Uses of Interface
org.orekit.utils.FieldPVCoordinatesProvider
Packages that use FieldPVCoordinatesProvider
Package
Description
This package provides classes to represent simple attitudes.
The measurements package defines everything that is related to orbit
determination measurements.
This package provides methods to handle GNSS measurements.
This package contains physical models for measurement prediction.
This package contains class managing CCSDS Attitude Data Message.
This package provides classes to represent orbits.
Propagation
Top level package for analytical propagators.
This package provides classes to propagate GNSS orbits.
This package provides classes to propagate Intelsat's 11 elements.
This package provides classes to read and extrapolate tle's.
This package provides interfaces and classes dealing with events occurring during propagation.
This package provides an interface and classes dealing with events occurrence only.
Utilities for integration-based propagators (both numerical and semi-analytical).
Top level package for numerical propagators.
This package provides interfaces and classes dealing with step handling during propagation.
This package provides an implementation of the Draper Semi-analytical
Satellite Theory (DSST).
This package contains methods and architecture for signal travel time.
This package provides useful objects.
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Uses of FieldPVCoordinatesProvider in org.orekit.attitudes
Methods in org.orekit.attitudes with parameters of type FieldPVCoordinatesProviderModifier and TypeMethodDescription<T extends CalculusFieldElement<T>>
FieldAttitude<T> AttitudeBuilder.build(Frame frame, FieldPVCoordinatesProvider<T> pvProv, TimeStampedFieldAngularCoordinates<T> rawAttitude) Build a filtered attitude.<T extends CalculusFieldElement<T>>
FieldAttitude<T> FixedFrameBuilder.build(Frame frame, FieldPVCoordinatesProvider<T> pvProv, TimeStampedFieldAngularCoordinates<T> rawAttitude) Build a filtered attitude.<T extends CalculusFieldElement<T>>
FieldAttitude<T> AggregateBoundedAttitudeProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> AlignedAndConstrained.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> AttitudeProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.default <T extends CalculusFieldElement<T>>
FieldAttitude<T> AttitudeProviderModifier.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> CelestialBodyPointed.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> FixedRate.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> FrameAlignedProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> GroundPointing.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> LofOffset.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> LofOffsetPointing.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> SpinStabilized.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> TabulatedLofOffset.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> TabulatedProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> TorqueFree.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> YawCompensation.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> YawSteering.getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldRotation<T> AggregateBoundedAttitudeProvider.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldRotation<T> AlignedAndConstrained.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.default <T extends CalculusFieldElement<T>>
FieldRotation<T> AttitudeProvider.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldRotation<T> CelestialBodyPointed.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldRotation<T> FixedRate.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldRotation<T> FrameAlignedProvider.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldRotation<T> GroundPointing.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldRotation<T> LofOffset.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldRotation<T> LofOffsetPointing.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldRotation<T> SpinStabilized.getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.<T extends CalculusFieldElement<T>>
FieldAttitude<T> GroundPointingAttitudeModifier.getBaseState(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the base system state at given date, without modifications.protected <T extends CalculusFieldElement<T>>
FieldVector3D<T> BodyCenterPointing.getTargetPosition(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position in specified frame.protected <T extends CalculusFieldElement<T>>
FieldVector3D<T> GroundPointing.getTargetPosition(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position in specified frame.protected <T extends CalculusFieldElement<T>>
FieldVector3D<T> GroundPointingAttitudeModifier.getTargetPosition(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position in specified frame.protected <T extends CalculusFieldElement<T>>
FieldVector3D<T> LofOffsetPointing.getTargetPosition(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position in specified frame.protected <T extends CalculusFieldElement<T>>
FieldVector3D<T> NadirPointing.getTargetPosition(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position in specified frame.protected <T extends CalculusFieldElement<T>>
FieldVector3D<T> TargetPointing.getTargetPosition(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position in specified frame.<T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> BodyCenterPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position/velocity in specified frame.protected abstract <T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> GroundPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position/velocity in specified frame.<T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> GroundPointingAttitudeModifier.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position/velocity in specified frame.<T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> LofOffsetPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position/velocity in specified frame.<T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> NadirPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position/velocity in specified frame.<T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> TargetPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the target point position/velocity in specified frame.<T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> NadirPointing.getTargetPVViaInterpolation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute target position-velocity-acceleration vector via interpolation (Field version).<T extends CalculusFieldElement<T>>
TYawCompensation.getYawAngle(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the yaw compensation angle at date. -
Uses of FieldPVCoordinatesProvider in org.orekit.estimation.measurements
Methods in org.orekit.estimation.measurements that return FieldPVCoordinatesProviderModifier and TypeMethodDescriptionstatic FieldPVCoordinatesProvider<Gradient> AbstractParticipant.extractFieldPVCoordinatesProvider(SpacecraftState templateState, TimeStampedFieldPVCoordinates<Gradient> pvCoordinates) Create PV provider from position-velocity-acceleration vector and template state.GroundStation.getFieldPVCoordinatesProvider(int freeParameters, Map<String, Integer> parameterIndices) Return the FieldPVCoordinatesProvider.Observer.getFieldPVCoordinatesProvider(int freeParameters, Map<String, Integer> parameterIndices) Return the FieldPVCoordinatesProvider.ObserverSatellite.getFieldPVCoordinatesProvider(int freeParameters, Map<String, Integer> parameterIndices) Return the FieldPVCoordinatesProvider.Methods in org.orekit.estimation.measurements with parameters of type FieldPVCoordinatesProviderModifier and TypeMethodDescriptionprotected FieldAbsoluteDate<Gradient> AngularMeasurement.computeEmissionDateField(Frame frame, FieldVector3D<Gradient> receiverPosition, FieldAbsoluteDate<Gradient> receptionDate, FieldPVCoordinatesProvider<Gradient> emitter) Compute the signal emission date.protected abstract EstimatedMeasurement<T> AbstractRangeRelatedMeasurement.oneWayTheoreticalEvaluation(int iteration, int evaluation, FieldPVCoordinatesProvider<Gradient> observablePVProvider, SpacecraftState state, Map<String, Integer> paramIndices, int nbParams) Evaluate measurement in one-way.protected EstimatedMeasurement<Range> Range.oneWayTheoreticalEvaluation(int iteration, int evaluation, FieldPVCoordinatesProvider<Gradient> satellitePVProvider, SpacecraftState state, Map<String, Integer> indices, int nbParams) Evaluate measurement in one-way.protected EstimatedMeasurement<RangeRate> RangeRate.oneWayTheoreticalEvaluation(int iteration, int evaluation, FieldPVCoordinatesProvider<Gradient> satellitePVProvider, SpacecraftState state, Map<String, Integer> indices, int nbParams) Evaluate measurement in one-way.protected abstract EstimatedMeasurement<T> AbstractRangeRelatedMeasurement.twoWayTheoreticalEvaluation(int iteration, int evaluation, FieldPVCoordinatesProvider<Gradient> observablePVProvider, SpacecraftState state, Map<String, Integer> paramIndices, int nbParams) Evaluate measurement in two-way.protected EstimatedMeasurement<Range> Range.twoWayTheoreticalEvaluation(int iteration, int evaluation, FieldPVCoordinatesProvider<Gradient> satellitePVProvider, SpacecraftState state, Map<String, Integer> indices, int nbParams) Evaluate measurement in two-way.protected EstimatedMeasurement<RangeRate> RangeRate.twoWayTheoreticalEvaluation(int iteration, int evaluation, FieldPVCoordinatesProvider<Gradient> satellitePVProvider, SpacecraftState state, Map<String, Integer> indices, int nbParams) Evaluate measurement in two-way. -
Uses of FieldPVCoordinatesProvider in org.orekit.estimation.measurements.gnss
Methods in org.orekit.estimation.measurements.gnss that return FieldPVCoordinatesProviderModifier and TypeMethodDescriptionprotected FieldPVCoordinatesProvider<Gradient> AbstractInterSatellitesMeasurement.getRemotePV(SpacecraftState state, int freeParameters) Return the FieldPVCoordinatesProvider. -
Uses of FieldPVCoordinatesProvider in org.orekit.estimation.measurements.model
Methods in org.orekit.estimation.measurements.model with parameters of type FieldPVCoordinatesProviderModifier and TypeMethodDescriptionprotected <T extends CalculusFieldElement<T>>
FieldVector3D<T> AbstractAngularMeasurementModel.getEmitterToReceiverVector(FieldSignalReceptionCondition<T> receptionCondition, FieldPVCoordinatesProvider<T> emitter, FieldAbsoluteDate<T> approxEmissionDate) Compute emitter-to-receiver vector with FIeld.<T extends CalculusFieldElement<T>>
TOneLeggedRangeRateModel.value(FieldSignalReceptionCondition<T> receptionCondition, FieldVector3D<T> receiverVelocity, FieldPVCoordinatesProvider<T> emitter) Compute measurement without guess.<T extends CalculusFieldElement<T>>
TOneLeggedRangeRateModel.value(FieldSignalReceptionCondition<T> receptionCondition, FieldVector3D<T> receiverVelocity, FieldPVCoordinatesProvider<T> emitter, FieldAbsoluteDate<T> approxEmissionDate) Compute measurement.<T extends CalculusFieldElement<T>>
T[]RaDecModel.value(FieldSignalReceptionCondition<T> receptionCondition, FieldPVCoordinatesProvider<T> emitter) Compute theoretical measurement with FIeld.<T extends CalculusFieldElement<T>>
T[]RaDecModel.value(FieldSignalReceptionCondition<T> receptionCondition, FieldPVCoordinatesProvider<T> emitter, FieldAbsoluteDate<T> approxEmissionDate) Compute theoretical measurement with FIeld with guess for emission date.<T extends CalculusFieldElement<T>>
T[]TopocentricAzElModel.value(FieldGeodeticPoint<T> receiver, FieldAbsoluteDate<T> receptionDate, FieldPVCoordinatesProvider<T> emitter) Compute theoretical measurement with FIeld.<T extends CalculusFieldElement<T>>
T[]TopocentricAzElModel.value(FieldGeodeticPoint<T> receiver, FieldAbsoluteDate<T> receptionDate, FieldPVCoordinatesProvider<T> emitter, FieldAbsoluteDate<T> approxEmissionDate) Compute theoretical measurement with FIeld with guess for emission date.<T extends CalculusFieldElement<T>>
TTwoLeggedRangeRateModel.value(FieldSignalReceptionCondition<T> receptionCondition, FieldVector3D<T> receiverVelocity, FieldPVCoordinatesProvider<T> relay, FieldAbsoluteDate<T> approxRelayDate, FieldPVCoordinatesProvider<T> emitter, FieldAbsoluteDate<T> approxEmissionDate) Compute measurement.<T extends CalculusFieldElement<T>>
TTwoLeggedRangeRateModel.value(FieldSignalReceptionCondition<T> receptionCondition, FieldVector3D<T> receiverVelocity, FieldPVCoordinatesProvider<T> relay, FieldPVCoordinatesProvider<T> emitter) Compute measurement without guess. -
Uses of FieldPVCoordinatesProvider in org.orekit.files.ccsds.ndm.adm
Methods in org.orekit.files.ccsds.ndm.adm with parameters of type FieldPVCoordinatesProviderModifier and TypeMethodDescription<T extends CalculusFieldElement<T>>
FieldAttitude<T> AttitudeEndpoints.build(Frame frame, FieldPVCoordinatesProvider<T> pvProv, TimeStampedFieldAngularCoordinates<T> rawAttitude) Build a filtered attitude. -
Uses of FieldPVCoordinatesProvider in org.orekit.orbits
Classes in org.orekit.orbits that implement FieldPVCoordinatesProviderModifier and TypeClassDescriptionclassFieldCartesianOrbit<T extends CalculusFieldElement<T>>This class holds Cartesian orbital parameters.classFieldCircularOrbit<T extends CalculusFieldElement<T>>This class handles circular orbital parameters.classFieldEquinoctialOrbit<T extends CalculusFieldElement<T>>This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.classFieldKeplerianOrbit<T extends CalculusFieldElement<T>>This class handles traditional Keplerian orbital parameters.classFieldOrbit<T extends CalculusFieldElement<T>>This class handles orbital parameters. -
Uses of FieldPVCoordinatesProvider in org.orekit.propagation
Subinterfaces of FieldPVCoordinatesProvider in org.orekit.propagationModifier and TypeInterfaceDescriptioninterfaceFieldBoundedPropagator<T extends CalculusFieldElement<T>>This interface is intended for ephemerides valid only during a time range.interfaceFieldPropagator<T extends CalculusFieldElement<T>>This interface provides a way to propagate an orbit at any time.Classes in org.orekit.propagation that implement FieldPVCoordinatesProviderModifier and TypeClassDescriptionclassFieldAbstractPropagator<T extends CalculusFieldElement<T>>Common handling ofPropagatormethods for analytical propagators. -
Uses of FieldPVCoordinatesProvider in org.orekit.propagation.analytical
Classes in org.orekit.propagation.analytical that implement FieldPVCoordinatesProviderModifier and TypeClassDescriptionclassFieldAbstractAnalyticalPropagator<T extends CalculusFieldElement<T>>Common handling ofFieldPropagatormethods for analytical propagators.classFieldBrouwerLyddanePropagator<T extends CalculusFieldElement<T>>This class propagates aFieldSpacecraftStateusing the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).classFieldEcksteinHechlerPropagator<T extends CalculusFieldElement<T>>This class propagates aFieldSpacecraftStateusing the analytical Eckstein-Hechler model.classFieldEphemeris<T extends CalculusFieldElement<T>>This class is designed to accept and handle tabulated orbital entries.classFieldKeplerianPropagator<T extends CalculusFieldElement<T>>Simple Keplerian orbit propagator. -
Uses of FieldPVCoordinatesProvider in org.orekit.propagation.analytical.gnss
Classes in org.orekit.propagation.analytical.gnss that implement FieldPVCoordinatesProviderModifier and TypeClassDescriptionclassFieldGnssPropagator<T extends CalculusFieldElement<T>>Common handling ofFieldAbstractAnalyticalPropagatormethods for GNSS propagators. -
Uses of FieldPVCoordinatesProvider in org.orekit.propagation.analytical.intelsat
Classes in org.orekit.propagation.analytical.intelsat that implement FieldPVCoordinatesProviderModifier and TypeClassDescriptionclassFieldIntelsatElevenElementsPropagator<T extends CalculusFieldElement<T>>This class provides elements to propagate Intelsat's 11 elements. -
Uses of FieldPVCoordinatesProvider in org.orekit.propagation.analytical.tle
Classes in org.orekit.propagation.analytical.tle that implement FieldPVCoordinatesProviderModifier and TypeClassDescriptionclassFieldDeepSDP4<T extends CalculusFieldElement<T>>This class contains the methods that compute deep space perturbation terms.classFieldSGP4<T extends CalculusFieldElement<T>>This class contains methods to compute propagated coordinates with the SGP4 model.classFieldTLEPropagator<T extends CalculusFieldElement<T>>This class provides elements to propagate TLE's. -
Uses of FieldPVCoordinatesProvider in org.orekit.propagation.events
Methods in org.orekit.propagation.events that return FieldPVCoordinatesProviderModifier and TypeMethodDescriptionFieldBetaAngleDetector.getCelestialBodyProvider()Coordinate provider for the celestial body.FieldExtremumApproachDetector.getSecondaryPVProvider()Get the secondary position-velocity provider stored in this instance.FieldRelativeDistanceDetector.getSecondaryPVProvider()Get the secondary position-velocity provider stored in this instance.Methods in org.orekit.propagation.events with parameters of type FieldPVCoordinatesProviderModifier and TypeMethodDescriptionstatic <T extends CalculusFieldElement<T>>
TFieldBetaAngleDetector.calculateBetaAngle(FieldSpacecraftState<T> state, FieldPVCoordinatesProvider<T> celestialBodyProvider) Calculate the beta angle between the orbit plane and the celestial body.static <T extends CalculusFieldElement<T>>
TFieldBetaAngleDetector.calculateBetaAngle(FieldSpacecraftState<T> state, FieldPVCoordinatesProvider<T> celestialBodyProvider, Frame frame) Calculate the beta angle between the orbit plane and the celestial body.FieldBetaAngleDetector.withCelestialProvider(FieldPVCoordinatesProvider<T> newProvider) Create a new instance with the provided coordinate provider.Constructors in org.orekit.propagation.events with parameters of type FieldPVCoordinatesProviderModifierConstructorDescriptionFieldBetaAngleDetector(Field<T> field, T betaAngleThreshold, FieldPVCoordinatesProvider<T> celestialBodyProvider, Frame inertialFrame) Class constructor.protectedFieldBetaAngleDetector(FieldEventDetectionSettings<T> detectionSettings, FieldEventHandler<T> handler, T betaAngleThreshold, FieldPVCoordinatesProvider<T> celestialBodyProvider, Frame inertialFrame) Protected constructor with full parameters.FieldExtremumApproachDetector(Field<T> field, FieldPVCoordinatesProvider<T> secondaryPVProvider) Constructor with default values.protectedFieldExtremumApproachDetector(FieldEventDetectionSettings<T> detectionSettings, FieldEventHandler<T> handler, FieldPVCoordinatesProvider<T> secondaryPVProvider) Constructor.protectedFieldRelativeDistanceDetector(FieldEventDetectionSettings<T> detectionSettings, FieldEventHandler<T> handler, FieldPVCoordinatesProvider<T> secondaryPVProvider, T distanceThreshold) Constructor.FieldRelativeDistanceDetector(FieldPVCoordinatesProvider<T> secondaryPVProvider, T distanceThreshold) Constructor with default values. -
Uses of FieldPVCoordinatesProvider in org.orekit.propagation.events.handlers
Methods in org.orekit.propagation.events.handlers that return FieldPVCoordinatesProviderModifier and TypeMethodDescriptionFieldSecondaryEventLogger.getSecondaryPVCoordinatesProvider()Getter for the secondary trajectory provider.Constructors in org.orekit.propagation.events.handlers with parameters of type FieldPVCoordinatesProviderModifierConstructorDescriptionFieldSecondaryEventLogger(FieldPVCoordinatesProvider<T> secondaryPVCoordinatesProvider) Constructor with default Action (CONTINUE).FieldSecondaryEventLogger(FieldPVCoordinatesProvider<T> secondaryPVCoordinatesProvider, Action action) Constructor. -
Uses of FieldPVCoordinatesProvider in org.orekit.propagation.integration
Classes in org.orekit.propagation.integration that implement FieldPVCoordinatesProviderModifier and TypeClassDescriptionclassFieldAbstractIntegratedPropagator<T extends CalculusFieldElement<T>>Common handling ofFieldPropagatormethods for both numerical and semi-analytical propagators.classFieldIntegratedEphemeris<T extends CalculusFieldElement<T>>This class stores sequentially generated orbital parameters for later retrieval. -
Uses of FieldPVCoordinatesProvider in org.orekit.propagation.numerical
Classes in org.orekit.propagation.numerical that implement FieldPVCoordinatesProviderModifier and TypeClassDescriptionclassFieldNumericalPropagator<T extends CalculusFieldElement<T>>This class propagatesorbitsusing numerical integration. -
Uses of FieldPVCoordinatesProvider in org.orekit.propagation.sampling
Subinterfaces of FieldPVCoordinatesProvider in org.orekit.propagation.samplingModifier and TypeInterfaceDescriptioninterfaceFieldOrekitStepInterpolator<T extends CalculusFieldElement<T>>This interface is a space-dynamics aware step interpolator. -
Uses of FieldPVCoordinatesProvider in org.orekit.propagation.semianalytical.dsst
Classes in org.orekit.propagation.semianalytical.dsst that implement FieldPVCoordinatesProviderModifier and TypeClassDescriptionclassFieldDSSTPropagator<T extends CalculusFieldElement<T>>This class propagatesorbitsusing the DSST theory. -
Uses of FieldPVCoordinatesProvider in org.orekit.signal
Methods in org.orekit.signal with parameters of type FieldPVCoordinatesProviderModifier and TypeMethodDescription<T extends CalculusFieldElement<T>>
T[]DifferencesOfSignalArrival.computeDelays(FieldSignalReceptionCondition<T> primaryReceptionCondition, FieldPVCoordinatesProvider<T> secondaryReceiver, FieldAbsoluteDate<T> approxSecondaryReception, FieldPVCoordinatesProvider<T> emitter, FieldAbsoluteDate<T> approxEmissionDate) Compute (positive) delays from emission.<T extends CalculusFieldElement<T>>
T[]DifferencesOfSignalArrival.computeDelays(FieldSignalReceptionCondition<T> primaryReceptionCondition, FieldPVCoordinatesProvider<T> secondaryReceiver, FieldPVCoordinatesProvider<T> emitter) Compute (positive) delays from emission without guesses.<T extends CalculusFieldElement<T>>
T[]TwoLeggedSignalTimer.computeDelays(FieldSignalReceptionCondition<T> endReceptionCondition, FieldPVCoordinatesProvider<T> relay, FieldAbsoluteDate<T> approxRelayDate, FieldPVCoordinatesProvider<T> emitter, FieldAbsoluteDate<T> approxEmissionDate) Compute first and second leg delays.<T extends CalculusFieldElement<T>>
T[]TwoLeggedSignalTimer.computeDelays(FieldSignalReceptionCondition<T> endReceptionCondition, FieldPVCoordinatesProvider<T> relay, FieldPVCoordinatesProvider<T> emitter) Compute first and second leg delays without guess.<T extends CalculusFieldElement<T>>
FieldAdjustableEmitterSignalTimer<T> SignalTravelTimeModel.getFieldAdjustableEmitterComputer(Field<T> field, FieldPVCoordinatesProvider<T> emitter) Method constructing a delay computer with input emitter.<T extends CalculusFieldElement<T>>
FieldAdjustableReceiverSignalTimer<T> SignalTravelTimeModel.getFieldAdjustableReceiverComputer(Field<T> field, FieldPVCoordinatesProvider<T> receiver) Method constructing a delay computer with input receiver.Constructors in org.orekit.signal with parameters of type FieldPVCoordinatesProviderModifierConstructorDescriptionFieldAdjustableEmitterSignalTimer(FieldPVCoordinatesProvider<T> adjustableEmitterPVProvider) Constructor with default iteration settings.FieldAdjustableEmitterSignalTimer(FieldPVCoordinatesProvider<T> adjustableEmitterPVProvider, ConvergenceChecker<T> convergenceChecker) Constructor.FieldAdjustableReceiverSignalTimer(FieldPVCoordinatesProvider<T> adjustableReceiverPVProvider) Constructor with default iteration settings.FieldAdjustableReceiverSignalTimer(FieldPVCoordinatesProvider<T> adjustableReceiverPVProvider, ConvergenceChecker<T> convergenceChecker) Constructor. -
Uses of FieldPVCoordinatesProvider in org.orekit.utils
Classes in org.orekit.utils with type parameters of type FieldPVCoordinatesProviderModifier and TypeInterfaceDescriptioninterfaceShiftableFieldPVCoordinatesHolder<S extends FieldPVCoordinatesProvider<T>,T extends CalculusFieldElement<T>> Interface for time-shiftable Field PV provider holding themselves PV coordinates.Subinterfaces of FieldPVCoordinatesProvider in org.orekit.utilsModifier and TypeInterfaceDescriptioninterfaceFieldBoundedPVCoordinatesProvider<T extends CalculusFieldElement<T>>Interface for bounded, Field PV coordinates providers.interfaceShiftableFieldPVCoordinatesHolder<S extends FieldPVCoordinatesProvider<T>,T extends CalculusFieldElement<T>> Interface for time-shiftable Field PV provider holding themselves PV coordinates.Classes in org.orekit.utils that implement FieldPVCoordinatesProviderModifier and TypeClassDescriptionclassFieldAbsolutePVCoordinates<T extends CalculusFieldElement<T>>Field implementation of AbsolutePVCoordinates.Methods in org.orekit.utils that return FieldPVCoordinatesProviderModifier and TypeMethodDescriptionprotected abstract <S extends CalculusFieldElement<S>>
FieldPVCoordinatesProvider<S> AbstractExtendedPositionProvider.getFieldProvider(Field<S> field) Build Field provider.default <T extends CalculusFieldElement<T>>
FieldPVCoordinatesProvider<T> ExtendedPositionProvider.toFieldPVCoordinatesProvider(Field<T> field) Convert to aFieldPVCoordinatesProviderwith a specific type.FieldAbsolutePVCoordinates.toTaylorProvider()Create a local provider using simply Taylor expansion throughFieldAbsolutePVCoordinates.shiftedBy(double).