 4-256 and 4.259)
computeInitValues(double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear: Compute the roots for the Hansen coefficients and their derivatives.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit: Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit: Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit: Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit: Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit: Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.Orbit: Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit: Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit: Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit: Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit: Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit: Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.Orbit: Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit: Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit: Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit: Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit: Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit: Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.Orbit: Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeLimitVisibilityPoint(double, double, double) - Method in class org.orekit.frames.TopocentricFrame: Compute the limit visibility point for a satellite in a given direction.
computeMeanState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Conversion from osculating to mean orbit.
computeOsculatingState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Conversion from mean to osculating orbit.
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).
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).
configureOceanLoadDeformationCoefficients(OceanLoadDeformationCoefficients) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Configure ocean load deformation coefficients.
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.
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(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.
contains(String) - Static method in enum org.orekit.files.ccsds.CcsdsTimeScale: Check if timeScale is one of the values supported by this enum.
containsSatellite(String) - Method in class org.orekit.files.sp3.SP3File: Tests whether a satellite with the given id is contained in this orbit file.
ContinueOnEvent<T extends EventDetector> - Class in org.orekit.propagation.events.handlers: Event handler which will always return continue as a state.
ContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.ContinueOnEvent
convert(double[]) - Method in interface org.orekit.data.SimpleTimeStampedTableParser.RowConverter: Convert a row.
convert(Propagator, double, int, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Convert a propagator to another.
convert(Propagator, double, int, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Convert a propagator to another.
convert(List<SpacecraftState>, boolean, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Find the propagator that minimize the mean square error for a sample of states.
convert() - Method in class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter: Convert an osculating orbit into a mean orbit, in DSST sense.
convert(Propagator, double, int, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter: Convert a propagator into another one.
convert(Propagator, double, int, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter: Convert a propagator into another one.
convert(List<SpacecraftState>, boolean, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter: Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter: Find the propagator that minimize the mean square error for a sample of states.
convertType(Orbit) - Method in enum org.orekit.orbits.OrbitType: Convert an orbit to the instance type.
convertType(FieldOrbit<T>) - Method in enum org.orekit.orbits.OrbitType: Convert an orbit to the instance type.
cosi0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: cosinus original inclination.
create(double, double, int, EventHandler<? super ImpulseManeuver<T>>) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Build a new instance.
create(OneAxisEllipsoid, GeodeticPoint) - Static method in class org.orekit.gnss.DOPComputer: Creates a DOP computer for one location.
create(double, double, int, EventHandler<? super T>) - Method in class org.orekit.propagation.events.AbstractDetector: Build a new instance.
create(double, double, int, EventHandler<? super AlignmentDetector>) - Method in class org.orekit.propagation.events.AlignmentDetector: Build a new instance.
create(double, double, int, EventHandler<? super AltitudeDetector>) - Method in class org.orekit.propagation.events.AltitudeDetector: Build a new instance.
create(double, double, int, EventHandler<? super AngularSeparationDetector>) - Method in class org.orekit.propagation.events.AngularSeparationDetector: Build a new instance.
create(double, double, int, EventHandler<? super ApsideDetector>) - Method in class org.orekit.propagation.events.ApsideDetector: Build a new instance.
create(double, double, int, EventHandler<? super BooleanDetector>) - Method in class org.orekit.propagation.events.BooleanDetector
create(double, double, int, EventHandler<? super CircularFieldOfViewDetector>) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector: Build a new instance.
create(double, double, int, EventHandler<? super DateDetector>) - Method in class org.orekit.propagation.events.DateDetector: Build a new instance.
create(double, double, int, EventHandler<? super EclipseDetector>) - Method in class org.orekit.propagation.events.EclipseDetector: Build a new instance.
create(double, double, int, EventHandler<? super ElevationDetector>) - Method in class org.orekit.propagation.events.ElevationDetector: Build a new instance.
create(double, double, int, EventHandler<? super ElevationExtremumDetector>) - Method in class org.orekit.propagation.events.ElevationExtremumDetector: Build a new instance.
create(double, double, int, EventHandler<? super EventEnablingPredicateFilter<T>>) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter: Build a new instance.
create(double, double, int, EventHandler<? super EventShifter<T>>) - Method in class org.orekit.propagation.events.EventShifter: Build a new instance.
create(double, double, int, EventHandler<? super EventSlopeFilter<T>>) - Method in class org.orekit.propagation.events.EventSlopeFilter: Build a new instance.
create(T, T, int, FieldEventHandler<? super D, T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector: Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldAltitudeDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector: Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldApsideDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldApsideDetector: Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldDateDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldDateDetector: Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldEclipseDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector: Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldElevationDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldElevationDetector: Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldNodeDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldNodeDetector: Build a new instance.
create(double, double, int, EventHandler<? super FieldOfViewDetector>) - Method in class org.orekit.propagation.events.FieldOfViewDetector: Build a new instance.
create(double, double, int, EventHandler<? super FootprintOverlapDetector>) - Method in class org.orekit.propagation.events.FootprintOverlapDetector: Build a new instance.
create(double, double, int, EventHandler<? super GeographicZoneDetector>) - Method in class org.orekit.propagation.events.GeographicZoneDetector: Build a new instance.
create(double, double, int, EventHandler<? super GroundFieldOfViewDetector>) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector: Build a new instance.
create(double, double, int, EventHandler<? super LatitudeCrossingDetector>) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector: Build a new instance.
create(double, double, int, EventHandler<? super LatitudeExtremumDetector>) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector: Build a new instance.
create(double, double, int, EventHandler<? super LongitudeCrossingDetector>) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector: Build a new instance.
create(double, double, int, EventHandler<? super LongitudeExtremumDetector>) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector: Build a new instance.
create(double, double, int, EventHandler<? super NegateDetector>) - Method in class org.orekit.propagation.events.NegateDetector
create(double, double, int, EventHandler<? super NodeDetector>) - Method in class org.orekit.propagation.events.NodeDetector: Build a new instance.
create(double, double, int, EventHandler<? super PositionAngleDetector>) - Method in class org.orekit.propagation.events.PositionAngleDetector: Build a new instance.
createBesselianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate: Build an instance corresponding to a Besselian Epoch (BE).
createBesselianEpoch(T) - Static method in class org.orekit.time.FieldAbsoluteDate: Build an instance corresponding to a Besselian Epoch (BE).
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, double) - Static method in class org.orekit.time.AbsoluteDate: Build an instance corresponding to a GPS date.
createGPSDate(int, T) - Static method in class org.orekit.time.FieldAbsoluteDate: Build an instance corresponding to a GPS date.
createInitialOrbit() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Build an initial orbit using the current selected parameters.
createJDDate(int, double, TimeScale) - Static method in class org.orekit.time.AbsoluteDate: Build an instance corresponding to a Julian Day date.
createJDDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate: Build an instance corresponding to a Julian Day date.
createJulianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate: Build an instance corresponding to a Julian Epoch (JE).
createJulianEpoch(T) - Static method in class org.orekit.time.FieldAbsoluteDate: Build an instance corresponding to a Julian Epoch (JE).
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Create a mapper between raw double components and spacecraft state.
createMapper(FieldAbsoluteDate<T>, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Create a mapper between raw double components and spacecraft state.
createMapper(FieldAbsoluteDate<T>, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Create a mapper between raw double components and spacecraft state.
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator: Create a mapper between raw double components and spacecraft state.
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Create a mapper between raw double components and spacecraft state.
createMJDDate(int, double, TimeScale) - Static method in class org.orekit.time.AbsoluteDate: Build an instance corresponding to a Modified Julian Day date.
createMJDDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate: Build an instance corresponding to a Modified Julian Day date.
createTransformedITRF(Frame, String) - Method in enum org.orekit.frames.HelmertTransformation.Predefined: Create an ITRF frame by transforming another ITRF frame.
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.

D

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: Singleton class managing all supported data providers.
DateComponents - Class in org.orekit.time: Class representing a date broken up as year, month and day components.
DateComponents(int, int, int) - Constructor for class org.orekit.time.DateComponents: Build a date from its components.
DateComponents(int, Month, int) - Constructor for class org.orekit.time.DateComponents: Build a date from its components.
DateComponents(int, int) - Constructor for class org.orekit.time.DateComponents: Build a date from a year and day number.
DateComponents(int) - Constructor for class org.orekit.time.DateComponents: Build a date from its offset with respect to a DateComponents.J2000_EPOCH.
DateComponents(DateComponents, int) - Constructor for class org.orekit.time.DateComponents: Build a date from its offset with respect to a reference epoch.
DateDetector - Class in org.orekit.propagation.events: Finder for date events.
DateDetector(double, double, TimeStamped...) - Constructor for class org.orekit.propagation.events.DateDetector: Build a new instance.
DateDetector(AbsoluteDate) - Constructor for class org.orekit.propagation.events.DateDetector: Build a new instance.
DateTimeComponents - Class in org.orekit.time: Holder for date and time components.
DateTimeComponents(DateComponents, TimeComponents) - Constructor for class org.orekit.time.DateTimeComponents: Build a new instance from its components.
DateTimeComponents(int, int, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from raw level components.
DateTimeComponents(int, Month, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from raw level components.
DateTimeComponents(int, int, int) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from raw level components.
DateTimeComponents(int, Month, int) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from raw level components.
DateTimeComponents(DateTimeComponents, double) - Constructor for class org.orekit.time.DateTimeComponents: Build an instance from a seconds offset with respect to another one.
deepPeriodicEffects(double) - Method in class org.orekit.propagation.analytical.tle.DeepSDP4: 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.
deepSecularEffects(double) - Method in class org.orekit.propagation.analytical.tle.DeepSDP4: Computes secular terms from current coordinates and epoch.
DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.TLE: Identifier for default type of ephemeris (SGP4/SDP4).
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_CORRECTION_FACTOR - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Default correction factor value.
DEFAULT_DE_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader: Default supported files name pattern for JPL DE files.
DEFAULT_EXTRAPOLATION_THRESHOLD_SEC - Static variable in class org.orekit.propagation.analytical.Ephemeris: Default extrapolation time threshold: 1ms.
DEFAULT_INPOP_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader: Default supported files name pattern for IMCCE INPOP files.
DEFAULT_INTERPOLATION_METHOD - Static variable in class org.orekit.files.ccsds.OEMWriter: Default interpolation method if the user specifies none.
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_LAW - Static variable in interface org.orekit.propagation.FieldPropagator: Default attitude provider.
DEFAULT_LAW - Static variable in interface org.orekit.propagation.Propagator: Default attitude provider.
DEFAULT_MASS - Static variable in interface org.orekit.propagation.FieldPropagator: Default mass.
DEFAULT_MASS - Static variable in interface org.orekit.propagation.Propagator: Default mass.
DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.AbstractDetector: Default cmaximum number of iterations in the event time search.
DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.FieldAbstractDetector: Default cmaximum number of iterations in the event time search.
DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.AbstractDetector: Default maximum checking interval (s).
DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.FieldAbstractDetector: Default maximum checking interval (s).
DEFAULT_ORIGINATOR - Static variable in class org.orekit.files.ccsds.OEMWriter: Default originator field value if user specifies none.
DEFAULT_ORIGINATOR - Static variable in class org.orekit.files.ccsds.StreamingOemWriter: Default value for Keyword.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_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Default local pressure at viewpoint (Pa).
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.KlobucharIonoCoefficientsLoader: Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.time.TAIUTCDatFilesLoader: Default supported files name pattern.
DEFAULT_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Default local temperature at viewpoint (K).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.AbstractDetector: Default convergence threshold (s).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.FieldAbstractDetector: Default convergence threshold (s).
DelaunayArguments - Class in org.orekit.data: Delaunay arguments used for nutation or tides.
DelaunayArguments(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.DelaunayArguments: Simple constructor.
DELTA_R_FILE_NAME - Static variable in class org.orekit.models.earth.SaastamoinenModel: Default file name for δR correction term table.
dependsOnPositionOnly() - Method in class org.orekit.forces.drag.DragForce: Check if force models depends on position only.
dependsOnPositionOnly() - Method in interface org.orekit.forces.ForceModel: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.NewtonianAttraction: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.OceanTides: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.Relativity: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.SolidTides: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.HarmonicParametricAcceleration: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.PolynomialParametricAcceleration: Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Check if force models depends on position only.
derivative(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries: Evaluate time derivative of a set of Poisson series.
derivative(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries: Evaluate time derivative of a set of Poisson series.
derivative(double) - Method in class org.orekit.data.PolynomialNutation: Evaluate the time derivative of the polynomial.
derivative(T) - Method in class org.orekit.data.PolynomialNutation: Evaluate the time derivative of the polynomial.
differentiate(ParameterFunction, ParameterDriver, int, double) - Static method in class org.orekit.utils.Differentiation: Differentiate a scalar function using finite differences.
differentiate(StateFunction, int, AttitudeProvider, OrbitType, PositionAngle, double, int) - Static method in class org.orekit.utils.Differentiation: Differentiate a vector function using finite differences.
Differentiation - Class in org.orekit.utils: Utility class for differentiating various kinds of functions.
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.
displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.OceanLoading: Compute displacement of a ground reference point.
displacement(BodiesElements, Frame, Vector3D) - Method in interface org.orekit.models.earth.displacement.StationDisplacement: Compute displacement of a ground reference point.
displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.TidalDisplacement: Compute displacement of a ground reference point.
doEvent(SpacecraftState) - Method in class org.orekit.propagation.events.EventState: Notify the user's listener of the event.
doEvent(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventState: Notify the user's listener of the event.
DOP - Class in org.orekit.gnss: This class is a container for the result of a single DOP computation.
DOP(GeodeticPoint, AbsoluteDate, int, double, double, double, double, double) - Constructor for class org.orekit.gnss.DOP: Constructor.
DOP_MIN_ELEVATION - Static variable in class org.orekit.gnss.DOPComputer: Minimum elevation : 0°.
DOPComputer - Class in org.orekit.gnss: This class aims at computing the dilution of precision.
DormandPrince54IntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for DormandPrince54Integrator.
DormandPrince54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder: Build a new instance.
DormandPrince853IntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for DormandPrince853Integrator.
DormandPrince853IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder: Build a new instance.
DRAG_COEFFICIENT - Static variable in interface org.orekit.forces.drag.DragSensitive: Parameter name for drag coefficient enabling Jacobian processing.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[], String) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Compute acceleration due to drag, with parameters derivatives.
dragAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft: Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[]) - Method in interface org.orekit.forces.drag.DragSensitive: Compute the acceleration due to drag.
dragAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in interface org.orekit.forces.drag.DragSensitive: Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[], String) - Method in interface org.orekit.forces.drag.DragSensitive: Compute acceleration due to drag, with parameters derivatives.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[]) - Method in class org.orekit.forces.drag.IsotropicDrag: Compute the acceleration due to drag.
dragAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.drag.IsotropicDrag: Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[], String) - Method in class org.orekit.forces.drag.IsotropicDrag: Compute acceleration due to drag, with parameters derivatives.
DragForce - Class in org.orekit.forces.drag: Atmospheric drag force model.
DragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.DragForce: Simple constructor.
DragSensitive - Interface in org.orekit.forces.drag: Interface for spacecraft that are sensitive to atmospheric drag forces.
DSSTAtmosphericDrag - Class in org.orekit.propagation.semianalytical.dsst.forces: Atmospheric drag contribution to the DSSTPropagator.
DSSTAtmosphericDrag(Atmosphere, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Simple constructor assuming spherical spacecraft.
DSSTAtmosphericDrag(Atmosphere, DragSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Simple constructor with custom spacecraft.
DSSTForceModel - Interface in org.orekit.propagation.semianalytical.dsst.forces: This interface represents a force modifying spacecraft motion for a DSSTPropagator.
DSSTPropagator - Class in org.orekit.propagation.semianalytical.dsst: This class propagates orbits using the DSST theory.
DSSTPropagator(ODEIntegrator, boolean) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Create a new instance of DSSTPropagator.
DSSTPropagator(ODEIntegrator) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator: Create a new instance of DSSTPropagator.
DSSTSolarRadiationPressure - Class in org.orekit.propagation.semianalytical.dsst.forces: Solar radiation pressure contribution to the DSSTPropagator.
DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Simple constructor with default reference values and spherical spacecraft.
DSSTSolarRadiationPressure(PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Simple constructor with default reference values, but custom spacecraft.
DSSTSolarRadiationPressure(double, double, double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Constructor with customizable reference values but spherical spacecraft.
DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Complete constructor.
DSSTTesseral - Class in org.orekit.propagation.semianalytical.dsst.forces: Tesseral contribution to the central body gravitational perturbation.
DSSTTesseral(Frame, double, UnnormalizedSphericalHarmonicsProvider, int, int, int, int, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Simple constructor.
DSSTThirdBody - Class in org.orekit.propagation.semianalytical.dsst.forces: Third body attraction perturbation to the DSSTPropagator.
DSSTThirdBody(CelestialBody) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Complete constructor.
DSSTZonal - Class in org.orekit.propagation.semianalytical.dsst.forces: Zonal contribution to the central body gravitational perturbation.
DSSTZonal(UnnormalizedSphericalHarmonicsProvider, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Simple constructor.
DTM2000 - Class in org.orekit.forces.drag.atmosphere: This atmosphere model is the realization of the DTM-2000 model.
DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.forces.drag.atmosphere.DTM2000: Simple constructor for independent computation.
DTM2000InputParameters - Interface in org.orekit.forces.drag.atmosphere: Container for solar activity data, compatible with DTM2000 Atmosphere model.
durationFrom(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate: Compute the physically elapsed duration between two instants.
durationFrom(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate: Compute the physically elapsed duration between two instants.
durationFrom(AbsoluteDate) - Method in class org.orekit.time.FieldAbsoluteDate: Compute the physically elapsed duration between two instants.

E

e - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: final eccentricity.
e0sq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: original eccentricity squared.
EARTH - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Earth.
EARTH_ANGULAR_VELOCITY - Static variable in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Earth Angular Velocity, in rad/s, from TIRF model.
EARTH_MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory: Predefined name for Earth-Moon barycenter.
EarthITU453AtmosphereRefraction - Class in org.orekit.models.earth: Implementation of refraction model for Earth exponential atmosphere based on ITU-R P.834-7 recommendation.
EarthITU453AtmosphereRefraction(double) - Constructor for class org.orekit.models.earth.EarthITU453AtmosphereRefraction: Creates a new default instance.
EarthShape - Interface in org.orekit.models.earth: All models of Earth's shape have some common properties that are not shared with arbitrary BodyShapes.
EarthStandardAtmosphereRefraction - Class in org.orekit.models.earth: Implementation of refraction model for Earth standard atmosphere.
EarthStandardAtmosphereRefraction() - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Creates a new default instance.
EarthStandardAtmosphereRefraction(double, double) - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction: Creates an instance given a specific pressure and temperature.
ecc - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Eccentricity.
eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit: Computes the mean latitude argument from the eccentric latitude argument.
eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit: Computes the mean longitude argument from the eccentric longitude argument.
eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit: Computes the mean latitude argument from the eccentric latitude argument.
eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit: Computes the mean longitude argument from the eccentric longitude argument.
eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit: Computes the true latitude argument from the eccentric latitude argument.
eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit: Computes the true longitude argument from the eccentric longitude argument.
eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit: Computes the true latitude argument from the eccentric latitude argument.
eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit: Computes the true longitude argument from the eccentric longitude argument.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder: Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder: Sets the Earth Centered Inertial frame used for propagation.
EcksteinHechlerPropagator - Class in org.orekit.propagation.analytical: This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Private helper constructor.
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit and potential.
EcksteinHechlerPropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, mass and potential provider.
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, mass and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, attitude provider and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, attitude provider and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, attitude provider, mass and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagatorBuilder - Class in org.orekit.propagation.conversion: Builder for Eckstein-Hechler propagator.
EcksteinHechlerPropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder: Build a new instance.
EcksteinHechlerPropagatorBuilder(Orbit, double, double, TideSystem, double, double, double, double, double, OrbitType, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder: Build a new instance.
EclipseDetector - Class in org.orekit.propagation.events: Finder for satellite eclipse related events.
EclipseDetector(PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector: Build a new eclipse detector.
EclipseDetector(double, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector: Build a new eclipse detector.
EclipseDetector(double, double, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector: Build a new eclipse detector.
EclipticProvider - Class in org.orekit.frames: An inertial frame aligned with the ecliptic.
EclipticProvider(IERSConventions) - Constructor for class org.orekit.frames.EclipticProvider: Create a transform provider from MOD to an ecliptically aligned frame.
eeta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: original eccentricity * eta.
EGM96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized second zonal coefficient from EGM96 model: -1.08262668355315e-3.
EGM96_EARTH_C30 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized third zonal coefficient from EGM96 model: 2.53265648533224e-6.
EGM96_EARTH_C40 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized fourth zonal coefficient from EGM96 model: 1.619621591367e-6.
EGM96_EARTH_C50 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized fifth zonal coefficient from EGM96 model: 2.27296082868698e-7.
EGM96_EARTH_C60 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized sixth zonal coefficient from EGM96 model: -5.40681239107085e-7.
EGM96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Earth equatorial radius from EGM96 model: 6378136.3 m.
EGM96_EARTH_MU - Static variable in interface org.orekit.utils.Constants: Earth gravitational constant from EGM96 model: 3.986004415e14 m³/s².
EGM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for EGM files.
EGMFormatReader - Class in org.orekit.forces.gravity.potential: This reader is adapted to the EGM Format.
EGMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader: Simple constructor.
EGMFormatReader(String, boolean, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader: Simple constructor that allows overriding 'standard' EGM96 ae and mu with WGS84 variants.
EIGEN5C_EARTH_C20 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized second zonal coefficient from EIGEN5C model: -1.082626457231767e-3.
EIGEN5C_EARTH_C30 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized third zonal coefficient from EIGEN5C model: 2.532547231862799e-6.
EIGEN5C_EARTH_C40 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized fourth zonal coefficient from EIGEN5C model: 1.619964434136e-6.
EIGEN5C_EARTH_C50 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized fifth zonal coefficient from EIGEN5C model: 2.277928487005437e-7.
EIGEN5C_EARTH_C60 - Static variable in interface org.orekit.utils.Constants: Earth un-normalized sixth zonal coefficient from EIGEN5C model: -5.406653715879098e-7.
EIGEN5C_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants: Earth equatorial radius from EIGEN5C model: 6378136.46 m.
EIGEN5C_EARTH_MU - Static variable in interface org.orekit.utils.Constants: Earth gravitational constant from EIGEN5C model: 3.986004415e14 m³/s².
ElevationDetector - Class in org.orekit.propagation.events: Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.
ElevationDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector: Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.
ElevationDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector: Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.
ElevationExtremumDetector - Class in org.orekit.propagation.events: Detector for elevation extremum with respect to a ground point.
ElevationExtremumDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector: Build a new detector.
ElevationExtremumDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector: Build a detector.
ElevationMask - Class in org.orekit.utils: Class for modeling the ground elevation values around a given point.
ElevationMask(double[][]) - Constructor for class org.orekit.utils.ElevationMask: Creates an instance of an Elevation mask based on the passed in parameter.
Ellipse - Class in org.orekit.bodies: Model of a 2D ellipse in 3D space.
Ellipse(Vector3D, Vector3D, Vector3D, double, double, Frame) - Constructor for class org.orekit.bodies.Ellipse: Simple constructor.
Ellipsoid - Class in org.orekit.bodies: Modeling of a general three-axes ellipsoid.
Ellipsoid(Frame, double, double, double) - Constructor for class org.orekit.bodies.Ellipsoid: Simple constructor.
EllipsoidTessellator - Class in org.orekit.models.earth.tessellation: Class used to tessellate an interest zone on an ellipsoid in either tiles or grids of geodetic points.
EllipsoidTessellator(OneAxisEllipsoid, TileAiming, int) - Constructor for class org.orekit.models.earth.tessellation.EllipsoidTessellator: Simple constructor.
ellipticEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit: Computes the mean anomaly from the elliptic eccentric anomaly.
ellipticEccentricToMean(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit: Computes the mean anomaly from the elliptic eccentric anomaly.
ellipticEccentricToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit: Computes the true anomaly from the elliptic eccentric anomaly.
ellipticEccentricToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit: Computes the true anomaly from the elliptic eccentric anomaly.
ellipticKeplerianToPosition(T, T, T, T, T, T, double) - Static method in class org.orekit.orbits.FieldKeplerianOrbit: Compute position from elliptic Keplerian parameters.
EME2000_ALIGNED - Static variable in class org.orekit.attitudes.InertialProvider: Dummy attitude provider, perfectly aligned with the EME2000 frame.
emptyCache() - Static method in class org.orekit.utils.ImmutableTimeStampedCache: Get an empty immutable cache, cast to the correct type.
EnablingPredicate<S extends EventDetector> - Interface in org.orekit.propagation.events: This interface represents an event enabling predicate function.
endParse() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: End parsing.
ensureCompatibleAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldSpacecraftState: Check if two instances have the same set of additional states available.
ensureCompatibleAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.SpacecraftState: Check if two instances have the same set of additional states available.
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) - Constructor for class org.orekit.frames.EOPEntry: Simple constructor.
EOPHistory - Class in org.orekit.frames: This class loads any kind of Earth Orientation Parameter data throughout a large time range.
EOPHistory(IERSConventions, Collection<EOPEntry>, boolean) - Constructor for class org.orekit.frames.EOPHistory: Simple constructor.
EOPHistoryLoader - Interface in org.orekit.frames: Interface for loading Earth Orientation Parameters history.
EphemeridesBlock() - Constructor for class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: EphemeridesBlock constructor.
Ephemeris - Class in org.orekit.propagation.analytical: This class is designed to accept and handle tabulated orbital entries.
Ephemeris(List<SpacecraftState>, int) - Constructor for class org.orekit.propagation.analytical.Ephemeris: Constructor with tabulated states.
Ephemeris(List<SpacecraftState>, int, double) - Constructor for class org.orekit.propagation.analytical.Ephemeris: Constructor with tabulated states.
EPHEMERIS_GENERATION_MODE - Static variable in interface org.orekit.propagation.FieldPropagator: Indicator for ephemeris generation mode.
EPHEMERIS_GENERATION_MODE - Static variable in interface org.orekit.propagation.Propagator: Indicator for ephemeris generation mode.
EphemerisFile - 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 - Interface in org.orekit.files.general: A segment of an ephemeris for a satellite.
EphemerisFile.SatelliteEphemeris - Interface in org.orekit.files.general: Contains the information about a single satellite from an EphemerisFile.
EphemerisFileParser - 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.
equals(Object) - Method in class org.orekit.bodies.FieldGeodeticPoint
equals(Object) - Method in class org.orekit.bodies.GeodeticPoint
equals(Object) - Method in class org.orekit.models.earth.displacement.Tide
equals(Object) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
equals(Object) - Method in class org.orekit.time.AbsoluteDate: Check if the instance represent the same time as another instance.
equals(Object) - Method in class org.orekit.time.DateComponents
equals(Object) - Method in class org.orekit.time.DateTimeComponents
equals(Object) - Method in class org.orekit.time.FieldAbsoluteDate: Check if the instance represent the same time as another instance.
equals(Object) - Method in class org.orekit.time.TimeComponents
EquinoctialOrbit - Class in org.orekit.orbits: This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
EquinoctialOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Creates a new instance.
EquinoctialOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Creates a new instance.
EquinoctialOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Constructor from Cartesian parameters.
EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Constructor from Cartesian parameters.
EquinoctialOrbit(Orbit) - Constructor for class org.orekit.orbits.EquinoctialOrbit: Constructor from any kind of orbital parameters.
equinoctialToPosition(T, T, T, T, T, T, double) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit: Compute position from equinoctial parameters.
estimate(Frame, PV, PV, PV) - Method in class org.orekit.estimation.iod.IodGibbs: Give an initial orbit estimation, assuming Keplerian motion.
estimate(Frame, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate) - Method in class org.orekit.estimation.iod.IodGibbs: Give an initial orbit estimation, assuming Keplerian motion.
estimate(Vector3D, Vector3D, Vector3D, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, double, double) - Method in class org.orekit.estimation.iod.IodGooding: Orbit got from Observed Three Lines of Sight (angles only).
estimate(Frame, boolean, int, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate) - Method in class org.orekit.estimation.iod.IodLambert: Estimate a Keplerian orbit given two position vectors and a duration.
estimate() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Estimate the orbital, propagation and measurements parameters.
estimate(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Estimate the theoretical value of the measurement.
estimate(int, int, SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Estimate the theoretical value of the measurement.
EstimatedEarthFrameProvider - Class in org.orekit.estimation.measurements: Class modeling an Earth frame whose Earth Orientation Parameters can be estimated.
EstimatedEarthFrameProvider(UT1Scale) - Constructor for class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Build an estimated Earth frame.
EstimatedMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements: Class holding an estimated theoretical value associated to an observed measurement.
EstimatedMeasurement(T, int, int, SpacecraftState[], TimeStampedPVCoordinates[]) - Constructor for class org.orekit.estimation.measurements.EstimatedMeasurement: Simple constructor.
estimateRate(Rotation, Rotation, double) - Static method in class org.orekit.utils.AngularCoordinates: Estimate rotation rate between two orientations.
estimateRate(FieldRotation<T>, FieldRotation<T>, double) - Static method in class org.orekit.utils.FieldAngularCoordinates: Estimate rotation rate between two orientations.
estimateRate(FieldRotation<T>, FieldRotation<T>, T) - Static method in class org.orekit.utils.FieldAngularCoordinates: Estimate rotation rate between two orientations.
estimateVelocity(FieldVector3D<T>, FieldVector3D<T>, double) - Static method in class org.orekit.utils.FieldPVCoordinates: Estimate velocity between two positions.
estimateVelocity(Vector3D, Vector3D, double) - Static method in class org.orekit.utils.PVCoordinates: Estimate velocity between two positions.
EstimationModifier<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements: Interface for estimated measurements modifiers used for orbit determination.
EstimationsProvider - Interface in org.orekit.estimation.measurements: Interface for retrieving estimated measurements during orbit determination.
eta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: eta from SPTRCK #3.
etasq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator: eta squared.
EulerIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for EulerIntegrator.
EulerIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.EulerIntegratorBuilder: Build a new instance.
evaluateAll(AbsoluteDate) - Method in class org.orekit.data.FundamentalNutationArguments: Evaluate all fundamental arguments for the current date (Delaunay plus planetary).
evaluateAll(FieldAbsoluteDate<T>) - Method in class org.orekit.data.FundamentalNutationArguments: Evaluate all fundamental arguments for the current date (Delaunay plus planetary).
evaluateStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState: Evaluate the impact of the proposed step on the event detector.
evaluateStep(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState: Evaluate the impact of the proposed step on the event detector.
evaluateTC(AbsoluteDate) - Method in enum org.orekit.utils.IERSConventions: Evaluate the date offset between the current date and the reference date.
evaluateTC(FieldAbsoluteDate<T>) - 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.
EventDetector - Interface in org.orekit.propagation.events: This interface represents space-dynamics aware events detectors.
EventEnablingPredicateFilter<T extends EventDetector> - Class in org.orekit.propagation.events: Wrapper used to detect events only when enabled by an external predicated function.
EventEnablingPredicateFilter(T, EnablingPredicate<T>) - Constructor for class org.orekit.propagation.events.EventEnablingPredicateFilter: Wrap an event detector.
EventHandler<T extends EventDetector> - Interface in org.orekit.propagation.events.handlers: An interface defining how to override event handling behavior in the standard propagator eventing classes without requiring subclassing.
EventHandler.Action - Enum in org.orekit.propagation.events.handlers: Enumerate for actions to be performed when an event occurs.
eventIsEnabled(SpacecraftState, S, double) - Method in interface org.orekit.propagation.events.EnablingPredicate: Compute an event enabling function of state.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.AbstractDetector: Handle the event.
eventOccurred(SpacecraftState, boolean) - Method in interface org.orekit.propagation.events.EventDetector: Handle the event.
eventOccurred(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.events.FieldAbstractDetector: Handle the event.
eventOccurred(FieldSpacecraftState<T>, boolean) - Method in interface org.orekit.propagation.events.FieldEventDetector: Handle the event.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.ContinueOnEvent: Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, T, boolean) - Method in interface org.orekit.propagation.events.handlers.EventHandler: eventOccurred method mirrors the same interface method as in EventDetector and its subclasses, but with an additional parameter that allows the calling method to pass in an object from the detector which would have potential additional data to allow the implementing class to determine the correct return state.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldContinueOnEvent: Specific implementation of the eventOccurred interface.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler: eventOccurred method mirrors the same interface method as in EventDetector and its subclasses, but with an additional parameter that allows the calling method to pass in an object from the detector which would have potential additional data to allow the implementing class to determine the correct return state.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnDecreasing: Handle a detection event and choose what to do next.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnEvent: Specific implementation of the eventOccurred interface.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnIncreasing: Handle a detection event and choose what to do next.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnDecreasing: Handle a detection event and choose what to do next.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnEvent: Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnIncreasing: Handle a detection event and choose what to do next.
EventShifter<T extends EventDetector> - Class in org.orekit.propagation.events: Wrapper shifting events occurrences times.
EventShifter(T, boolean, double, double) - Constructor for class org.orekit.propagation.events.EventShifter: Build a new instance.
EventsLogger - Class in org.orekit.propagation.events: This class logs events detectors events during propagation.
EventsLogger() - Constructor for class org.orekit.propagation.events.EventsLogger: Simple constructor.
EventsLogger.LoggedEvent - Class in org.orekit.propagation.events: Class for logged events entries.
EventSlopeFilter<T extends EventDetector> - Class in org.orekit.propagation.events: Wrapper used to detect only increasing or decreasing events.
EventSlopeFilter(T, FilterType) - Constructor for class org.orekit.propagation.events.EventSlopeFilter: Wrap an event detector.
EventState<T extends EventDetector> - Class in org.orekit.propagation.events: This class handles the state for one event detector during integration steps.
EventState(T) - Constructor for class org.orekit.propagation.events.EventState: Simple constructor.
EventState.EventOccurrence - Class in org.orekit.propagation.events: Class to hold the data related to an event occurrence that is needed to decide how to modify integration.
extendListOfLists(List<List<Double>>, int, int, double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Extend a list of lists of coefficients if needed.

F

f - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Equinoctial frame f vector.
Facet(Vector3D, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet: Simple constructor.
FactoryManagedFrame - Class in org.orekit.frames: Base class for the predefined frames that are managed by FramesFactory.
FactoryManagedFrame(Frame, TransformProvider, boolean, Predefined) - Constructor for class org.orekit.frames.FactoryManagedFrame: Simple constructor.
feed(Pattern, DataLoader) - Method in class org.orekit.data.ClasspathCrawler: Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader) - Method in interface org.orekit.data.DataProvider: Feed a data file loader by browsing the data collection.
feed(String, DataLoader) - Method in class org.orekit.data.DataProvidersManager: Feed a data file loader by browsing all data providers.
feed(Pattern, DataLoader) - Method in class org.orekit.data.DirectoryCrawler: Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader) - Method in class org.orekit.data.NetworkCrawler: Feed a data file loader by browsing the data collection.
feed(Pattern, DataLoader) - Method in class org.orekit.data.ZipJarCrawler: Feed a data file loader by browsing the data collection.
FES_CHAT_EPSILON_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for FES C hat and epsilon tides files.
FES_CNM_SNM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for FES Cnm, Snm tides files.
FES_HF_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory: Default regular expression for FES Hf tides files.
FESCHatEpsilonReader - Class in org.orekit.forces.gravity.potential: Reader for ocean tides files following the fes2004.dat format.
FESCHatEpsilonReader(String, double, double, OceanLoadDeformationCoefficients, Map<Integer, Double>) - Constructor for class org.orekit.forces.gravity.potential.FESCHatEpsilonReader: Simple constructor.
FESCnmSnmReader - Class in org.orekit.forces.gravity.potential: Reader for ocean tides files following the fes2004_Cnm-Snm.dat format.
FESCnmSnmReader(String, double) - Constructor for class org.orekit.forces.gravity.potential.FESCnmSnmReader: Simple constructor.
FieldAbsoluteDate<T extends RealFieldElement<T>> - Class in org.orekit.time: This class represents a specific instant in time.
FieldAbsoluteDate(Field<T>, AbsoluteDate) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an AbsoluteDate.
FieldAbsoluteDate(Field<T>) - Constructor for class org.orekit.time.FieldAbsoluteDate: Create an instance with a default value (FieldAbsoluteDate.getJ2000Epoch(Field)).
FieldAbsoluteDate(FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(Field<T>, String, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from a location (parsed from a string) in a time scale.
FieldAbsoluteDate(Field<T>, DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, DateComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, int, int, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, Month, int, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, Date, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from a location in a time scale.
FieldAbsoluteDate(FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(AbsoluteDate, T) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(FieldAbsoluteDate<T>, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate: Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.
FieldAbstractAnalyticalPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation.analytical: Common handling of FieldPropagator methods for analytical propagators.
FieldAbstractAnalyticalPropagator(Field<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Build a new instance.
FieldAbstractDetector<D extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events: Common parts shared by several orbital events finders.
FieldAbstractDetector(T, T, int, FieldEventHandler<? super D, T>) - Constructor for class org.orekit.propagation.events.FieldAbstractDetector: Build a new instance.
FieldAbstractIntegratedPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation.integration: Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.
FieldAbstractIntegratedPropagator(Field<T>, FieldODEIntegrator<T>, boolean) - Constructor for class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Build a new instance.
FieldAbstractIntegratedPropagator.MainStateEquations<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.integration: Differential equations for the main state (orbit, attitude and mass).
FieldAbstractPropagator<T extends RealFieldElement<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.
FieldAdditionalEquations<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.integration: This interface allows users to add their own differential equations to a numerical propagator.
FieldAdditionalStateProvider<T extends RealFieldElement<T>> - Interface in org.orekit.propagation: This interface represents providers for additional state data beyond SpacecraftState.
FieldAltitudeDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events: Finder for satellite altitude crossing events.
FieldAltitudeDetector(T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector: Build a new altitude detector.
FieldAltitudeDetector(T, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector: Build a new altitude detector.
FieldAltitudeDetector(T, T, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector: Build a new altitude detector.
FieldAngularCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils: Simple container for rotation / rotation rate pairs, using RealFieldElement.
FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates: Builds a rotation/rotation rate pair.
FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates: Builds a rotation / rotation rate / rotation acceleration triplet.
FieldAngularCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.FieldAngularCoordinates: Build the rotation that transforms a pair of pv coordinates into another one.
FieldAngularCoordinates(Field<T>, AngularCoordinates) - Constructor for class org.orekit.utils.FieldAngularCoordinates: Builds a FieldAngularCoordinates from a field and a regular AngularCoordinates.
FieldApsideDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events: Finder for apside crossing events.
FieldApsideDetector(FieldOrbit<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector: Build a new instance.
FieldApsideDetector(T, FieldOrbit<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector: Build a new instance.
FieldAttitude<T extends RealFieldElement<T>> - Class in org.orekit.attitudes: This class handles attitude definition at a given date.
FieldAttitude(Frame, TimeStampedFieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude: Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, FieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude: Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.attitudes.FieldAttitude: Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, Rotation, Vector3D, Vector3D, Field<T>) - Constructor for class org.orekit.attitudes.FieldAttitude: Creates a new instance.
FieldAttitude(Field<T>, Attitude) - Constructor for class org.orekit.attitudes.FieldAttitude: Builds an instance for a regular Attitude.
FieldBodiesElements<T extends RealFieldElement<T>> - Class in org.orekit.data: Elements of the bodies having an effect on nutation.
FieldBodiesElements(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldBodiesElements: Simple constructor.
FieldBoundedPropagator<T extends RealFieldElement<T>> - Interface in org.orekit.propagation: This interface is intended for ephemerides valid only during a time range.
FieldCartesianOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits: This class holds Cartesian orbital parameters.
FieldCartesianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldCartesianOrbit: Constructor from Cartesian parameters.
FieldCartesianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldCartesianOrbit: Constructor from Cartesian parameters.
FieldCartesianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCartesianOrbit: Constructor from any kind of orbital parameters.
FieldCircularOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits: This class handles circular orbital parameters.
FieldCircularOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldCircularOrbit: Creates a new instance.
FieldCircularOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldCircularOrbit: Creates a new instance.
FieldCircularOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldCircularOrbit: Constructor from Cartesian parameters.
FieldCircularOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldCircularOrbit: Constructor from Cartesian parameters.
FieldCircularOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCircularOrbit: Constructor from any kind of orbital parameters.
FieldContinueOnEvent<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers: Event handler which will always return continue as a state.
FieldContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldContinueOnEvent
FieldDateDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events: Finder for date events.
FieldDateDetector(T, T, FieldTimeStamped<T>...) - Constructor for class org.orekit.propagation.events.FieldDateDetector: Build a new instance.
FieldDateDetector(FieldAbsoluteDate<T>) - Constructor for class org.orekit.propagation.events.FieldDateDetector: Build a new instance.
FieldDelaunayArguments<T extends RealFieldElement<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.
FieldEcksteinHechlerPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation.analytical: This class propagates a FieldSpacecraftState using the analytical Eckstein-Hechler model.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from FieldOrbit and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Private helper constructor.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from FieldOrbit and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from FieldOrbit, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, T, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from FieldOrbit, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from FieldOrbit, attitude provider and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from FieldOrbit, attitude provider and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from FieldOrbit, attitude provider, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEclipseDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events: Finder for satellite eclipse related events.
FieldEclipseDetector(PVCoordinatesProvider, double, PVCoordinatesProvider, double, Field<T>) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector: Build a new eclipse detector.
FieldEclipseDetector(T, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector: Build a new eclipse detector.
FieldEclipseDetector(T, T, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector: Build a new eclipse detector.
FieldElevationDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events: Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.
FieldElevationDetector(Field<T>, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector: Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.
FieldElevationDetector(T, T, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector: Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.
FieldEquinoctialOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits: This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
FieldEquinoctialOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit: Creates a new instance.
FieldEquinoctialOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit: Creates a new instance.
FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit: Constructor from Cartesian parameters.
FieldEquinoctialOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit: Constructor from Cartesian parameters.
FieldEquinoctialOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit: Constructor from any kind of orbital parameters.
FieldEventDetector<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.events: This interface represents space-dynamics aware events detectors.
FieldEventHandler<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Interface in org.orekit.propagation.events.handlers: An interface defining how to override event handling behavior in the standard propagator eventing classes without requiring subclassing.
FieldEventHandler.Action - Enum in org.orekit.propagation.events.handlers: Enumerate for actions to be performed when an event occurs.
FieldEventsLogger<T extends RealFieldElement<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 RealFieldElement<T>> - Class in org.orekit.propagation.events: Class for logged events entries.
FieldEventState<D extends FieldEventDetector<T>,T extends RealFieldElement<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 RealFieldElement<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.
FieldGeodeticPoint<T extends RealFieldElement<T>> - Class in org.orekit.bodies: Point location relative to a 2D body surface, using RealFieldElement.
FieldGeodeticPoint(T, T, T) - Constructor for class org.orekit.bodies.FieldGeodeticPoint: Build a new instance.
FieldIntegratedEphemeris<T extends RealFieldElement<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>, boolean, FieldDenseOutputModel<T>, Map<String, T[]>, List<FieldAdditionalStateProvider<T>>, String[]) - Constructor for class org.orekit.propagation.integration.FieldIntegratedEphemeris: Creates a new instance of IntegratedEphemeris.
FieldKeplerianOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits: This class handles traditional Keplerian orbital parameters.
FieldKeplerianOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Creates a new instance.
FieldKeplerianOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Creates a new instance.
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Constructor from Cartesian parameters.
FieldKeplerianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Constructor from Cartesian parameters.
FieldKeplerianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit: Constructor from any kind of orbital parameters.
FieldKeplerianPropagator<T extends RealFieldElement<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>, double) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator: Build a propagator from orbit and central attraction coefficient μ.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator: Build a propagator from orbit and attitude provider.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator: Build a propagator from orbit, attitude provider and central attraction coefficient μ.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, double, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator: Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
FieldModeHandler<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.integration: Common interface for all propagator mode handlers initialization.
FieldNodeDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events: Finder for node crossing events.
FieldNodeDetector(FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector: Build a new instance.
FieldNodeDetector(T, FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector: Build a new instance.
FieldNumericalPropagator<T extends RealFieldElement<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.
FieldOfView - Class in org.orekit.propagation.events: Class representing a spacecraft sensor Field Of View.
FieldOfView(SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.FieldOfView: Build a new instance.
FieldOfView(Vector3D, Vector3D, double, Vector3D, double, double) - Constructor for class org.orekit.propagation.events.FieldOfView: Build a Field Of View with dihedral shape (i.e.
FieldOfView(Vector3D, Vector3D, double, int, double) - Constructor for class org.orekit.propagation.events.FieldOfView: Build Field Of View with a regular polygon shape.
FieldOfViewDetector - Class in org.orekit.propagation.events: Finder for target entry/exit events with respect to a satellite sensor Field Of View.
FieldOfViewDetector(PVCoordinatesProvider, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector: Build a new instance.
FieldOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits: This class handles orbital parameters.
FieldOrbit(Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldOrbit: Default constructor.
FieldOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldOrbit: Set the orbit from Cartesian parameters.
FieldOrekitFixedStepHandler<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.sampling: This interface is a space-dynamics aware fixed size step handler.
FieldOrekitStepHandler<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.sampling: This interface is a space-dynamics aware step handler.
FieldOrekitStepHandlerMultiplexer<T extends RealFieldElement<T>> - Class in org.orekit.propagation.sampling: This class gathers several OrekitStepHandler instances into one.
FieldOrekitStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.FieldOrekitStepHandlerMultiplexer: Simple constructor.
FieldOrekitStepInterpolator<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.sampling: This interface is a space-dynamics aware step interpolator.
FieldOrekitStepNormalizer<T extends RealFieldElement<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.
FieldPoleCorrection<T extends RealFieldElement<T>> - Class in org.orekit.frames: Simple container class for pole correction parameters.
FieldPoleCorrection(T, T) - Constructor for class org.orekit.frames.FieldPoleCorrection: Simple constructor.
FieldPropagator<T extends RealFieldElement<T>> - Interface in org.orekit.propagation: This interface provides a way to propagate an orbit at any time.
FieldPVCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils: Simple container for Position/Velocity pairs, using RealFieldElement.
FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Builds a FieldPVCoordinates triplet with zero acceleration.
FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Builds a FieldPVCoordinates triplet.
FieldPVCoordinates(Field<T>, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Builds a FieldPVCoordinates from a field and a regular PVCoordinates.
FieldPVCoordinates(double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Multiplicative constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Multiplicative constructor.
FieldPVCoordinates(T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Multiplicative constructor.
FieldPVCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Subtractive constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates: Linear constructor.
FieldPVCoordinatesProvider<T extends RealFieldElement<T>> - Interface in org.orekit.utils: Interface for PV coordinates providers.
FieldSpacecraftState<T extends RealFieldElement<T>> - Class in org.orekit.propagation: This class is the representation of a complete state holding orbit, attitude and mass information at a given date.
FieldSpacecraftState(FieldOrbit<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit and attitude provider.
FieldSpacecraftState(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Create a new instance from orbit and mass.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit, attitude provider and mass.
FieldSpacecraftState(FieldOrbit<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit and attitude provider.
FieldSpacecraftState(FieldOrbit<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Create a new instance from orbit and mass.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Build a spacecraft state from orbit, attitude provider and mass.
FieldSpacecraftState(Field<T>, SpacecraftState) - Constructor for class org.orekit.propagation.FieldSpacecraftState: Convert a SpacecraftState.
FieldStateMapper<T extends RealFieldElement<T>> - Class in org.orekit.propagation.integration: This class maps between raw double elements and FieldSpacecraftState instances.
FieldStateMapper(FieldAbsoluteDate<T>, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.FieldStateMapper: Simple constructor.
FieldStopOnDecreasing<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers: Handle a detection event and choose what to do next.
FieldStopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnDecreasing
FieldStopOnEvent<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers: Event handler which will always return continue as a state.
FieldStopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnEvent
FieldStopOnIncreasing<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers: Handle a detection event and choose what to do next.
FieldStopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnIncreasing
FieldTimeDerivativesEquations<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.numerical: Interface summing up the contribution of several forces into orbit and mass derivatives.
FieldTimeInterpolable<T extends FieldTimeInterpolable<T,KK>,KK extends RealFieldElement<KK>> - Interface in org.orekit.time: This interface represents objects that can be interpolated in time.
FieldTimeShiftable<T extends FieldTimeInterpolable<T,KK>,KK extends RealFieldElement<KK>> - Interface in org.orekit.time: This interface represents objects that can be shifted in time.
FieldTimeSpanMap<T,D extends RealFieldElement<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 RealFieldElement<D>> - Class in org.orekit.utils: Local class holding transition times.
FieldTimeStamped<T extends RealFieldElement<T>> - Interface in org.orekit.time: This interface represents objects that have a AbsoluteDate date attached to them.
FieldTransform<T extends RealFieldElement<T>> - Class in org.orekit.frames: Transformation class in three dimensional space.
FieldTransform(Field<T>, Transform) - Constructor for class org.orekit.frames.FieldTransform: Build a transform from a regular transform.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a translation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a translation transform, with its first time derivative.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a translation transform, with its first and second time derivatives.
FieldTransform(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a translation transform, with its first time derivative.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldAngularCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldTransform<T>, FieldTransform<T>) - Constructor for class org.orekit.frames.FieldTransform: Build a transform by combining two existing ones.
FieldTransformGenerator<T extends RealFieldElement<T>> - Class in org.orekit.frames: Generator to use field transforms in GenericTimeStampedCache.
FieldTransformGenerator(Field<T>, int, TransformProvider, double) - Constructor for class org.orekit.frames.FieldTransformGenerator: simple constructor.
FIFTIES_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
FIFTIES_EPOCH - Static variable in class org.orekit.time.DateComponents: Reference epoch for 1950 dates: 1950-01-01.
fillHalfRow(T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit: Fill a Jacobian half row with a single vector.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a single vector.
fillHalfRow(double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit: Fill a Jacobian half row with a linear combination of vectors.
fillHistory(IERSConventions.NutationCorrectionConverter, SortedSet<EOPEntry>) - Method in interface org.orekit.frames.EOPHistoryLoader: Load celestial body.
filter(boolean) - Method in class org.orekit.utils.ParameterDriversList: Filter parameters to keep only one type of selection status.
FilterType - Enum in org.orekit.propagation.events: Enumerate for filtering events.
findEOP(Frame) - Static method in class org.orekit.frames.FramesFactory: Retrieve EOP from a frame hierarchy.
FiniteDifferencePropagatorConverter - Class in org.orekit.propagation.conversion: Propagator converter using finite differences to compute the Jacobian.
FiniteDifferencePropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter: Simple constructor.
fit() - Method in class org.orekit.utils.SecularAndHarmonic: Fit parameters.
FixedNumberInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities: Interpolation grid where a fixed number of points are evenly spaced between the start and the end of the integration step.
FixedNumberInterpolationGrid(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid: Constructor.
FixedRate - Class in org.orekit.attitudes: This class handles a simple attitude provider at constant rate around a fixed axis.
FixedRate(Attitude) - Constructor for class org.orekit.attitudes.FixedRate: Creates a new instance.
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: 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.FixedTroposphericDelay: Creates a new FixedTroposphericDelay instance.
FixedTroposphericDelay(String) - Constructor for class org.orekit.models.earth.FixedTroposphericDelay: Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the DataProvidersManager.
FLOW_RATE - Static variable in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Parameter name for flow rate.
FootprintOverlapDetector - Class in org.orekit.propagation.events: Detector triggered by geographical region entering/leaving a spacecraft sensor Field Of View.
FootprintOverlapDetector(FieldOfView, OneAxisEllipsoid, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.FootprintOverlapDetector: Build a new instance.
ForceModel - Interface in org.orekit.forces: This interface represents a force modifying spacecraft motion.
Frame - Class in org.orekit.frames: Tridimensional references frames class.
Frame(Frame, Transform, String) - Constructor for class org.orekit.frames.Frame: Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, TransformProvider, String) - Constructor for class org.orekit.frames.Frame: Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.Frame: Build a frame from its transform with respect to its parent.
Frame(Frame, TransformProvider, String, boolean) - Constructor for class org.orekit.frames.Frame: Build a frame from its transform with respect to its parent.
FrameAncestorException - Exception in org.orekit.errors: This class is the base class for exception thrown by the UpdatableFrame.updateTransform method.
FrameAncestorException(Localizable, Object...) - Constructor for exception org.orekit.errors.FrameAncestorException: Simple constructor.
FramesFactory - Class in org.orekit.frames: Factory for predefined reference frames.
freeze() - Method in class org.orekit.frames.FieldTransform: Get a frozen transform.
freeze() - Method in class org.orekit.frames.Transform: Get a frozen transform.
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, List<double[]>) - Constructor for class org.orekit.data.FundamentalNutationArguments: Build a model of fundamental arguments from an IERS table file.
FUTURE_INFINITY - Static variable in class org.orekit.time.AbsoluteDate: Dummy date at infinity in the future direction.

G

g(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.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.ApsideDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.BooleanDetector
g(SpacecraftState) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector: 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 class org.orekit.propagation.events.EclipseDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector: Compute the value of the detection function.
g(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventShifter: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventSlopeFilter: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldApsideDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldDateDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector: Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector: Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FieldOfViewDetector: Compute the value of the switching function.
g(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.GeographicZoneDetector: Compute the value of the detection 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.LatitudeCrossingDetector: Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector: Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector: Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector: Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.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.PositionAngleDetector: Compute the value of the detection function.
g - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Equinoctial frame g vector.
G0_STANDARD_GRAVITY - Static variable in interface org.orekit.utils.Constants: Standard gravity constant, used in maneuvers definition: 9.80665 m/s².
GALILEO_EPOCH - Static variable in class org.orekit.time.AbsoluteDate: Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
GALILEO_EPOCH - Static variable in class org.orekit.time.DateComponents: Reference epoch for Galileo System Time: 1999-08-22.
GalileoScale - Class in org.orekit.time: Galileo system time scale.
GammaMnsFunction - Class in org.orekit.propagation.semianalytical.dsst.utilities: Compute the Γ^m_n,s(γ) function from equation 2.7.1-(13).
GammaMnsFunction(int, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction: Simple constructor.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.FieldTransformGenerator: Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.TransformGenerator: Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedGenerator: Generate a chronologically sorted list of entries to be cached.
generateCartesianOrbit() - Method in class org.orekit.files.ccsds.OMMFile: Generate a CartesianOrbit from the KeplerianOrbit.
generateCartesianOrbit() - Method in class org.orekit.files.ccsds.OPMFile: Generate a CartesianOrbit from the OPM state vector data.
generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.OMMFile: Generate a KeplerianOrbit based on the OMM mean Keplerian elements.
generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.OPMFile: Generate a KeplerianOrbit from the OPM Keplerian elements if hasKeplerianElements is true, or from the state vector data otherwise.
generateSpacecraftState() - Method in class org.orekit.files.ccsds.OMMFile: Generate spacecraft state from the KeplerianOrbit generated by generateKeplerianOrbit.
generateSpacecraftState() - Method in class org.orekit.files.ccsds.OPMFile: Generate spacecraft state from the CartesianOrbit generated by generateCartesianOrbit.
generateTLE() - Method in class org.orekit.files.ccsds.OMMFile: Generate TLE from OMM file.
GenericTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils: Generic thread-safe cache for time-stamped data.
GenericTimeStampedCache(int, int, double, double, TimeStampedGenerator<T>) - Constructor for class org.orekit.utils.GenericTimeStampedCache: Simple constructor.
GeodeticPoint - Class in org.orekit.bodies: Point location relative to a 2D body surface.
GeodeticPoint(double, double, double) - Constructor for class org.orekit.bodies.GeodeticPoint: Build a new instance.
GeographicZoneDetector - Class in org.orekit.propagation.events: Detector for entry/exit of a zone defined by geographic boundaries.
GeographicZoneDetector(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector: Build a new detector.
GeographicZoneDetector(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector: Build a detector.
Geoid - Class in org.orekit.models.earth: A geoid is a level surface of the gravity potential of a body.
Geoid(NormalizedSphericalHarmonicsProvider, ReferenceEllipsoid) - Constructor for class org.orekit.models.earth.Geoid: Creates a geoid from the given geopotential, reference ellipsoid and the assumptions in the comment for Geoid.
GeoMagneticElements - Class in org.orekit.models.earth: Contains the elements to represent a magnetic field at a single point.
GeoMagneticElements(Vector3D) - Constructor for class org.orekit.models.earth.GeoMagneticElements: Construct a new element with the given field vector.
GeoMagneticField - Class in org.orekit.models.earth: Used to calculate the geomagnetic field at a given geodetic point on earth.
GeoMagneticField(String, double, int, int, double, double) - Constructor for class org.orekit.models.earth.GeoMagneticField: Create a new geomagnetic field model with the given parameters.
GeoMagneticFieldFactory - Class in org.orekit.models.earth: Factory for different GeoMagneticField models.
GeoMagneticFieldFactory.FieldModel - Enum in org.orekit.models.earth: The currently supported geomagnetic field models.
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
get(FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap: Get the entry valid at a specified date.
get(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap: Get the entry valid at a specified date.
get24HoursKp(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation: The Kp index is derived from the Ap index.
get24HoursKp(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters: Get the last 24H mean geomagnetic index.
getA() - Method in class org.orekit.bodies.Ellipse: Get the semi major axis.
getA() - Method in class org.orekit.bodies.Ellipsoid: Get the length of the first semi-axis.
getA() - Method in class org.orekit.files.ccsds.OGMFile: Get the orbit semi-major axis.
getA() - Method in class org.orekit.orbits.CartesianOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.CircularOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.KeplerianOrbit: Get the semi-major axis.
getA() - Method in class org.orekit.orbits.Orbit: Get the semi-major axis.
getA() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the semi-major axis.
getA() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.SpacecraftState: Get the semi-major axis.
getAbscissaGrid() - Method in class org.orekit.utils.InterpolationTableLoader: Returns a copy of the abscissa grid for the interpolation function.
getAbsoluteDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition: Get the transition field absolute date.
getAcceleration() - Method in class org.orekit.frames.FieldTransform: Get the second time derivative of the translation.
getAcceleration() - Method in class org.orekit.frames.Transform: Get the second time derivative of the translation.
getAcceleration() - Method in class org.orekit.utils.FieldPVCoordinates: Gets the acceleration.
getAcceleration() - Method in class org.orekit.utils.PVCoordinates: Gets the acceleration.
getAccuracy() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris: Get the formal accuracy for this satellite.
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.
getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the adapted propagator.
getAdditionalState(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider: Get the additional state.
getAdditionalState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider: Get the additional state.
getAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState: Get an additional state.
getAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState: Get an additional state.
getAdditionalStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper: Compute the length of the one-dimensional additional state array needed.
getAdditionalStateProviders() - Method in class org.orekit.propagation.AbstractPropagator: Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in interface org.orekit.propagation.FieldPropagator: Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in interface org.orekit.propagation.Propagator: Get an unmodifiable list of providers for additional state.
getAdditionalStates() - Method in class org.orekit.propagation.FieldSpacecraftState: Get an unmodifiable map of additional states.
getAdditionalStates() - Method in class org.orekit.propagation.SpacecraftState: Get an unmodifiable map of additional states.
getADot() - Method in class org.orekit.orbits.CartesianOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.CircularOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.Orbit: Get the semi-major axis derivative.
getAe() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the value of the central body reference radius.
getAe() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the central body reference radius.
getAe() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Get the value of the central body reference radius.
getAf0() - Method in class org.orekit.gnss.GPSAlmanac: Gets the Zeroth Order Clock Correction.
getAf1() - Method in class org.orekit.gnss.GPSAlmanac: Gets the First Order Clock Correction.
getAfter() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition: Get the entry valid after transition.
getAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition: Get the entry valid after transition.
getAgency() - Method in class org.orekit.files.sp3.SP3File: Returns the agency that prepared this SP3 file.
getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector: Get the alignment angle (rad).
getAll() - Method in class org.orekit.utils.ImmutableTimeStampedCache: Get all of the data in this cache.
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.
getAlmanacs() - Method in class org.orekit.gnss.SEMParser: Gets all the GPS almanacs read from the file.
getAlmanacs() - Method in class org.orekit.gnss.YUMAParser: Gets all the GPS almanacs read from the file.
getAlpha() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader: Returns the alpha coefficients array.
getAlpha(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit: Get the latitude argument.
getAlpha(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit: Get the latitude argument.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get direction cosine α for central body.
getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit: Get the latitude argument derivative.
getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit: Get the latitude argument derivative.
getAlphaE() - Method in class org.orekit.orbits.CircularOrbit: Get the eccentric latitude argument.
getAlphaE() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the eccentric latitude argument.
getAlphaEDot() - Method in class org.orekit.orbits.CircularOrbit: Get the eccentric latitude argument derivative.
getAlphaEDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the eccentric latitude argument derivative.
getAlphaM() - Method in class org.orekit.orbits.CircularOrbit: Get the mean latitude argument.
getAlphaM() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the mean latitude argument.
getAlphaMDot() - Method in class org.orekit.orbits.CircularOrbit: Get the mean latitude argument derivative.
getAlphaMDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the mean latitude argument derivative.
getAlphaV() - Method in class org.orekit.orbits.CircularOrbit: Get the true latitude argument.
getAlphaV() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the true latitude argument.
getAlphaVDot() - Method in class org.orekit.orbits.CircularOrbit: Get the true latitude argument derivative.
getAlphaVDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the true latitude argument derivative.
getAltitude() - Method in class org.orekit.bodies.FieldGeodeticPoint: Get the altitude.
getAltitude() - Method in class org.orekit.bodies.GeodeticPoint: Get the altitude.
getAltitude() - Method in class org.orekit.propagation.events.AltitudeDetector: Get the threshold altitude value.
getAltitude() - Method in class org.orekit.propagation.events.FieldAltitudeDetector: Get the threshold altitude value.
getAncestor(int) - Method in class org.orekit.frames.Frame: Get the n^th ancestor of the frame.
getAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector: Get the fixed angle to be crossed (radians).
getAngleType() - Method in class org.orekit.files.ccsds.TDMFile.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.
getAngularVelocity() - Method in class org.orekit.utils.FieldPVCoordinates: Get the angular velocity (spin) of this point as seen from the origin.
getAngularVelocity() - Method in class org.orekit.utils.PVCoordinates: Get the angular velocity (spin) of this point as seen from the origin.
getAnomaly() - Method in class org.orekit.files.ccsds.OGMFile: Get the orbit anomaly.
getAnomaly(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the anomaly.
getAnomaly(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit: Get the anomaly.
getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the anomaly derivative.
getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit: Get the anomaly derivative.
getAnomalyType() - Method in class org.orekit.files.ccsds.OGMFile: Get the type of anomaly (true or mean).
getAp(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters: Get the A_p geomagnetic indices.
getArea() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet: Get facet area.
getAstronomicalAmplitudesMap() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader: Get astronomical amplitudes map.
getAtmosphere() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the atmospheric model.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AttitudesSequence: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FixedRate: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.InertialProvider: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.InertialProvider: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffset: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.SpinStabilized: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedProvider: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedProvider: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the attitude corresponding to an orbital state.
getAttitude() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the attitude.
getAttitude() - Method in class org.orekit.propagation.SpacecraftState: Get the attitude.
getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Get the Attitude Provider to use during maneuver.
getAttitudeProvider() - Method in class org.orekit.propagation.AbstractPropagator: Get 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.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
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.OrekitEphemerisFile.OrekitEphemerisSegment
getAvailableDerivatives() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
getAvailableSatelliteNumbers() - Method in class org.orekit.propagation.analytical.tle.TLESeries: Deprecated.

Get the available satellite numbers.
getAverageFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters: Get the value of the 81 day average of F10.7 solar flux centered on current day.
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.
getB() - Method in class org.orekit.bodies.Ellipse: Get the semi minor axis.
getB() - Method in class org.orekit.bodies.Ellipsoid: Get the length of the second semi-axis.
getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get B = sqrt(1 - e²).
getBaseFrame() - Method in class org.orekit.estimation.measurements.GroundStation: Get the base frame associated with the station.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the base system state at given date, without compensation.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation: Compute the base system state at given date, without compensation.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the base system state at given date, without compensation.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering: Compute the base system state at given date, without compensation.
getBaseWeight() - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Get the base weight associated with the measurement
getBaseWeight() - Method in 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.
getBeacon() - Method in class org.orekit.propagation.events.AngularSeparationDetector: Get the beacon at the center of the proximity zone.
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.
getBeta() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader: Returns the beta coefficients array.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get direction cosine β for central body.
getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory: Get a celestial body.
getBody() - Method in class org.orekit.propagation.events.FootprintOverlapDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.GeographicZoneDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeExtremumDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeExtremumDetector: Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Get third body.
getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing: Get the body frame.
getBodyFrame() - Method in interface org.orekit.bodies.BodyShape: Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid: Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.models.earth.Geoid
getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody: Get a body oriented, body centered frame.
getBodyShape() - Method in class org.orekit.propagation.events.AltitudeDetector: Get the body shape.
getBodyShape() - Method in class org.orekit.propagation.events.FieldAltitudeDetector: Get the body shape.
getBStar() - Method in class org.orekit.files.ccsds.OMMFile: Get the SGP/SGP4 drag-like coefficient.
getBStar() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the ballistic coefficient.
getC() - Method in class org.orekit.bodies.Ellipsoid: Get the length of the third semi-axis.
getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get C = 1 + p² + q².
getC2n0(int) - Method in class org.orekit.models.earth.ReferenceEllipsoid: Get the fully normalized coefficient C_2n,0 for the normal gravity potential.
getCacheSlotsNumber() - Static method in class org.orekit.utils.OrekitConfiguration: Get the number of slots to use in caches.
getCalendarWeek() - Method in class org.orekit.time.DateComponents: Get the calendar week number.
getCalls() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the number of calls to the differential equations computation method.
getCalls() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get the number of calls to the differential equations computation method.
getCapitalizedAbbreviation() - Method in enum org.orekit.time.Month: Get the capitalized three letters abbreviation.
getCapitalizedName() - Method in enum org.orekit.time.Month: Get the capitalized full name.
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.
getCCSDSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).
getCelestialBody() - Method in enum org.orekit.files.ccsds.CenterName: Get the celestial body corresponding to the CCSDS constant.
getCenter() - Method in class org.orekit.bodies.Ellipse: Get the center of the 2D ellipse.
getCenter() - Method in class org.orekit.models.earth.tessellation.Tile: Get the center point.
getCenter() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector: Get the direction of FOV center.
getCenterBody() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the CelestialBody corresponding to the center name.
getCenterName() - Method in class org.orekit.files.ccsds.CcsdsModifiedFrame: Get the CCSDS center name.
getCenterName() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the origin of reference frame.
getCenterOfCurvature(Vector2D) - Method in class org.orekit.bodies.Ellipse: Find the center of curvature (point on the evolute) at the nadir of a point.
getChildren() - Method in class org.orekit.frames.OrphanFrame: Get all children of the instance.
getCic() - Method in class org.orekit.gnss.GPSAlmanac
getCic() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements: Gets the Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination.
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) - Static method in class org.orekit.frames.FramesFactory: Get the CIRF2000 reference frame.
getCis() - Method in class org.orekit.gnss.GPSAlmanac
getCis() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements: Gets the Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination.
getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient: Get the C_j coefficient.
getClassification() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the classification.
getClassificationType() - Method in class org.orekit.files.ccsds.OMMFile: Get the classification type.
getClockCorrection() - Method in class org.orekit.files.sp3.SP3File.SP3Coordinate: Returns the clock correction value.
getClockRateChange() - Method in class org.orekit.files.sp3.SP3File.SP3Coordinate: Returns the clock rate.
getClosestTLE(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLESeries: Deprecated.

Get the closest TLE to the selected date.
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 interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms: Computes the coefficients involved in the contributions.
getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms: Get the prefix for short period coefficients keys.
getComment() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the meta-data comment.
getComment() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Get the maneuvers data comment, each string in the list corresponds to one line of comment.
getComment() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Get the meta-data comment.
getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate: Split the instance into date/time components.
getComponents(int) - Method in class org.orekit.time.AbsoluteDate: Split the instance into date/time components for a local time.
getComponents(TimeZone) - Method in class org.orekit.time.AbsoluteDate: Split the instance into date/time components for a time zone.
getComponents(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate: Split the instance into date/time components.
getComponents(int) - Method in class org.orekit.time.FieldAbsoluteDate: Split the instance into date/time components for a local time.
getComponents(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate: Split the instance into date/time components for a time zone.
getConstantNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the constant gravity field coefficients provider from the first supported file.
getConstantProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get a time-independent provider for read spherical harmonics coefficients.
getConstantUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory: Get the constant gravity field coefficients provider from the first supported file.
getConventions() - Method in class org.orekit.files.ccsds.ODMFile: Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.ODMParser: Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.TDMParser: Get IERS conventions.
getConventions() - Method in class org.orekit.frames.EOPHistory: Get the IERS conventions to which these EOP apply.
getCoordinates(SpacecraftState, int, DSFactory) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement: Get Cartesian coordinates as derivatives.
getCoordinates() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
getCoordinates() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment: Get the coordinates for this ephemeris segment.
getCoordinates() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
getCoordinates() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3File: Returns the coordinate system of the entries in this orbit file.
getCorrectionAngle1() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Getter for the correctionAngle1.
getCorrectionAngle2() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Getter for the correctionAngle2.
getCorrectionDoppler() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Getter for the correctionDoppler.
getCorrectionRange() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Getter for the correctionRange.
getCorrectionReceive() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Getter for the correctionReceive.
getCorrectionsApplied() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Getter for the correctionApplied.
getCorrectionTransmit() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Getter for the correctionTransmit.
getCount() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the evaluations counter.
getCovarianceComment() - Method in class org.orekit.files.ccsds.OGMFile: Get the comment for covariance.
getCovarianceMatrices() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get the list of Covariance Matrices.
getCovarianceMatrix() - Method in class org.orekit.files.ccsds.OGMFile: Get the Position/Velocity covariance matrix.
getCovRefFrame() - Method in class org.orekit.files.ccsds.OGMFile: Get coordinate system for covariance matrix, for absolute frames.
getCovRefLofType() - Method in class org.orekit.files.ccsds.OGMFile: Get coordinate system for covariance matrix, for Local Orbital Frames.
getCrc() - Method in class org.orekit.gnss.GPSAlmanac
getCrc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements: Gets the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius.
getCreationDate() - Method in class org.orekit.files.ccsds.ODMFile: Get the file creation date and time in UTC.
getCreationDate() - Method in class org.orekit.files.ccsds.TDMFile: Get the file creation date and time in UTC.
getCrs() - Method in class org.orekit.gnss.GPSAlmanac
getCrs() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements: Gets the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius.
getCuc() - Method in class org.orekit.gnss.GPSAlmanac
getCuc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements: Gets the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude.
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.
getCurrentWeight() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the current weight.
getCus() - Method in class org.orekit.gnss.GPSAlmanac
getCus() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements: Gets the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude.
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 interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters: Get the value of the daily F10.7 solar flux for previous day.
getDataQuality() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Getter for the dataQuality.
getDataUsed() - Method in class org.orekit.files.sp3.SP3File: Returns the data used indicator from the SP3 file.
getDate() - Method in class org.orekit.attitudes.Attitude: Get the date of attitude parameters.
getDate() - Method in class org.orekit.attitudes.FieldAttitude: Get the date of attitude parameters.
getDate() - Method in class org.orekit.data.DelaunayArguments: Get the date.
getDate() - Method in class org.orekit.data.FieldDelaunayArguments: Get the date.
getDate() - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Get the date.
getDate() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the date.
getDate() - Method in class org.orekit.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.gnss.GPSAlmanac
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.tle.TLE: Get the TLE current date.
getDate() - Method in class org.orekit.propagation.events.DateDetector: Get the current event date according to the propagator.
getDate() - Method in class org.orekit.propagation.events.FieldDateDetector: Get the current event date according to the propagator.
getDate() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the date.
getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the date of the orbit.
getDate() - Method in class org.orekit.propagation.SpacecraftState: Get the date.
getDate() - Method in class org.orekit.time.AbsoluteDate: Get the date.
getDate() - Method in class org.orekit.time.DateTimeComponents: Get the date component.
getDate() - Method in class org.orekit.time.FieldAbsoluteDate: Get the date.
getDate() - Method in interface org.orekit.time.FieldTimeStamped: Get the date.
getDate() - Method in interface org.orekit.time.TimeStamped: Get the 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.
getDay() - Method in class org.orekit.time.DateComponents: Get the day.
getDayFraction() - Method in class org.orekit.files.sp3.SP3File: Returns the day fraction for this SP3 file.
getDayOfWeek() - Method in class org.orekit.time.DateComponents: Get the day of week.
getDayOfYear() - Method in class org.orekit.time.DateComponents: Get the day number in year.
getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient: Get the dC_j / dh coefficient.
getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient: Get the dC_j / dk coefficient.
getDdEps() - Method in class org.orekit.frames.EOPEntry: Get the correction for nutation in obliquity δΔε.
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 degrees.
getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter: Get the decreasing events time shift.
getDefaultModel() - Static method in class org.orekit.models.earth.FixedTroposphericDelay: Returns the default model, loading delay values from the file "tropospheric-delay.txt".
getDelaunayMultipliers() - Method in class org.orekit.models.earth.displacement.Tide: Get the multipliers for Delaunay arguments (l, l', F, D, Ω).
getDeltaMass() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Get mass change during maneuver (value is < 0).
getDeltaVSat() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Get the velocity increment in satellite frame.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere: Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere: Get the local density.
getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.DTM2000: Get the local density with initial entries.
getDensity(int, T, T, T, T, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.DTM2000: Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.DTM2000: Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.DTM2000: Get the local density.
getDensity(Vector3D, Vector3D) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester: Get the local density.
getDensity(Vector3D, FieldVector3D<T>) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester: Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester: Get the local density at some position.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester: Get the local density at some position.
getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.JB2008: Get the local density with initial entries.
getDensity(T, T, T, T, T, T, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.JB2008: Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.JB2008: Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.JB2008: Get the local density.
getDensity(int) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00.FieldOutput: Get one of the stored densities.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00: Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00: Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere: Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere
getDepth() - Method in class org.orekit.frames.Frame: Get the depth of the frame.
getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction: Get Γ function derivative.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear: Compute the value of the derivative dK_j^{-n-1, s} / de².
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear: Compute the value of the Hansen coefficient dK₀^{n, s} / dΧ.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear: Get the dK₀^-n-1,s / dΧ coefficient derivative.
getDerivativesDrivers() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get all the drivers with set derivatives.
getDetector() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event: Get the detector.
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.GHIJjsPolynomials: Get the dG_js / dβ 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.GHIJjsPolynomials: Get the dG_js / dk 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.GHmsjPolynomials: Get the dG_ms^j / d_β 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.GHmsjPolynomials: Get the dG_ms^j / d_k 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.GHIJjsPolynomials: Get the dH_js / dβ 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.GHIJjsPolynomials: Get the dH_js / dk 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.GHmsjPolynomials: Get the dH_ms^j / d_β 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.GHmsjPolynomials: Get the dH_ms^j / d_k 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.GHIJjsPolynomials: Get the dI_js / dβ 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.GHIJjsPolynomials: Get the dI_js / dk coefficient.
getDimension() - Method in class org.orekit.estimation.measurements.AbstractMeasurement: Get the dimension of the measurement.
getDimension() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement: Get the dimension of the measurement.
getDisplacements() - Method in class org.orekit.estimation.measurements.GroundStation: Get the displacement models.
getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the dJ_js / dα 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.GHIJjsPolynomials: Get the dJ_js / dh 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.LnsCoefficients: Get the value of dL_n^s / dγ (γ).
getDnl(double, double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds: Get the upper bound value D_n^l(Χ).
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.
getDragArea() - Method in class org.orekit.files.ccsds.OGMFile: Get the drag area.
getDragCoeff() - Method in class org.orekit.files.ccsds.OGMFile: Get the drag coefficient.
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.
getDrivers(double, Orbit, PositionAngle) - Method in enum org.orekit.orbits.OrbitType: Get parameters drivers initialized from a reference orbit.
getDrivers() - Method in class org.orekit.utils.ParameterDriversList: Get delegating drivers for all parameters.
getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient: Get the dS_j / dh coefficient.
getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient: Get the dS_j / dk coefficient.
getDSTDTC(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters: Get the temperature change computed from Dst index.
getDuration() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Get duration (value is 0 for impulsive maneuver).
getDV() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Get velocity increment.
getDx() - Method in class org.orekit.frames.EOPEntry: Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getDy() - Method in class org.orekit.frames.EOPEntry: Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getE() - Method in class org.orekit.files.ccsds.OGMFile: Get the orbit eccentricity.
getE() - Method in class org.orekit.gnss.GPSAlmanac
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 interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements: Gets the Eccentricity.
getE() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the eccentricity.
getE() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the eccentricity.
getE() - Method in class org.orekit.propagation.SpacecraftState: Get the eccentricity.
getEarliest() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the earliest cached entry.
getEarliest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
getEarliest() - Method in interface org.orekit.utils.TimeStampedCache: Get the earliest entry in this cache.
getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Earth singleton body.
getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Earth-Moon barycenter singleton bodies pair.
getEarthOrientationAngleFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions: Get the function computing the raw Earth Orientation Angle.
getEast() - Method in class org.orekit.bodies.FieldGeodeticPoint: Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.bodies.GeodeticPoint: Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.frames.TopocentricFrame: Get the east direction of topocentric frame, expressed in parent shape frame.
getEastOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation: Get a driver allowing to change station position along East axis.
getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the eccentricity.
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.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator: Gets the Earth Centered Earth Fixed frame used to propagate GPS orbits according to the GPS Interface Specification.
getECI() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator: Gets the Earth Centered Inertial frame used to propagate the orbit.
getEcliptic(IERSConventions) - Static method in class org.orekit.frames.FramesFactory: Get the ecliptic frame.
getEDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.CircularOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.Orbit: Get the eccentricity derivative.
getEffects() - Method in class org.orekit.propagation.analytical.AdapterPropagator: Get the differential effects.
getElem(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix: Get the value of an element.
getElementNumber() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the element number.
getElementSetNumber() - Method in class org.orekit.files.ccsds.OMMFile: Get the element set number for this satellite.
getElevation(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame: Get the elevation of a point with regards to the local point.
getElevation(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector: Get the elevation value.
getElevation(double) - Method in class org.orekit.utils.ElevationMask: Get the interpolated elevation for a given azimuth according to the mask.
getElevationMask() - Method in class org.orekit.gnss.DOPComputer: Get the elevation mask.
getElevationMask() - Method in class org.orekit.propagation.events.ElevationDetector: Returns the currently configured elevation mask.
getElevationMask() - Method in class org.orekit.propagation.events.FieldElevationDetector: Returns the currently configured elevation mask.
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() - Static method in class org.orekit.frames.FramesFactory: Get the unique EME2000 frame.
getEndDate() - Method in class org.orekit.frames.EOPHistory: Get the date of the last available Earth Orientation Parameters.
getEntries() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the total number of entries cached.
getEOPHistory() - Method in interface org.orekit.frames.EOPBasedTransformProvider: Get the EOP history.
getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get Earth Orientation Parameters history.
getEOPHistory() - Method in class org.orekit.frames.GTODProvider: Get the EOP history.
getEOPHistory() - Method in class org.orekit.time.UT1Scale: Get the EOP history.
getEOPTidalCorrection() - Method in enum org.orekit.utils.IERSConventions: Get the function computing tidal corrections for Earth Orientation Parameters.
getEphemeridesBlocks() - Method in class org.orekit.files.ccsds.OEMFile: Get the list of ephemerides blocks as an unmodifiable list.
getEphemeridesDataLinesComment() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get the ephemerides data lines comment.
getEphemerisType() - Method in class org.orekit.files.ccsds.OMMFile: Get the ephemeris type.
getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the type of ephemeris.
getEpoch() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix: Get the epoch relative to the covariance matrix.
getEpoch() - Method in class org.orekit.files.ccsds.OGMFile: Get epoch of state vector, Keplerian elements and covariance matrix data.
getEpoch() - Method in class org.orekit.files.ccsds.TDMFile.Observation: Getter for the epoch.
getEpoch() - Method in class org.orekit.files.sp3.SP3File: 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.
getEpochComment() - Method in class org.orekit.files.ccsds.OGMFile: Get the comment for epoch.
getEpochIgnition() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver: Get epoch ignition.
getEpochInterval() - Method in class org.orekit.files.sp3.SP3File: Returns the time interval between epochs (in seconds).
getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the equatorial radius of the 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 derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.KeplerianOrbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.Orbit: Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEx() - Method in class org.orekit.propagation.SpacecraftState: Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialExDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.Orbit: Get the first component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.KeplerianOrbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.Orbit: Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the second component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEy() - Method in class org.orekit.propagation.SpacecraftState: Get the second component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEyDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.Orbit: Get the second component of the equinoctial eccentricity vector.
getEquinoxNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the correction to the nutation parameters for equinox-based paradigm.
getEquinoxNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory: Get the correction to the nutation parameters for equinox-based paradigm.
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.
getEstimatedUT1() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider: Get the estimated UT1 time scale.
getEstimatedUT1() - Method in class org.orekit.estimation.measurements.GroundStation: Get the estimated UT1 scale, including the estimated linear models for prime meridian.
getEstimatedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the estimated value.
getEvaluations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the number of objective function evaluations.
getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Get the number of evaluations used for last estimation.
getEventDate() - Method in class org.orekit.propagation.events.EventState: Get the occurrence time of the event triggered in the current step.
getEventDate() - Method in class org.orekit.propagation.events.FieldEventState: Get the occurrence time of the event triggered in the current step.
getEventDetector() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent: Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.EventState: Get the underlying event detector.
getEventDetector() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent: Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.FieldEventState: Get the underlying event detector.
getEvents() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue: Get the events passed to this handler.
getEventsDetectors() - Method in class org.orekit.forces.AbstractParametricAcceleration: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.drag.DragForce: Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.forces.ForceModel: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.NewtonianAttraction: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.OceanTides: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.Relativity: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.SolidTides: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in interface org.orekit.propagation.Propagator: Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal: Get the discrete events related to the model.
getException() - Method in exception org.orekit.errors.OrekitExceptionWrapper: Get the wrapped exception.
getExtrapolationThreshold() - Method in class org.orekit.propagation.analytical.Ephemeris: Get the maximum timespan outside of the stored ephemeris that is allowed for extrapolation.
getF() - Method in class org.orekit.data.DelaunayArguments: Get L - Ω where L is the mean longitude of the Moon.
getF() - Method in class org.orekit.data.FieldDelaunayArguments: Get L - Ω where L is the mean longitude of the Moon.
getF10(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters: Get the value of the instantaneous solar flux index (1e^-22*Watt/(m²*Hertz)).
getF10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.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.
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(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory: Get the GeoMagneticField for the given model type and year.
getField() - Method in class org.orekit.propagation.FieldAbstractPropagator: Field getter.
getField() - Method in class org.orekit.time.FieldAbsoluteDate: Get the field.
getFieldDate() - Method in class org.orekit.frames.FieldTransform: Get the date.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.AbstractParametricAcceleration: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.drag.DragForce: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.forces.ForceModel: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.OceanTides: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.Relativity: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SolidTides: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get the discrete events related to the model.
getFieldOfView() - Method in class org.orekit.propagation.events.FieldOfViewDetector: Get the Field Of View.
getFieldOfView() - Method in class org.orekit.propagation.events.FootprintOverlapDetector: Get the Field Of View.
getFieldOfView() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector: Get the Field Of View.
getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements: Returns the magnetic field vector in nTesla.
getFiftiesEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
getFileDate(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation: Get the date of the file from which data at the specified date comes from.
getFileFormat() - Method in class org.orekit.files.ccsds.TDMParser: Get file format.
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.
getFirst() - Method in class org.orekit.propagation.analytical.tle.TLESeries: Deprecated.

Get the first TLE.
getFirstDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries: Deprecated.

Get the start date of the series.
getFirstKnownLeapSecond() - Method in class org.orekit.time.UTCScale: Get the date of the first known leap second.
getFittedParameters() - Method in class org.orekit.utils.SecularAndHarmonic: Get a copy of the last fitted parameters.
getFixedStepSize() - Method in class org.orekit.propagation.AbstractPropagator: Get the fixed step size.
getFixedStepSize() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get the fixed step size.
getFlattening() - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the flattening of the body: f = (a-b)/a.
getFlowRate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the flow rate.
getForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Deprecated.
as of 9.1, this method is deprecated, the perturbing force models are retrieved together with the Newtonian attraction by calling FieldNumericalPropagator.getAllForceModels()
getFormatVersion() - Method in class org.orekit.files.ccsds.ODMFile: Get the CCSDS ODM (OPM, OMM or OEM) format version.
getFormatVersion() - Method in class org.orekit.files.ccsds.TDMFile: Get the CCSDS TDM format version.
getFrame() - Method in class org.orekit.bodies.Ellipse: Get the defining frame.
getFrame() - Method in class org.orekit.bodies.Ellipsoid: Get the ellipsoid central frame.
getFrame(IERSConventions, boolean) - Method in enum org.orekit.files.ccsds.CCSDSFrame: Get the frame corresponding to the CCSDS constant.
getFrame() - Method in class org.orekit.files.ccsds.ODMMetaData: 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.OEMFile.CovarianceMatrix: Get coordinate system for covariance matrix, for absolute frames.
getFrame() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
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
getFrame() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
getFrame() - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere: Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.DTM2000: Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester: Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.JB2008: Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00: Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere: Get the frame of the central body.
getFrame(Predefined) - Static method in class org.orekit.frames.FramesFactory: Get one of the predefined frames.
getFrame() - Method in class org.orekit.frames.OrphanFrame: Get the associated frame.
getFrame() - Method in class org.orekit.orbits.FieldOrbit: Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.orbits.Orbit: Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.propagation.AbstractPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.Ephemeris
getFrame() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter: Get the frame of the initial state.
getFrame() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.events.FieldNodeDetector: Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector: Get the sensor reference frame.
getFrame() - Method in class org.orekit.propagation.events.NodeDetector: Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in interface org.orekit.propagation.FieldPropagator: Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the inertial 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.SpacecraftState: Get the inertial frame.
getFrameCenterString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
getFrameCenterString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment: Get the name of the center of the coordinate system the ephemeris is provided in.
getFrameCenterString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
getFrameCenterString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
getFrameEpoch() - Method in class org.orekit.files.ccsds.ODMMetaData: Get epoch of reference frame, if not intrinsic to the definition of the reference frame.
getFrameEpochString() - Method in class org.orekit.files.ccsds.ODMMetaData: Get epoch of reference frame, if not intrinsic to the definition of the reference frame.
getFrameString() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the reference frame specifier as it appeared in the file.
getFrameString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
getFrameString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment: Get the defining frame for this ephemeris segment.
getFrameString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
getFrameString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
getFreqOffset() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Getter for the freqOffset.
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.
getFutureInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Dummy date at infinity in the future direction.
getGalileoEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
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.utilities.AuxiliaryElements: Get direction cosine γ for central body.
getGammaDot() - Method in class org.orekit.data.DelaunayArguments: Get the tide parameter γ = GMST + π time derivative.
getGammaDot() - Method in class org.orekit.data.FieldDelaunayArguments: Get the tide parameter γ = GMST + π time derivative.
getGASTFunction(TimeScale, EOPHistory) - Method in enum org.orekit.utils.IERSConventions: Get the function computing Greenwich apparent sidereal time, in radians.
getGCRF() - Static method in class org.orekit.frames.FramesFactory: Get the unique GCRF frame.
getGdop() - Method in class org.orekit.gnss.DOP: Gets the geometric dilution of precision.
getGenerateCalls() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the number of calls to the generate method.
getGeneratedEphemeris() - Method in class org.orekit.propagation.AbstractPropagator: Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.FieldPropagator: Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.Propagator: Get the ephemeris generated during propagation.
getGenerator() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the generator.
getGetNeighborsCalls() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the number of calls to the GenericTimeStampedCache.getNeighbors(AbsoluteDate) method.
getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the G_js coefficient.
getGLONASS() - Static method in class org.orekit.time.TimeScalesFactory: Get the GLObal NAvigation Satellite System time scale.
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.
getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials: Get the G_ms^j coefficient.
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.
getGMSTRateFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions: Get the function computing Greenwich mean sidereal time rate, in radians per second.
getGnssNb() - Method in class org.orekit.gnss.DOP: Gets the number of GNSS satellites taken into account for DOP computation.
getGPS() - Static method in class org.orekit.time.TimeScalesFactory: Get the Global Positioning System scale.
getGPSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
getGPSOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator: Gets the underlying GPS orbital elements.
getGpsWeek() - Method in class org.orekit.files.sp3.SP3File: Returns the GPS week as contained in the SP3 file.
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.
getGrs80(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid: Get the GRS80 ellipsoid, attached to the given body frame.
getGST() - Static method in class org.orekit.time.TimeScalesFactory: Get the Galileo System Time scale.
getGTOD(boolean) - Static method in class org.orekit.frames.FramesFactory: Get the GTOD reference frame.
getGTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the GTOD reference frame.
getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the y component of eccentricity vector.
getHalfAperture() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector: Get FOV half aperture angle.
getHandler() - Method in class org.orekit.propagation.events.AbstractDetector: Get the handler.
getHandler() - Method in class org.orekit.propagation.events.FieldAbstractDetector: Get the handler.
getHarmonicAmplitude() - Method in class org.orekit.utils.SecularAndHarmonic: Get an upper bound of the fitted harmonic amplitude.
getHasCreatableBody() - Method in class org.orekit.files.ccsds.ODMMetaData: Get boolean testing whether the body corresponding to the centerName attribute can be created through the CelestialBodyFactory.
getHasManeuver() - Method in class org.orekit.files.ccsds.OPMFile: Get boolean testing whether the OPM contains at least one maneuver.
getHasRefFrameEpoch() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get boolean testing whether the reference frame has an epoch associated to it.
getHdop() - Method in class org.orekit.gnss.DOP: Gets the horizontal dilution of precision.
getHeaderComment() - Method in class org.orekit.files.ccsds.ODMFile: Get the header comment.
getHeaderComment() - Method in class org.orekit.files.ccsds.TDMFile: Get the header comment.
getHealth() - Method in class org.orekit.gnss.GPSAlmanac: Gets the Health status.
getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the H_js 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).
getHour() - Method in class org.orekit.time.TimeComponents: Get the hour number.
getHx() - Method in class org.orekit.orbits.CartesianOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.KeplerianOrbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.Orbit: Get the first component of the inclination vector.
getHx() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the first component of the inclination vector (as per equinoctial parameters).
getHx() - Method in class org.orekit.propagation.SpacecraftState: Get the first component of the inclination vector (as per equinoctial parameters).
getHxDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.CircularOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.Orbit: Get the first component of the inclination vector derivative.
getHy() - Method in class org.orekit.orbits.CartesianOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.KeplerianOrbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.Orbit: Get the second component of the inclination vector.
getHy() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the second component of the inclination vector (as per equinoctial parameters).
getHy() - Method in class org.orekit.propagation.SpacecraftState: Get the second component of the inclination vector (as per equinoctial parameters).
getHyDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.CircularOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.Orbit: Get the second component of the inclination vector derivative.
getI() - Method in class org.orekit.files.ccsds.OGMFile: 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.TLE: Get the inclination.
getI() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the inclination.
getI() - Method in class org.orekit.propagation.SpacecraftState: Get the inclination.
getI0() - Method in class org.orekit.gnss.GPSAlmanac
getI0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements: Gets the Inclination Angle at Reference Time.
getICRF() - Static method in class org.orekit.frames.FramesFactory: Get the unique ICRF frame.
getId() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris
getId() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris: Get the satellite ID.
getId() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
getId() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
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.GPSAlmanac
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 interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements: Gets the Rate of Inclination Angle.
getIGRF(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory: Get the IGRF model for the given year.
getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the I_js coefficient.
getImaginary(int, int) - Method in class org.orekit.utils.LoveNumbers: Get the imaginary part of a nominal Love numbers.
getInclination() - Method in class org.orekit.models.earth.GeoMagneticElements: Returns the inclination of the magnetic field in degrees.
getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter: Get the increasing events time shift.
getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Get the inertial velocity increment of the maneuver.
getInertialFrame() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Get the inertial frame in which the velocity increment is defined.
getInertiallyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody: Get an inertially oriented, body centered frame.
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.
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.
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.
getInstance() - Static method in class org.orekit.data.DataProvidersManager: Get the unique instance.
getInstantFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation: Get the value of the instantaneous solar flux.
getInstantFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters: Get the value of the instantaneous solar flux.
getIntegrationInterval() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Getter for the integrationInterval.
getIntegrationRef() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData: Getter for the integrationRef.
getIntegrator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the integrator used by the propagator.
getIntegrator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get the integrator used by the propagator.
getInterpolatedPoint(double, double) - Method in class org.orekit.models.earth.tessellation.Tile: Get an interpolated point inside the tile.
getInterpolatedState(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator: Get the state at interpolated date.
getInterpolatedState(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator: Get the state at interpolated date.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get the interpolation degree.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get the interpolation method to be used.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
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.OrekitEphemerisFile.OrekitEphemerisSegment
getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape: Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape: Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid: Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid: Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid: Get the intersection point of a line with the surface of the body.
getInverse() - Method in class org.orekit.frames.FieldTransform: Get the inverse transform of the instance.
getInverse() - Method in class org.orekit.frames.Transform: Get the inverse transform of the instance.
getISP() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver: Get the specific impulse.
getIsp() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver: Get the specific impulse.
getIteration() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement: Get the iteration number.
getIterationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Get the number of iterations used for last estimation.
getITRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the ITRF2008 reference frame, using IERS 2010 conventions.
getITRFEquinox(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory: Get the equinox-based ITRF reference frame.
getJ2000Day() - Method in class org.orekit.time.DateComponents: Get the day number with respect to J2000 epoch.
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, PositionAngle, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel: Compute the Jacobian of the orbit with respect to maneuver parameters.
getJacobian(CartesianDerivativesFilter, T[][]) - Method in class org.orekit.frames.FieldTransform: Compute the Jacobian of the FieldTransform.transformPVCoordinates(FieldPVCoordinates) method of the transform.
getJacobian(CartesianDerivativesFilter, double[][]) - Method in class org.orekit.frames.Transform: Compute the Jacobian of the Transform.transformPVCoordinates(PVCoordinates) method of the transform.
getJacobianWrtCartesian(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit: Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit: Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtParameters(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit: Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJacobianWrtParameters(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit: Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJavaEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials: Get the J_js coefficient.
getJulianDay() - Method in class org.orekit.files.sp3.SP3File: Returns the julian day for this SP3 file.
getJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate: Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Jupiter singleton body.
getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the x component of eccentricity vector.
getKeplerianElementsComment() - Method in class org.orekit.files.ccsds.OGMFile: Get the comment for Keplerian elements.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.FieldOrbit: Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.Orbit: Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.SpacecraftState: Get the Keplerian mean motion.
getKeplerianPeriod() - Method in class org.orekit.orbits.FieldOrbit: Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.orbits.Orbit: Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.SpacecraftState: Get the Keplerian period.
getKeyword() - Method in class org.orekit.files.ccsds.TDMFile.Observation: Getter for the keyword.
getL() - Method in class org.orekit.data.DelaunayArguments: Get the mean anomaly of the Moon.
getL() - Method in class org.orekit.data.FieldDelaunayArguments: Get the mean anomaly of the Moon.
getL(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit: Get the longitude argument.
getL(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the longitude argument.
getLast() - Method in class org.orekit.propagation.analytical.tle.TLESeries: Deprecated.

Get the last TLE.
getLastDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries: Deprecated.

Get the last date of the series.
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.
getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the latest cached entry.
getLatest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
getLatest() - Method in interface org.orekit.utils.TimeStampedCache: Get the latest entry in this cache.
getLatitude() - Method in class org.orekit.bodies.FieldGeodeticPoint: Get the latitude.
getLatitude() - Method in class org.orekit.bodies.GeodeticPoint: Get the latitude.
getLatitude() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector: Get the fixed latitude to be crossed (radians).
getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the launch number.
getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMParser: Get the launch number.
getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the launch number.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMParser: Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the launch piece.
getLaunchYear() - Method in class org.orekit.files.ccsds.ODMMetaData: Get the launch year.
getLaunchYear() - Method in class org.orekit.files.ccsds.ODMParser: Get the launch year.
getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the launch year.
getLDot() - Method in class org.orekit.data.DelaunayArguments: Get the mean anomaly of the Moon time derivative.
getLDot() - Method in class org.orekit.data.FieldDelaunayArguments: Get the mean anomaly of the Moon time derivative.
getLDot(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit: Get the longitude argument derivative.
getLDot(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the longitude argument derivative.
getLE() - Method in class org.orekit.data.BodiesElements: Get the mean Earth longitude.
getLE() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Earth longitude.
getLE() - Method in class org.orekit.orbits.CartesianOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.CircularOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.KeplerianOrbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.Orbit: Get the eccentric longitude argument.
getLE() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the eccentric latitude argument (as per equinoctial parameters).
getLE() - Method in class org.orekit.propagation.SpacecraftState: Get the eccentric latitude argument (as per equinoctial parameters).
getLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale: Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale: Get the value of the previous leap.
getLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale: Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale: Get the value of the previous leap.
getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale: Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale: Get the value of the previous leap.
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.
getLf() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the eccentric longitude.
getLightingRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get the lighting ratio ([0-1]).
getLightingRatio(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure: Get the lighting ratio ([0-1]).
getLine1() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the first line.
getLine2() - Method in class org.orekit.propagation.analytical.tle.TLE: Get the second line.
getLJu() - Method in class org.orekit.data.BodiesElements: Get the mean Jupiter longitude.
getLJu() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Jupiter longitude.
getLJuDot() - Method in class org.orekit.data.BodiesElements: Get the mean Jupiter longitude time derivative.
getLJuDot() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Jupiter longitude time derivative.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag: Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure: Compute the limits in L, the true longitude, for integration.
getLM() - Method in class org.orekit.orbits.CartesianOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.CircularOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.KeplerianOrbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.Orbit: Get the mean longitude argument.
getLM() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the mean latitude argument (as per equinoctial parameters).
getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the mean longitude.
getLM() - Method in class org.orekit.propagation.SpacecraftState: Get the mean latitude argument (as per equinoctial parameters).
getLMa() - Method in class org.orekit.data.BodiesElements: Get the mean Mars longitude.
getLMa() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Mars longitude.
getLMaDot() - Method in class org.orekit.data.BodiesElements: Get the mean Mars longitude time derivative.
getLMaDot() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Mars longitude time derivative.
getLMDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.CircularOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.Orbit: Get the mean longitude argument derivative.
getLMe() - Method in class org.orekit.data.BodiesElements: Get the mean Mercury longitude.
getLMe() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Mercury longitude.
getLMeDot() - Method in class org.orekit.data.BodiesElements: Get the mean Mercury longitude time derivative.
getLMeDot() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Mercury longitude time derivative.
getLNe() - Method in class org.orekit.data.BodiesElements: Get the mean Neptune longitude.
getLNe() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Neptune longitude.
getLNeDot() - Method in class org.orekit.data.BodiesElements: Get the mean Neptune longitude time derivative.
getLNeDot() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Neptune longitude time derivative.
getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients: Get the value of L_n^s(γ).
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.OrekitParseException
getLocalizedString(Locale) - Method in enum org.orekit.errors.OrekitMessages
getLocation() - Method in class org.orekit.gnss.DOP: Gets the location with respect to the Earth where DOP was calculated.
getLOD() - Method in class org.orekit.frames.EOPEntry: Get the LoD (Length of Day) value.
getLOD(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory: Get the LoD (Length of Day) value.
getLOD(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory: Get the LoD (Length of Day) value.
getLofType() - Method in enum org.orekit.files.ccsds.CCSDSFrame: Get the type of Local Orbital frame.
getLofType() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix: Get coordinate system for covariance matrix, for Local Orbital Frames.
getLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger: Get an immutable copy of the logged events.
getLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger: Get an immutable copy of the logged events.
getLongitude() - Method in class org.orekit.bodies.FieldGeodeticPoint: Get the longitude.
getLongitude() - Method in class org.orekit.bodies.GeodeticPoint: Get the longitude.
getLongitude() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector: Get the fixed longitude to be crossed (radians).
getLoveNumbers() - Method in enum org.orekit.utils.IERSConventions: Get the Love numbers.
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.
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.
getLUr() - Method in class org.orekit.data.BodiesElements: Get the mean Uranus longitude.
getLUr() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Uranus longitude.
getLUrDot() - Method in class org.orekit.data.BodiesElements: Get the mean Uranus longitude time derivative.
getLUrDot() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Uranus longitude time derivative.
getLv() - Method in class org.orekit.orbits.CartesianOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.CircularOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.KeplerianOrbit: Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.Orbit: Get the true longitude argument.
getLv() - Method in class org.orekit.propagation.FieldSpacecraftState: Get the true latitude argument (as per equinoctial parameters).
getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements: Get the true longitude.
getLv() - Method in class org.orekit.propagation.SpacecraftState: Get the true latitude argument (as per equinoctial parameters).
getLvDot() - Method in class org.orekit.orbits.CartesianOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.CircularOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.EquinoctialOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldCartesianOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldCircularOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.Orbit: Get the true longitude argument derivative.
getLVe() - Method in class org.orekit.data.BodiesElements: Get the mean Venus longitude.
getLVe() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Venus longitude.
getLVeDot() - Method in class org.orekit.data.BodiesElements: Get the mean Venus longitude time derivative.
getLVeDot() - Method in class org.orekit.data.FieldBodiesElements: Get the mean Venus longitude time derivative.
getM0() - Method in class org.orekit.gnss.GPSAlmanac
getM0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements: Gets the Mean Anomaly at Reference Time.
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator: Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.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).
getManagedAdditionalStates() - Method in class org.orekit.propagation.AbstractPropagator: Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.analytical.Ephemeris: Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.FieldAbstractPropagator: Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.FieldPropagator: Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator: Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator: Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.Propagator: Get all the names of all managed states.
getManeuver(int) - Method in class org.orekit.files.ccsds.OPMFile: Get a maneuver.
getManeuvers() - Method in class org.orekit.files.ccsds.OPMFile: Get a list of all maneuvers.
getMapper() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations: Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMargin() - Method in class org.orekit.propagation.events.FieldOfView: Get the angular margin to apply (radians).
getMargin() - Method in class org.orekit.propagation.events.GeographicZoneDetector: Get the angular margin to apply (radians).
getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Mars singleton body.
getMass() - Method in class org.orekit.files.ccsds.OGMFile: Get the spacecraft mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris: Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator: Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator: Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator: 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() - Method in class org.orekit.propagation.FieldSpacecraftState: Gets the current mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Get the mass.
getMass() - Method in class org.orekit.propagation.SpacecraftState: Gets the current mass.
getMasterStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange: Get the master ground station from which measurement is performed.
getMatrix() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix: Get the covariance matrix.
getMatrixLine(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix: Get a line of the matrix.
getMaxAlt() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester: Get the maximal altitude for the model.
getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the maximal degree available in the last file parsed.
getMaxAvailableOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the maximal order available in the last file parsed.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.AbstractDetector: Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.EventDetector: Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.FieldAbstractDetector: Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.FieldEventDetector: Get maximal time interval between switching function checks.
getMaxChunksDuration() - Method in class org.orekit.bodies.JPLEphemeridesLoader: Get the maximal chunks duration.
getMaxDate() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation: Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters: Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters: Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters: Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
getMaxDate() - Method in class org.orekit.propagation.analytical.Ephemeris: Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator: Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator: Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris: Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris: Get the last date of the range.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the maximal supported degree.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave: Get the maximum supported degree.
getMaxDegree() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Get the maximal supported degree.
getMaxIterationCount() - Method in class org.orekit.propagation.events.AbstractDetector: Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.EventDetector: Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.FieldAbstractDetector: Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.FieldEventDetector: Get maximal number of iterations in the event time search.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider: Get the maximal supported order.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave: Get the maximum supported order.
getMaxOrder() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider: Get the maximal supported order.
getMaxOrder() - Method in enum org.orekit.utils.AngularDerivativesFilter: Get the maximum derivation order.
getMaxOrder() - Method in enum org.orekit.utils.CartesianDerivativesFilter: Get the maximum derivation order.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Get the degree limit for the next file parsing.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the degree limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader: Get the order limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader: Get the order limit for the next file parsing.
getMaxSlots() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the maximum number of independent cached time slots.
getMaxSpan() - Method in class org.orekit.utils.GenericTimeStampedCache: Get the maximum duration span in seconds of one slot.
getMaxValue() - Method in class org.orekit.utils.ParameterDriver: Get maximum parameter value.
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.TLE: Get the mean anomaly.
getMeanAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit: Get the mean anomaly derivative.
getMeanAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit: Get the mean anomaly derivative.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody: Computes the mean equinoctial elements rates da_i / dt.
getMeanElementRate(SpacecraftState) - 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.OMMFile.OMMMetaData: Get the description of the Mean Element Theory.
getMeanFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation: Get the value of the mean solar flux.
getMeanFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters: Get the value of the mean solar flux.
getMeanMotion() - Method in class org.orekit.files.ccsds.OMMFile: Get the orbit mean motion.
getMeanMotion() - Method in class org.orekit.gnss.GPSAlmanac
getMeanMotion() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements: Gets 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.utilities.AuxiliaryElements: Get the Keplerian mean motion.
getMeanMotionDot() - Method in class org.orekit.files.ccsds.OMMFile: Get the first time derivative of the mean motion.
getMeanMotionDotDot() - Method in class org.orekit.files.ccsds.OMMFile: Get the second time derivative of the mean motion.
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.TLE: Get the mean motion second derivative.
getMeanObliquityFunction() - Method in enum org.orekit.utils.IERSConventions: Get the function computing mean obliquity of the ecliptic.
getMeasurement() - Method in class org.orekit.files.ccsds.TDMFile.Observation: Getter for the measurement.
getMeasurementsParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator: Get the measurements parameters supported by this estimator (including measurements and modifiers).
getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory: Get the Mercury singleton body.
getMessage(Locale) - Method in interface org.orekit.errors.LocalizedException: Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitException: Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalArgumentException: Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalStateException: Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitInternalError: Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitInternalError
getMessage(Locale) - Method in exception org.orekit.errors.OrekitParseException: Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitParseException
getMetaData() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock: Get the meta-data for the block.
getMetaData() - Method in class org.orekit.files.ccsds.OGMFile: Get the meta data.
getMetaData() - Method in class org.orekit.files.ccsds.OMMFile: Get the meta data.
getMetaData() - Method in class org.orekit.files.ccsds.OPMFile: Get the meta data.
getMetaData() - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock: Get the meta-data for the block.
getMetaDataComment() - Method in class org.orekit.files.ccsds.OPMFile: Get the comment for meta-data.
getMinAlt() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester: Get the minimal altitude for the model.
getMinDate() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation: Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters: Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters: Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.forces.drag.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.