Uses of Class
org.orekit.utils.TimeStampedFieldPVCoordinates
Packages that use TimeStampedFieldPVCoordinates
Package
Description
This package provides classes to represent simple attitudes.
This package provides interface to represent the position and geometry of
space objects such as stars, planets or asteroids.
Package relative provides classes to compute typical maneuvers of relative proximity operations (RPO).
The measurements package defines everything that is related to orbit
determination measurements.
This package provides measurement modifier.
This package provides all gravity-related forces.
This package provides classes to handle frames and transforms between them.
This package provides classes to represent orbits.
Propagation
Top level package for relative motion propagation.
This package provides an implementation of the equations of Clohessy and Wiltshire.
This package provides an implementation of the equations of Yamanaka and Ankersen.
This package provides interfaces and classes dealing with step handling during propagation.
This package provides useful objects.
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Uses of TimeStampedFieldPVCoordinates in org.orekit.attitudes
Methods in org.orekit.attitudes that return TimeStampedFieldPVCoordinatesModifier and TypeMethodDescription<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).Methods in org.orekit.attitudes with parameters of type TimeStampedFieldPVCoordinatesModifier and TypeMethodDescription<T extends CalculusFieldElement<T>>
FieldVector3D<FieldUnivariateDerivative2<T>> GroundPointTarget.getDerivative2TargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedFieldPVCoordinates<T> pv, Frame frame) Get a target vector.default <T extends CalculusFieldElement<T>>
FieldVector3D<FieldUnivariateDerivative2<T>> TargetProvider.getDerivative2TargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedFieldPVCoordinates<T> pv, Frame frame) Get a target vector.<T extends CalculusFieldElement<T>>
FieldVector3D<T> GroundPointTarget.getTargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedFieldPVCoordinates<T> pv, Frame frame) Get a target vector.<T extends CalculusFieldElement<T>>
FieldVector3D<T> TargetProvider.getTargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedFieldPVCoordinates<T> pv, Frame frame) Get a target vector. -
Uses of TimeStampedFieldPVCoordinates in org.orekit.bodies
Methods in org.orekit.bodies that return TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptionFieldEllipse.projectToEllipse(TimeStampedFieldPVCoordinates<T> pv) Project position-velocity-acceleration on an ellipse.Methods in org.orekit.bodies with parameters of type TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptionFieldEllipse.projectToEllipse(TimeStampedFieldPVCoordinates<T> pv) Project position-velocity-acceleration on an ellipse. -
Uses of TimeStampedFieldPVCoordinates in org.orekit.control.relative
Methods in org.orekit.control.relative that return TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptiondefault <T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> RPO.computeNaturalCircumnavigationInjectionCircular(FieldAbsoluteDate<T> startDate, T distanceAlongVBar, T inclination, T targetMeanMotion) Computes the injection PVT for a natural circumnavigation around a target in a circular orbit.Methods in org.orekit.control.relative that return types with arguments of type TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptiondefault <T extends CalculusFieldElement<T>>
List<TimeStampedFieldPVCoordinates<T>> RPO.computeForcedCircularMotionWaypoints(FieldAbsoluteDate<T> startDate, FieldVector3D<T> centerOffset, T radius, T inclination, T raan, T orbitDuration, int pointsOnOrbit, int numberOfRevolutions, T startAngle, boolean retrograde) Computes the waypoints to perform a forced circular orbit.default <T extends CalculusFieldElement<T>>
List<TimeStampedFieldPVCoordinates<T>> RPO.computeForcedLinearWaypoints(TimeStampedFieldPVCoordinates<T> initialPVT, TimeStampedFieldPVCoordinates<T> finalPVT, int numberOfPoints) Computes the waypoints along the linear path.<T extends CalculusFieldElement<T>>
List<TimeStampedFieldPVCoordinates<T>> RPO.computeTeardropWaypoints(FieldAbsoluteDate<T> injectionDate, FieldOrbit<T> targetOrbit, T turnAroundDistance, T maneuverDistance, int numberOfTeardrops) Computes teardrop waypoints.FieldTeardropCircularWaypointCalculator.computeTearDropWaypoints(FieldAbsoluteDate<T> injectionDate) Computes the waypoints of the teardrop relative orbit in QSW Local Orbital Frame to use them with Clohessy-Wiltshire maneuvers.Methods in org.orekit.control.relative with parameters of type TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptiondefault <T extends CalculusFieldElement<T>>
List<TimeStampedFieldPVCoordinates<T>> RPO.computeForcedLinearWaypoints(TimeStampedFieldPVCoordinates<T> initialPVT, TimeStampedFieldPVCoordinates<T> finalPVT, int numberOfPoints) Computes the waypoints along the linear path.Method parameters in org.orekit.control.relative with type arguments of type TimeStampedFieldPVCoordinatesModifier and TypeMethodDescription<T extends CalculusFieldElement<T>>
List<FieldRelativeManeuver<T>> RPO.computeForcedManeuvers(List<TimeStampedFieldPVCoordinates<T>> waypoints, FieldVector3D<T> initialVelocity, FieldOrbit<T> targetOrbit, FieldRelativeProvider<T> provider) Compute relative maneuvers to realize a forced trajectory defined by the waypoints (ForcedLinear/ForcedCircular).<T extends CalculusFieldElement<T>>
List<FieldRelativeManeuver<T>> RPO.computeTeardropManeuvers(List<TimeStampedFieldPVCoordinates<T>> waypoints, FieldRelativeProvider<T> relativeProvider) Computes the relative maneuvers of the teardrop relative orbit in the RPOModel Local Orbital Frame. -
Uses of TimeStampedFieldPVCoordinates in org.orekit.estimation.measurements
Methods in org.orekit.estimation.measurements that return TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptionAbstractMeasurement.getCoordinates(SpacecraftState state, int firstDerivative, int freeParameters) Get Cartesian coordinates as derivatives.Methods in org.orekit.estimation.measurements with parameters of type TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptionstatic FieldPVCoordinatesProvider<Gradient> AbstractParticipant.extractFieldPVCoordinatesProvider(SpacecraftState templateState, TimeStampedFieldPVCoordinates<Gradient> pvCoordinates) Create PV provider from position-velocity-acceleration vector and template state. -
Uses of TimeStampedFieldPVCoordinates in org.orekit.estimation.measurements.modifiers
Methods in org.orekit.estimation.measurements.modifiers with parameters of type TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptionstatic Gradient[]AberrationModifier.fieldNaturalToProper(Gradient[] naturalRaDec, TimeStampedFieldPVCoordinates<Gradient> pvCoords, Frame frame) Natural to proper correction for aberration of light.static Gradient[]AberrationModifier.fieldNaturalToProper(Gradient[] naturalRaDec, TimeStampedFieldPVCoordinates<Gradient> pvCoords, Frame frame, DataContext context) Natural to proper correction for aberration of light.static Gradient[]AberrationModifier.fieldProperToNatural(Gradient[] properRaDec, TimeStampedFieldPVCoordinates<Gradient> pvCoords, Frame frame) Proper to natural correction for aberration of light.static Gradient[]AberrationModifier.fieldProperToNatural(Gradient[] properRaDec, TimeStampedFieldPVCoordinates<Gradient> pvCoords, Frame frame, DataContext context) Proper to natural correction for aberration of light. -
Uses of TimeStampedFieldPVCoordinates in org.orekit.forces.gravity
Methods in org.orekit.forces.gravity that return TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptionprotected <T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> AbstractBodyAttraction.getBodyPVCoordinates(FieldAbsoluteDate<T> date, Frame frame) Get the body's position-velocity-acceleration vector. -
Uses of TimeStampedFieldPVCoordinates in org.orekit.frames
Methods in org.orekit.frames that return TimeStampedFieldPVCoordinatesModifier and TypeMethodDescription<T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> TopocentricFrame.getPVCoordinates(FieldAbsoluteDate<T> date, Frame frame) Get the position-velocity-acceleration in the selected frame.default TimeStampedFieldPVCoordinates<T> FieldKinematicTransform.transformOnlyPV(TimeStampedFieldPVCoordinates<T> pv) TransformTimeStampedPVCoordinates, without the acceleration vector.FieldTransform.transformPVCoordinates(TimeStampedFieldPVCoordinates<T> pv) TransformTimeStampedFieldPVCoordinatesincluding kinematic effects.FieldTransform.transformPVCoordinates(TimeStampedPVCoordinates pv) TransformTimeStampedPVCoordinatesincluding kinematic effects.<T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> Transform.transformPVCoordinates(TimeStampedFieldPVCoordinates<T> pv) TransformTimeStampedFieldPVCoordinatesincluding kinematic effects.Methods in org.orekit.frames with parameters of type TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptiondefault TimeStampedFieldPVCoordinates<T> FieldKinematicTransform.transformOnlyPV(TimeStampedFieldPVCoordinates<T> pv) TransformTimeStampedPVCoordinates, without the acceleration vector.FieldTransform.transformPVCoordinates(TimeStampedFieldPVCoordinates<T> pv) TransformTimeStampedFieldPVCoordinatesincluding kinematic effects.<T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> Transform.transformPVCoordinates(TimeStampedFieldPVCoordinates<T> pv) TransformTimeStampedFieldPVCoordinatesincluding kinematic effects. -
Uses of TimeStampedFieldPVCoordinates in org.orekit.orbits
Methods in org.orekit.orbits that return TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptionFieldOrbit.getPVCoordinates()Get theTimeStampedPVCoordinatesin definition frame.FieldOrbit.getPVCoordinates(Frame outputFrame) Get theTimeStampedPVCoordinatesin a specified frame.FieldOrbit.getPVCoordinates(FieldAbsoluteDate<T> otherDate, Frame otherFrame) Get theFieldPVCoordinatesof the body in the selected frame.protected TimeStampedFieldPVCoordinates<T> FieldCartesianOrbit.initPVCoordinates()Compute the position/velocity coordinates from the canonical parameters.protected TimeStampedFieldPVCoordinates<T> FieldCircularOrbit.initPVCoordinates()Compute the position/velocity coordinates from the canonical parameters.protected TimeStampedFieldPVCoordinates<T> FieldEquinoctialOrbit.initPVCoordinates()Compute the position/velocity coordinates from the canonical parameters.protected TimeStampedFieldPVCoordinates<T> FieldKeplerianOrbit.initPVCoordinates()Compute the position/velocity coordinates from the canonical parameters.protected abstract TimeStampedFieldPVCoordinates<T> FieldOrbit.initPVCoordinates()Compute the position/velocity coordinates from the canonical parameters.Constructors in org.orekit.orbits with parameters of type TimeStampedFieldPVCoordinatesModifierConstructorDescriptionFieldCartesianOrbit(TimeStampedFieldPVCoordinates<T> pvaCoordinates, Frame frame, T mu) Constructor from Cartesian parameters.FieldCircularOrbit(TimeStampedFieldPVCoordinates<T> pvCoordinates, Frame frame, T mu) Constructor from Cartesian parameters.FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates<T> pvCoordinates, Frame frame, T mu) Constructor from Cartesian parameters.FieldKeplerianOrbit(TimeStampedFieldPVCoordinates<T> pvCoordinates, Frame frame, T mu) Constructor from Cartesian parameters.protectedFieldOrbit(TimeStampedFieldPVCoordinates<T> fieldPVCoordinates, Frame frame, T mu) Set the orbit from Cartesian parameters. -
Uses of TimeStampedFieldPVCoordinates in org.orekit.propagation
Methods in org.orekit.propagation that return TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptiondefault TimeStampedFieldPVCoordinates<T> FieldPropagator.getPVCoordinates(FieldAbsoluteDate<T> date, Frame frame) Get theFieldPVCoordinatesof the body in the selected frame.FieldSpacecraftState.getPVCoordinates()Get theTimeStampedFieldPVCoordinatesin orbit definition frame.FieldSpacecraftState.getPVCoordinates(Frame outputFrame) Get theTimeStampedFieldPVCoordinatesin given output frame. -
Uses of TimeStampedFieldPVCoordinates in org.orekit.propagation.relative
Methods in org.orekit.propagation.relative that return TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptionFieldRelativeProvider.extractChaserPVT(FieldSpacecraftState<T> targetState) Extracts the chaser's PVT in the target LOF from the given targetFieldSpacecraftState.default TimeStampedFieldPVCoordinates<T> FieldRelativeProvider.extractChaserPVT(FieldSpacecraftState<T> targetState, Frame outputFrame) Extracts the chaser's PVT from the given targetFieldSpacecraftStateand converts it to the desired output frame.FieldAbstractRelativeProvider.getInitialChaserPVTLof()Get the initial TimeStampedPVCoordinates of the chaser in the Local Orbital Frame of the target.FieldRelativeProvider.getInitialChaserPVTLof()Get the initial TimeStampedPVCoordinates of the chaser in the Local Orbital Frame of the target.FieldTwoImpulseTransfer.getPvt1()Gets the PVT of the chaser just after the first maneuver, i.e. at the start of the transfer orbit.Get the PVT of the chaser just after the first maneuver expressed in the given frame.FieldTwoImpulseTransfer.getPvt1BeforeMan()Get the PVT before the injection maneuver into the transfer orbit.FieldTwoImpulseTransfer.getPvt2()Gets the PVT of the chaser just before the second maneuver, i.e. at the end of the transfer orbit.Get the PVT of the chaser just before the second maneuver expressed in the given frame.FieldTwoImpulseTransfer.getPvt2AfterMan()Get the PVT after the velocity-synchronization maneuver into the target orbit.Methods in org.orekit.propagation.relative with parameters of type TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptionFieldTwoImpulseTransfer.fromPVTAndVelocities(TimeStampedFieldPVCoordinates<T> pvt1BeforeMan, FieldVector3D<T> v1AfterMan, TimeStampedFieldPVCoordinates<T> pvt2AfterMan, FieldVector3D<T> v2BeforeMan, Frame inputFrame) Creates a newTwoImpulseTransferobject from the given PVT before the first maneuver and after the second maneuver (on the initial and final orbits), as well as the velocity vectors after the first maneuver and before the second maneuver (on the transfer orbit).voidFieldAbstractRelativeProvider.setInitialChaserPVTLof(TimeStampedFieldPVCoordinates<T> initialChaserPVTLof) Set the initial TimeStampedPVCoordinates of the chaser in the Local Orbital Frame of the target.voidFieldRelativeProvider.setInitialChaserPVTLof(TimeStampedFieldPVCoordinates<T> initialChaserPVTLof) Set the initial TimeStampedPVCoordinates of the chaser in the Local Orbital Frame of the target.Constructors in org.orekit.propagation.relative with parameters of type TimeStampedFieldPVCoordinatesModifierConstructorDescriptionFieldAbstractRelativeProvider(FieldOrbit<T> targetOrbit, TimeStampedFieldPVCoordinates<T> initialChaserPVTLof, String additionalEquationsName, LOF lof) Builds a new RelativeProvider object from the target orbit and an initial PVT of the chaser.FieldAbstractRelativeProvider(FieldOrbit<T> targetOrbit, TimeStampedFieldPVCoordinates<T> initialChaserPVT, Frame inputPVTFrame, String additionalEquationsName, LOF lof) Builds a new Relativeprovider object from the target orbit and an initial PVT of the chaser expressed in the given input frame.FieldTwoImpulseTransfer(TimeStampedFieldPVCoordinates<T> pvt1, TimeStampedFieldPVCoordinates<T> pvt2, FieldVector3D<T> deltaV1, FieldVector3D<T> deltaV2, Frame frame) Creates a new TwoImpulseTransfer object from the given PVT and ΔV vectors. -
Uses of TimeStampedFieldPVCoordinates in org.orekit.propagation.relative.clohessywiltshire
Methods in org.orekit.propagation.relative.clohessywiltshire that return TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptionFieldClohessyWiltshireProvider.extractChaserPVT(FieldSpacecraftState<T> targetState) Extracts the chaser's PVT in the target LOF from the given targetFieldSpacecraftState.FieldClohessyWiltshireMatrices.transform(TimeStampedFieldPVCoordinates<T> pvt) Transforms the input initial PVT expressed in the target's QSW LOF to the PVT at the time encoded in the Clohessy-Wiltshire matrices contained in the object.Methods in org.orekit.propagation.relative.clohessywiltshire with parameters of type TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptionFieldClohessyWiltshireRendezVous.computeRendezVous(TimeStampedFieldPVCoordinates<T> chaserPVTInitial, TimeStampedFieldPVCoordinates<T> chaserPVTFinal, Frame chaserPVFrame, FieldOrbit<T> targetOrbit) Computes a two-impulse transfer between an initial and final positions using the Clohessy-Wiltshire closed-form solution.FieldClohessyWiltshireMatrices.transform(TimeStampedFieldPVCoordinates<T> pvt) Transforms the input initial PVT expressed in the target's QSW LOF to the PVT at the time encoded in the Clohessy-Wiltshire matrices contained in the object.Constructors in org.orekit.propagation.relative.clohessywiltshire with parameters of type TimeStampedFieldPVCoordinatesModifierConstructorDescriptionFieldClohessyWiltshireProvider(FieldOrbit<T> targetOrbit, TimeStampedFieldPVCoordinates<T> initialChaserPVTLof) Builds a new provider object from the target orbit and an initial PVT of the chaser.FieldClohessyWiltshireProvider(FieldOrbit<T> targetOrbit, TimeStampedFieldPVCoordinates<T> initialChaserPVTLof, String additionalEquationsName) Builds a new ClohessyWiltshireProvider object from the target orbit and an initial PVT of the chaser.FieldClohessyWiltshireProvider(FieldOrbit<T> targetOrbit, TimeStampedFieldPVCoordinates<T> initialChaserPVT, Frame inputPVTFrame) Builds a new ClohessyWiltshireProvider object from the target orbit and an initial PVT of the chaser expressed in the given input frame.FieldClohessyWiltshireProvider(FieldOrbit<T> targetOrbit, TimeStampedFieldPVCoordinates<T> initialChaserPVT, Frame inputPVTFrame, String additionalEquationsName) Builds a new ClohessyWiltshireProvider object from the target orbit and an initial PVT of the chaser expressed in the given input frame. -
Uses of TimeStampedFieldPVCoordinates in org.orekit.propagation.relative.yamanakaankersen
Methods in org.orekit.propagation.relative.yamanakaankersen that return TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptionFieldYamanakaAnkersenProvider.extractChaserPVT(FieldSpacecraftState<T> targetState) Extracts the chaser's PVT in the target LOF from the given targetFieldSpacecraftState.FieldYamanakaAnkersenMatrices.transform(TimeStampedFieldPVCoordinates<T> pvt, T initialTrueAnomaly, T trueAnomaly, T eccentricity, T sma, T mu) Transforms the input initial PVT expressed in the target's LVLH CCSDS LOF to the PVT at the time and true anomaly associated encoded in the Yamanaka-Ankersen matrices contained in the object.Methods in org.orekit.propagation.relative.yamanakaankersen with parameters of type TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptionFieldYamanakaAnkersenRendezVous.computeRendezVous(TimeStampedFieldPVCoordinates<T> chaserPVTInitial, TimeStampedFieldPVCoordinates<T> chaserPVTFinal, Frame chaserPVFrame, FieldOrbit<T> targetOrbit, FieldPropagator<T> propagator) Computes a two-impulse transfer between an initial and final positions using the Yamanaka-Ankersen closed-form solution.FieldYamanakaAnkersenMatrices.transform(TimeStampedFieldPVCoordinates<T> pvt, T initialTrueAnomaly, T trueAnomaly, T eccentricity, T sma, T mu) Transforms the input initial PVT expressed in the target's LVLH CCSDS LOF to the PVT at the time and true anomaly associated encoded in the Yamanaka-Ankersen matrices contained in the object.Constructors in org.orekit.propagation.relative.yamanakaankersen with parameters of type TimeStampedFieldPVCoordinatesModifierConstructorDescriptionFieldYamanakaAnkersenProvider(FieldOrbit<T> targetOrbit, TimeStampedFieldPVCoordinates<T> initialChaserPVTLof) Builds a new YamanakaAnkersenProvider object from the target orbit and an all-zero PVT for the chaser.FieldYamanakaAnkersenProvider(FieldOrbit<T> targetOrbit, TimeStampedFieldPVCoordinates<T> initialChaserPVTLof, String additionalEquationsName) Builds a new YamanakaAnkersenProvider object from the target orbit and an initial PVT of the chaser.FieldYamanakaAnkersenProvider(FieldOrbit<T> targetOrbit, TimeStampedFieldPVCoordinates<T> initialChaserPVT, Frame inputPVTFrame) Builds a new YamanakaAnkersenProvider object from the target orbit and an initial PVT of the chaser expressed in the given input frame.FieldYamanakaAnkersenProvider(FieldOrbit<T> targetOrbit, TimeStampedFieldPVCoordinates<T> initialChaserPVT, Frame inputPVTFrame, String additionalEquationsName) Builds a new YamanakaAnkersenProvider object from the target orbit and an initial PVT of the chaser expressed in the given input frame. -
Uses of TimeStampedFieldPVCoordinates in org.orekit.propagation.sampling
Methods in org.orekit.propagation.sampling that return TimeStampedFieldPVCoordinatesModifier and TypeMethodDescriptiondefault TimeStampedFieldPVCoordinates<T> FieldOrekitStepInterpolator.getPVCoordinates(FieldAbsoluteDate<T> date, Frame frame) Get theFieldPVCoordinatesof the body in the selected frame. -
Uses of TimeStampedFieldPVCoordinates in org.orekit.utils
Methods in org.orekit.utils that return TimeStampedFieldPVCoordinatesModifier and TypeMethodDescription<T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> AngularCoordinates.applyTo(TimeStampedFieldPVCoordinates<T> pv) Apply the rotation to a pv coordinates.FieldAngularCoordinates.applyTo(TimeStampedFieldPVCoordinates<T> pv) Apply the rotation to a pv coordinates.FieldAngularCoordinates.applyTo(TimeStampedPVCoordinates pv) Apply the rotation to a pv coordinates.<S extends CalculusFieldElement<S>>
TimeStampedFieldPVCoordinates<S> AbstractExtendedPositionProvider.getPVCoordinates(FieldAbsoluteDate<S> date, Frame frame) Get the position-velocity-acceleration in the selected frame.<T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> ConstantPositionProvider.getPVCoordinates(FieldAbsoluteDate<T> date, Frame frame) Get the position-velocity-acceleration in the selected frame.default <T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> ExtendedPositionProvider.getPVCoordinates(FieldAbsoluteDate<T> date, Frame frame) Get the position-velocity-acceleration in the selected frame.FieldAbsolutePVCoordinates.getPVCoordinates()Get the TimeStampedFieldPVCoordinates.FieldPVCoordinatesProvider.getPVCoordinates(FieldAbsoluteDate<T> date, Frame frame) Get theFieldPVCoordinatesof the body in the selected frame.<T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> FrameAdapter.getPVCoordinates(FieldAbsoluteDate<T> date, Frame frame) Get the position-velocity-acceleration in the selected frame.ShiftableFieldPVCoordinatesHolder.getPVCoordinates()Getter for the intrinsic position-velocity vector.default TimeStampedFieldPVCoordinates<T> ShiftableFieldPVCoordinatesHolder.getPVCoordinates(Frame outputFrame) Get the position-velocity vector in a specified frame.default TimeStampedFieldPVCoordinates<T> ShiftableFieldPVCoordinatesHolder.getPVCoordinates(FieldAbsoluteDate<T> date, Frame outputFrame) protected TimeStampedFieldPVCoordinates<KK> TimeStampedFieldPVCoordinatesHermiteInterpolator.interpolate(AbstractFieldTimeInterpolator<TimeStampedFieldPVCoordinates<KK>, KK>.InterpolationData interpolationData) Interpolate instance from given interpolation data.TimeStampedFieldPVCoordinates.shiftedBy(double dt) Get a time-shifted state.TimeStampedFieldPVCoordinates.shiftedBy(TimeOffset dt) Get a time-shifted state.Get a time-shifted state.TimeStampedFieldPVCoordinates.toDerivativeStructurePV(int order) TimeStampedPVCoordinates.toDerivativeStructurePV(int order) TimeStampedFieldPVCoordinates.toUnivariateDerivative1PV()TimeStampedPVCoordinates.toUnivariateDerivative1PV()TimeStampedFieldPVCoordinates.toUnivariateDerivative2PV()TimeStampedPVCoordinates.toUnivariateDerivative2PV()Methods in org.orekit.utils with parameters of type TimeStampedFieldPVCoordinatesModifier and TypeMethodDescription<T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T> AngularCoordinates.applyTo(TimeStampedFieldPVCoordinates<T> pv) Apply the rotation to a pv coordinates.FieldAngularCoordinates.applyTo(TimeStampedFieldPVCoordinates<T> pv) Apply the rotation to a pv coordinates.Constructors in org.orekit.utils with parameters of type TimeStampedFieldPVCoordinatesModifierConstructorDescriptionFieldAbsolutePVCoordinates(Frame frame, TimeStampedFieldPVCoordinates<T> pva) Build from frame and TimeStampedFieldPVCoordinates.