Uses of Class
org.orekit.utils.TimeStampedPVCoordinates

Packages that use TimeStampedPVCoordinates

Package	Description
org.orekit.attitudes	This package provides classes to represent simple attitudes.
org.orekit.bodies	This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.
org.orekit.control.indirect.shooting	This package provides routines to solve indirect optimal control within the frame of orbital mechanics, using shooting methods.
org.orekit.control.relative	Package relative provides classes to compute typical maneuvers of relative proximity operations (RPO).
org.orekit.estimation.measurements	The measurements package defines everything that is related to orbit determination measurements.
org.orekit.estimation.measurements.gnss	This package provides methods to handle GNSS measurements.
org.orekit.files.ccsds.ndm.odm	This package contains class managing CCSDS Orbit Data Message.
org.orekit.files.ccsds.ndm.odm.ocm	This package contains class managing CCSDS Orbit Comprehensive Message.
org.orekit.files.ccsds.ndm.odm.oem	This package contains class managing CCSDS Orbit Ephemeris Message.
org.orekit.files.ccsds.ndm.odm.opm	This package contains class managing CCSDS Orbit Parameter Message.
org.orekit.files.general	This package provides interfaces for orbit file representations and corresponding parsers.
org.orekit.files.iirv	This package provides parsers and writers for Improved Interrange Vector (IIRV) messages.
org.orekit.files.ilrs	This package provides parsers for laser ranging data stored in CDR and CPF formats.
org.orekit.files.sp3	This package provides a parser for orbit data stored in SP3 format.
org.orekit.files.stk	This package provides a parser for STK ephemeris files.
org.orekit.forces.gravity	This package provides all gravity-related forces.
org.orekit.frames	This package provides classes to handle frames and transforms between them.
org.orekit.models.earth	This package provides models that simulate certain physical phenomena of Earth and the near-Earth environment.
org.orekit.orbits	This package provides classes to represent orbits.
org.orekit.propagation	Propagation
org.orekit.propagation.analytical	Top level package for analytical propagators.
org.orekit.propagation.relative	Top level package for relative motion propagation.
org.orekit.propagation.relative.clohessywiltshire	This package provides an implementation of the equations of Clohessy and Wiltshire.
org.orekit.propagation.relative.yamanakaankersen	This package provides an implementation of the equations of Yamanaka and Ankersen.
org.orekit.propagation.sampling	This package provides interfaces and classes dealing with step handling during propagation.
org.orekit.utils	This package provides useful objects.

Uses of TimeStampedPVCoordinates in org.orekit.attitudes

Methods in org.orekit.attitudes that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	BodyCenterPointing.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
protected abstract TimeStampedPVCoordinates	GroundPointing.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
TimeStampedPVCoordinates	GroundPointingAttitudeModifier.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
TimeStampedPVCoordinates	LofOffsetPointing.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
TimeStampedPVCoordinates	NadirPointing.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
TimeStampedPVCoordinates	TargetPointing.getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute the target point position/velocity in specified frame.
TimeStampedPVCoordinates	NadirPointing.getTargetPVViaInterpolation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)	Compute target position-velocity-acceleration vector via interpolation.

Methods in org.orekit.attitudes with parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
FieldVector3D<UnivariateDerivative2>	GroundPointTarget.getDerivative2TargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedPVCoordinates pv, Frame frame)	Get a target vector.
default FieldVector3D<UnivariateDerivative2>	TargetProvider.getDerivative2TargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedPVCoordinates pv, Frame frame)	Get a target vector.
Vector3D	GroundPointTarget.getTargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedPVCoordinates pv, Frame frame)	Get a target vector.
default Vector3D	TargetProvider.getTargetDirection(ExtendedPositionProvider sun, OneAxisEllipsoid earth, TimeStampedPVCoordinates pv, Frame frame)	Get a target vector.

Uses of TimeStampedPVCoordinates in org.orekit.bodies

Methods in org.orekit.bodies that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	Ellipse.projectToEllipse(TimeStampedPVCoordinates pv)	Project position-velocity-acceleration on an ellipse.
TimeStampedPVCoordinates	BodyShape.projectToGround(TimeStampedPVCoordinates pv, Frame frame)	Project a moving point to the ground.
TimeStampedPVCoordinates	OneAxisEllipsoid.projectToGround(TimeStampedPVCoordinates pv, Frame frame)	Project a moving point to the ground.

Methods in org.orekit.bodies with parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	Ellipse.projectToEllipse(TimeStampedPVCoordinates pv)	Project position-velocity-acceleration on an ellipse.
TimeStampedPVCoordinates	BodyShape.projectToGround(TimeStampedPVCoordinates pv, Frame frame)	Project a moving point to the ground.
TimeStampedPVCoordinates	OneAxisEllipsoid.projectToGround(TimeStampedPVCoordinates pv, Frame frame)	Project a moving point to the ground.

Uses of TimeStampedPVCoordinates in org.orekit.control.indirect.shooting

Methods in org.orekit.control.indirect.shooting that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
protected TimeStampedPVCoordinates	AbstractFixedBoundaryCartesianSingleShooting.getTerminalCartesianState()	Getter for the target terminal Cartesian state vector.

Uses of TimeStampedPVCoordinates in org.orekit.control.relative

Methods in org.orekit.control.relative that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
default TimeStampedPVCoordinates	RPO.computeNaturalCircumnavigationInjectionCircular(AbsoluteDate startDate, double distanceAlongVBar, double inclination, double 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 TimeStampedPVCoordinates

Modifier and Type	Method	Description
default List<TimeStampedPVCoordinates>	RPO.computeForcedCircularMotionWaypoints(AbsoluteDate startDate, Vector3D centerOffset, double radius, double inclination, double raan, double orbitDuration, int pointsOnOrbit, int numberOfRevolutions, double startAngle, boolean retrograde)	Computes the waypoints to perform a forced circular orbit.
default List<TimeStampedPVCoordinates>	RPO.computeForcedLinearWaypoints(TimeStampedPVCoordinates initialPVT, TimeStampedPVCoordinates finalPVT, int numberOfPoints)	Computes the waypoints along the linear path.
List<TimeStampedPVCoordinates>	RPO.computeTeardropWaypoints(AbsoluteDate injectionDate, Orbit targetOrbit, double turnAroundDistance, double maneuverDistance, int numberOfTeardrops)	Computes teardrop waypoints.
List<TimeStampedPVCoordinates>	TeardropCircularWaypointCalculator.computeTearDropWaypoints(AbsoluteDate 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 TimeStampedPVCoordinates

Modifier and Type	Method	Description
default List<TimeStampedPVCoordinates>	RPO.computeForcedLinearWaypoints(TimeStampedPVCoordinates initialPVT, TimeStampedPVCoordinates finalPVT, int numberOfPoints)	Computes the waypoints along the linear path.

Method parameters in org.orekit.control.relative with type arguments of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
List<RelativeManeuver>	RPO.computeForcedManeuvers(List<TimeStampedPVCoordinates> waypoints, Vector3D initialVelocity, Orbit targetOrbit, RelativeProvider provider)	Compute relative maneuvers to realize a forced trajectory defined by the waypoints (ForcedLinear/ForcedCircular).
List<RelativeManeuver>	RPO.computeTeardropManeuvers(List<TimeStampedPVCoordinates> waypoints, RelativeProvider relativeProvider)	Computes the relative maneuvers of the teardrop relative orbit in the RPOModel Local Orbital Frame.

Uses of TimeStampedPVCoordinates in org.orekit.estimation.measurements

Methods in org.orekit.estimation.measurements that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates[]	EstimatedMeasurementBase.getParticipants()	Get the coordinates of the measurements participants in signal travel order.

Methods in org.orekit.estimation.measurements with parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
static PVCoordinatesProvider	AbstractParticipant.extractPVCoordinatesProvider(SpacecraftState templateState, TimeStampedPVCoordinates pvCoordinates)	Create PV provider from position-velocity-acceleration vector and template state.

Constructors in org.orekit.estimation.measurements with parameters of type TimeStampedPVCoordinates

Modifier	Constructor	Description
	EstimatedMeasurement(T observedMeasurement, int iteration, int count, SpacecraftState[] states, TimeStampedPVCoordinates[] participants)	Simple constructor.
	EstimatedMeasurementBase(T observedMeasurement, int iteration, int count, SpacecraftState[] states, TimeStampedPVCoordinates[] participants)	Simple constructor.

Uses of TimeStampedPVCoordinates in org.orekit.estimation.measurements.gnss

Methods in org.orekit.estimation.measurements.gnss with parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
void	AbstractWindUp.cacheAngularWindUp(TimeStampedPVCoordinates[] participants, Rotation receiverToInert, Rotation emitterToInert)	Cache angular wind-up.

Uses of TimeStampedPVCoordinates in org.orekit.files.ccsds.ndm.odm

Methods in org.orekit.files.ccsds.ndm.odm that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	StateVector.toTimeStampedPVCoordinates()	Convert to TimeStampedPVCoordinates.

Uses of TimeStampedPVCoordinates in org.orekit.files.ccsds.ndm.odm.ocm

Methods in org.orekit.files.ccsds.ndm.odm.ocm with type parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
<C extends TimeStampedPVCoordinates, S extends EphemerisFile.EphemerisSegment<C>> void	EphemerisOcmWriter.write(Appendable appendable, EphemerisFile<C,S> ephemerisFile)	Write the passed in EphemerisFile using the passed in Appendable.

Methods in org.orekit.files.ccsds.ndm.odm.ocm that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	OrbitElementsType.toCartesian(AbsoluteDate date, double[] elements, OneAxisEllipsoid body, double mu)	Convert to Cartesian coordinates.
TimeStampedPVCoordinates	TrajectoryState.toCartesian(OneAxisEllipsoid body, double mu)	Convert to Cartesian coordinates.

Methods in org.orekit.files.ccsds.ndm.odm.ocm that return types with arguments of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
List<TimeStampedPVCoordinates>	TrajectoryStateHistory.getCoordinates()	Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().

Methods in org.orekit.files.ccsds.ndm.odm.ocm with parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
double[]	OrbitElementsType.toRawElements(TimeStampedPVCoordinates pv, Frame frame, OneAxisEllipsoid body, double mu)	Convert to raw elements array.

Uses of TimeStampedPVCoordinates in org.orekit.files.ccsds.ndm.odm.oem

Methods in org.orekit.files.ccsds.ndm.odm.oem with type parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
<C extends TimeStampedPVCoordinates, S extends EphemerisFile.EphemerisSegment<C>> void	EphemerisOemWriter.write(Appendable appendable, EphemerisFile<C,S> ephemerisFile)	Write the passed in EphemerisFile using the passed in Appendable.
<C extends TimeStampedPVCoordinates, S extends EphemerisFile.EphemerisSegment<C>> void	EphemerisOemWriter.writeSegment(Generator generator, S segment)	Write one segment.

Methods in org.orekit.files.ccsds.ndm.odm.oem that return types with arguments of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
List<TimeStampedPVCoordinates>	OemData.getCoordinates()	Get an unmodifiable view of the data points.
List<TimeStampedPVCoordinates>	OemSegment.getCoordinates()	Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
List<TimeStampedPVCoordinates>	OemData.getEphemeridesDataLines()	Get the list of Ephemerides data lines.

Methods in org.orekit.files.ccsds.ndm.odm.oem with parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
boolean	OemData.addData(TimeStampedPVCoordinates data, boolean hasAcceleration)	Add a data point.

Uses of TimeStampedPVCoordinates in org.orekit.files.ccsds.ndm.odm.opm

Methods in org.orekit.files.ccsds.ndm.odm.opm that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	Opm.getPVCoordinates()	Get the position/velocity coordinates contained in the OPM.

Uses of TimeStampedPVCoordinates in org.orekit.files.general

Classes in org.orekit.files.general with type parameters of type TimeStampedPVCoordinates

Modifier and Type	Interface	Description
interface	EphemerisFile<C extends TimeStampedPVCoordinates,S extends EphemerisFile.EphemerisSegment<C>>	An interface for accessing the data stored in an ephemeris file and using the data to create a working Propagator.
static interface	EphemerisFile.EphemerisSegment<C extends TimeStampedPVCoordinates>	A segment of an ephemeris for a satellite.
static interface	EphemerisFile.SatelliteEphemeris<C extends TimeStampedPVCoordinates,S extends EphemerisFile.EphemerisSegment<C>>	Contains the information about a single satellite from an EphemerisFile.
class	EphemerisSegmentPropagator<C extends TimeStampedPVCoordinates>	A Propagator based on a EphemerisFile.EphemerisSegment.

Methods in org.orekit.files.general with type parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
<C extends TimeStampedPVCoordinates, S extends EphemerisFile.EphemerisSegment<C>> void	EphemerisFileWriter.write(Appendable writer, EphemerisFile<C,S> ephemerisFile)	Write the passed in EphemerisFile using the passed in Appendable.
default <C extends TimeStampedPVCoordinates, S extends EphemerisFile.EphemerisSegment<C>> void	EphemerisFileWriter.write(String outputFilePath, EphemerisFile<C,S> ephemerisFile)	Write the passed in EphemerisFile to a file at the output path specified.

Methods in org.orekit.files.general that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	EphemerisSegmentPropagator.getPVCoordinates(AbsoluteDate date, Frame frame)

Methods in org.orekit.files.general that return types with arguments of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
List<TimeStampedPVCoordinates>	OrekitEphemerisFile.OrekitEphemerisSegment.getCoordinates()	Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().

Constructor parameters in org.orekit.files.general with type arguments of type TimeStampedPVCoordinates

Modifier	Constructor	Description
	OrekitEphemerisSegment(List<TimeStampedPVCoordinates> coordinates, Frame frame, double mu, int interpolationSamples)	constructor for OrekitEphemerisSegment.

Uses of TimeStampedPVCoordinates in org.orekit.files.iirv

Methods in org.orekit.files.iirv with type parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
<C extends TimeStampedPVCoordinates> IIRVEphemerisFile	IIRVBuilder.buildEphemerisFile(List<C> timeStampedPVCoordinates)	Constructs an IIRVEphemerisFile from the inputted list of TimeStampedPVCoordinates, inferring the start year from the first coordinate's AbsoluteDate.
<C extends TimeStampedPVCoordinates> IIRVMessage	IIRVBuilder.buildIIRVMessage(List<C> timeStampedPVCoordinates)	Constructs an IIRVMessage where each IIRVVector in initialized from the inputted list of TimeStampedPVCoordinates.
<C extends TimeStampedPVCoordinates, S extends EphemerisFile.EphemerisSegment<C>> void	IIRVFileWriter.write(Appendable writer, EphemerisFile<C,S> ephemerisFile)	Write the passed in EphemerisFile using the passed in Appendable.

Methods in org.orekit.files.iirv that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	IIRVVector.getTimeStampedPVCoordinates(int year)	Gets the state vector and time data as a TimeStampedPVCoordinates instance.

Methods in org.orekit.files.iirv that return types with arguments of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
List<TimeStampedPVCoordinates>	IIRVSegment.getCoordinates()	Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().

Methods in org.orekit.files.iirv with parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
IIRVVector	IIRVBuilder.buildVector(TimeStampedPVCoordinates timeStampedPVCoordinates)	Constructs an IIRV vector using the configured parameters, with position, velocity, and time variables derived from instances of TimeStampedPVCoordinates and AbsoluteDate.

Uses of TimeStampedPVCoordinates in org.orekit.files.ilrs

Subclasses of TimeStampedPVCoordinates in org.orekit.files.ilrs

Modifier and Type	Class	Description
static class	CPF.CPFCoordinate	A single record of position and possibility velocity in an SP3 file.

Methods in org.orekit.files.ilrs with type parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
<C extends TimeStampedPVCoordinates, S extends EphemerisFile.EphemerisSegment<C>> void	CPFWriter.write(Appendable writer, EphemerisFile<C,S> ephemerisFile)	Write the passed in EphemerisFile using the passed in Appendable.

Methods in org.orekit.files.ilrs with parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
void	StreamingCpfWriter.Segment.writeEphemerisLine(TimeStampedPVCoordinates pv)	Write ephemeris lines.

Uses of TimeStampedPVCoordinates in org.orekit.files.sp3

Subclasses of TimeStampedPVCoordinates in org.orekit.files.sp3

Modifier and Type	Class	Description
class	SP3Coordinate	A single record of position clock and possibly derivatives in an SP3 file.

Uses of TimeStampedPVCoordinates in org.orekit.files.stk

Methods in org.orekit.files.stk that return types with arguments of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
List<TimeStampedPVCoordinates>	STKEphemerisFile.STKEphemerisSegment.getCoordinates()

Constructor parameters in org.orekit.files.stk with type arguments of type TimeStampedPVCoordinates

Modifier	Constructor	Description
	STKEphemerisSegment(double mu, Frame frame, int interpolationSamples, CartesianDerivativesFilter cartesianDerivativesFilter, List<TimeStampedPVCoordinates> timeStampedPVCoordinates)	Constructs a STKEphemerisFile.STKEphemerisSegment instance.

Uses of TimeStampedPVCoordinates in org.orekit.forces.gravity

Methods in org.orekit.forces.gravity that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
protected TimeStampedPVCoordinates	AbstractBodyAttraction.getBodyPVCoordinates(AbsoluteDate date, Frame frame)	Get the body's position-velocity-acceleration vector.

Uses of TimeStampedPVCoordinates in org.orekit.frames

Methods in org.orekit.frames that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	TopocentricFrame.getPVCoordinates(AbsoluteDate date, Frame frame)	Get the PVCoordinates of the body in the selected frame.
default TimeStampedPVCoordinates	KinematicTransform.transformOnlyPV(TimeStampedPVCoordinates pv)	Transform TimeStampedPVCoordinates, without the acceleration vector.
TimeStampedPVCoordinates	Transform.transformPVCoordinates(TimeStampedPVCoordinates pv)	Transform TimeStampedPVCoordinates including kinematic effects.

Methods in org.orekit.frames with parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
default TimeStampedPVCoordinates	KinematicTransform.transformOnlyPV(TimeStampedPVCoordinates pv)	Transform TimeStampedPVCoordinates, without the acceleration vector.
TimeStampedFieldPVCoordinates<T>	FieldTransform.transformPVCoordinates(TimeStampedPVCoordinates pv)	Transform TimeStampedPVCoordinates including kinematic effects.
TimeStampedPVCoordinates	Transform.transformPVCoordinates(TimeStampedPVCoordinates pv)	Transform TimeStampedPVCoordinates including kinematic effects.

Uses of TimeStampedPVCoordinates in org.orekit.models.earth

Methods in org.orekit.models.earth that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	Geoid.projectToGround(TimeStampedPVCoordinates pv, Frame frame)

Methods in org.orekit.models.earth with parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	Geoid.projectToGround(TimeStampedPVCoordinates pv, Frame frame)

Uses of TimeStampedPVCoordinates in org.orekit.orbits

Methods in org.orekit.orbits that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	Orbit.getPVCoordinates()	Get the TimeStampedPVCoordinates in definition frame.
protected TimeStampedPVCoordinates	CartesianOrbit.initPVCoordinates()	Compute the position/velocity coordinates from the canonical parameters.
protected TimeStampedPVCoordinates	CircularOrbit.initPVCoordinates()	Compute the position/velocity coordinates from the canonical parameters.
protected TimeStampedPVCoordinates	EquinoctialOrbit.initPVCoordinates()	Compute the position/velocity coordinates from the canonical parameters.
protected TimeStampedPVCoordinates	KeplerianOrbit.initPVCoordinates()	Compute the position/velocity coordinates from the canonical parameters.
protected abstract TimeStampedPVCoordinates	Orbit.initPVCoordinates()	Compute the position/velocity coordinates from the canonical parameters.

Constructors in org.orekit.orbits with parameters of type TimeStampedPVCoordinates

Modifier	Constructor	Description
	CartesianOrbit(TimeStampedPVCoordinates pvaCoordinates, Frame frame, double mu)	Constructor from Cartesian parameters.
	CircularOrbit(TimeStampedPVCoordinates pvCoordinates, Frame frame, double mu)	Constructor from Cartesian parameters.
	EquinoctialOrbit(TimeStampedPVCoordinates pvCoordinates, Frame frame, double mu)	Constructor from Cartesian parameters.
	KeplerianOrbit(TimeStampedPVCoordinates pvCoordinates, Frame frame, double mu)	Constructor from Cartesian parameters.
protected	Orbit(TimeStampedPVCoordinates pvCoordinates, Frame frame, double mu)	Set the orbit from Cartesian parameters.

Uses of TimeStampedPVCoordinates in org.orekit.propagation

Methods in org.orekit.propagation that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
default TimeStampedPVCoordinates	Propagator.getPVCoordinates(AbsoluteDate date, Frame frame)	Get the PVCoordinates of the body in the selected frame.
TimeStampedPVCoordinates	SpacecraftState.getPVCoordinates()	Get the TimeStampedPVCoordinates in orbit definition frame.
TimeStampedPVCoordinates	SpacecraftState.getPVCoordinates(Frame outputFrame)	Get the TimeStampedPVCoordinates in given output frame.

Uses of TimeStampedPVCoordinates in org.orekit.propagation.analytical

Methods in org.orekit.propagation.analytical that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	AggregateBoundedPropagator.getPVCoordinates(AbsoluteDate date, Frame frame)

Uses of TimeStampedPVCoordinates in org.orekit.propagation.relative

Methods in org.orekit.propagation.relative that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	RelativeProvider.extractChaserPVT(SpacecraftState targetState)	Extracts the chaser's PVT in the target LOF from the given target SpacecraftState.
default TimeStampedPVCoordinates	RelativeProvider.extractChaserPVT(SpacecraftState targetState, Frame outputFrame)	Extracts the chaser's PVT from the given target SpacecraftState and converts it to the desired output frame.
TimeStampedPVCoordinates	AbstractRelativeProvider.getInitialChaserPVTLof()
TimeStampedPVCoordinates	RelativeProvider.getInitialChaserPVTLof()	Get the initial TimeStampedPVCoordinates of the chaser in the Local Orbital Frame of the target.
TimeStampedPVCoordinates	TwoImpulseTransfer.getPvt1()	Get the PVT of the chaser just after the first maneuver.
TimeStampedPVCoordinates	TwoImpulseTransfer.getPvt1(Frame outputFrame)	Get PVT of the chaser just after the first maneuver.
TimeStampedPVCoordinates	TwoImpulseTransfer.getPvt1BeforeMan()	Returns the PVT of the chaser just before the injection maneuver into the transfer orbit.
TimeStampedPVCoordinates	TwoImpulseTransfer.getPvt2()	Get PVT of the chaser just before the second maneuver.
TimeStampedPVCoordinates	TwoImpulseTransfer.getPvt2(Frame outputFrame)	Get PVT of the chaser just before the second maneuver.
TimeStampedPVCoordinates	TwoImpulseTransfer.getPvt2AfterMan()	Returns the PVT of the chaser just after the velocity-synchronization maneuver into the target orbit.

Methods in org.orekit.propagation.relative with parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
static TwoImpulseTransfer	TwoImpulseTransfer.fromPVTAndVelocities(TimeStampedPVCoordinates pvt1BeforeMan, Vector3D v1AfterMan, TimeStampedPVCoordinates pvt2AfterMan, Vector3D v2BeforeMan, Frame frame)	Creates a new TwoImpulseTransfer object 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).
void	AbstractRelativeProvider.setInitialChaserPVTLof(TimeStampedPVCoordinates initialChaserPVTLof)	Set the initial TimeStampedPVCoordinates of the chaser in the Local Orbital Frame of the target.
void	RelativeProvider.setInitialChaserPVTLof(TimeStampedPVCoordinates 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 TimeStampedPVCoordinates

Modifier	Constructor	Description
	AbstractRelativeProvider(Orbit targetOrbit, TimeStampedPVCoordinates initialChaserPVTLof, String additionalEquationsName, LOF lof)	Builds a new RelativeProvider object from the target orbit and an initial PVT of the chaser.
	AbstractRelativeProvider(Orbit targetOrbit, TimeStampedPVCoordinates 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.
	TwoImpulseTransfer(TimeStampedPVCoordinates pvt1, TimeStampedPVCoordinates pvt2, Vector3D deltaV1, Vector3D deltaV2, Frame frame)	Creates a new TwoImpulseTransfer object from the given PVT and ΔV vectors.

Uses of TimeStampedPVCoordinates in org.orekit.propagation.relative.clohessywiltshire

Methods in org.orekit.propagation.relative.clohessywiltshire that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	ClohessyWiltshireProvider.extractChaserPVT(SpacecraftState targetState)	Extracts the chaser's PVT in the target LOF from the given target SpacecraftState.
TimeStampedPVCoordinates	ClohessyWiltshireMatrices.transform(TimeStampedPVCoordinates 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 TimeStampedPVCoordinates

Modifier and Type	Method	Description
static TwoImpulseTransfer	ClohessyWiltshireRendezVous.computeRendezVous(TimeStampedPVCoordinates chaserPVTInitial, TimeStampedPVCoordinates chaserPVTFinal, Frame chaserPVFrame, Orbit targetOrbit)	Computes a two-impulse transfer between an initial and final positions using the Clohessy-Wiltshire closed-form solution.
TimeStampedPVCoordinates	ClohessyWiltshireMatrices.transform(TimeStampedPVCoordinates 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 TimeStampedPVCoordinates

Modifier	Constructor	Description
	ClohessyWiltshireProvider(Orbit targetOrbit, TimeStampedPVCoordinates initialChaserPVTLof)	Builds a new ClohessyWiltshireProvider object from the target orbit and an initial PVT of the chaser.
	ClohessyWiltshireProvider(Orbit targetOrbit, TimeStampedPVCoordinates initialChaserPVTLof, String additionalEquationsName)	Builds a new ClohessyWiltshireProvider object from the target orbit and an initial PVT of the chaser.
	ClohessyWiltshireProvider(Orbit targetOrbit, TimeStampedPVCoordinates 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.
	ClohessyWiltshireProvider(Orbit targetOrbit, TimeStampedPVCoordinates 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 TimeStampedPVCoordinates in org.orekit.propagation.relative.yamanakaankersen

Methods in org.orekit.propagation.relative.yamanakaankersen that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	YamanakaAnkersenProvider.extractChaserPVT(SpacecraftState targetState)	Extracts the chaser's PVT in the target LOF from the given target SpacecraftState.
TimeStampedPVCoordinates	YamanakaAnkersenMatrices.transform(TimeStampedPVCoordinates pvt, double initialTrueAnomaly, double trueAnomaly, double eccentricity, double sma, double 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 TimeStampedPVCoordinates

Modifier and Type	Method	Description
static TwoImpulseTransfer	YamanakaAnkersenRendezVous.computeRendezVous(TimeStampedPVCoordinates chaserPVTInitial, TimeStampedPVCoordinates chaserPVTFinal, Frame chaserPVFrame, Orbit targetOrbit, Propagator propagator)	Computes a two-impulse transfer between an initial and final positions using the Yamanaka-Ankersen closed-form solution.
TimeStampedPVCoordinates	YamanakaAnkersenMatrices.transform(TimeStampedPVCoordinates pvt, double initialTrueAnomaly, double trueAnomaly, double eccentricity, double sma, double 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 TimeStampedPVCoordinates

Modifier	Constructor	Description
	YamanakaAnkersenProvider(Orbit targetOrbit, TimeStampedPVCoordinates initialChaserPVTLof)	Builds a new YamanakaAnkersenProvider object from the target orbit and an all-zero PVT for the chaser.
	YamanakaAnkersenProvider(Orbit targetOrbit, TimeStampedPVCoordinates initialChaserPVTLof, String additionalEquationsName)	Builds a new YamanakaAnkersenProvider object from the target orbit and an initial PVT of the chaser.
	YamanakaAnkersenProvider(Orbit targetOrbit, TimeStampedPVCoordinates 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.
	YamanakaAnkersenProvider(Orbit targetOrbit, TimeStampedPVCoordinates 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 TimeStampedPVCoordinates in org.orekit.propagation.sampling

Methods in org.orekit.propagation.sampling that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
default TimeStampedPVCoordinates	OrekitStepInterpolator.getPVCoordinates(AbsoluteDate date, Frame frame)	Get the PVCoordinates of the body in the selected frame.

Uses of TimeStampedPVCoordinates in org.orekit.utils

Methods in org.orekit.utils that return TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	AngularCoordinates.applyTo(TimeStampedPVCoordinates pv)	Apply the rotation to a pv coordinates.
TimeStampedPVCoordinates	AbsolutePVCoordinates.getPVCoordinates()	Get the TimeStampedPVCoordinates.
TimeStampedPVCoordinates	AbstractExtendedPositionProvider.getPVCoordinates(AbsoluteDate date, Frame frame)	Get the PVCoordinates of the body in the selected frame.
TimeStampedPVCoordinates	AggregatedPVCoordinatesProvider.getPVCoordinates(AbsoluteDate date, Frame frame)
TimeStampedPVCoordinates	AggregatedPVCoordinatesProvider.InvalidPVProvider.getPVCoordinates(AbsoluteDate date, Frame frame)
TimeStampedPVCoordinates	ConstantPositionProvider.getPVCoordinates(AbsoluteDate date, Frame frame)	Get the PVCoordinates of the body in the selected frame.
default TimeStampedPVCoordinates	ExtendedPositionProvider.getPVCoordinates(AbsoluteDate date, Frame frame)	Get the PVCoordinates of the body in the selected frame.
TimeStampedPVCoordinates	FrameAdapter.getPVCoordinates(AbsoluteDate date, Frame frame)	Get the PVCoordinates of the body in the selected frame.
TimeStampedPVCoordinates	PVCoordinatesProvider.getPVCoordinates(AbsoluteDate date, Frame frame)	Get the PVCoordinates of the body in the selected frame.
TimeStampedPVCoordinates	ShiftablePVCoordinatesHolder.getPVCoordinates()	Getter for the intrinsic position-velocity vector.
default TimeStampedPVCoordinates	ShiftablePVCoordinatesHolder.getPVCoordinates(Frame outputFrame)	Get the TimeStampedPVCoordinates in a specified frame.
default TimeStampedPVCoordinates	ShiftablePVCoordinatesHolder.getPVCoordinates(AbsoluteDate date, Frame outputFrame)
protected TimeStampedPVCoordinates	TimeStampedPVCoordinatesHermiteInterpolator.interpolate(AbstractTimeInterpolator<TimeStampedPVCoordinates>.InterpolationData interpolationData)	Interpolate instance from given interpolation data.
TimeStampedPVCoordinates	TimeStampedPVCoordinates.shiftedBy(double dt)	Get a time-shifted state.
TimeStampedPVCoordinates	TimeStampedPVCoordinates.shiftedBy(TimeOffset dt)	Get a time-shifted state.
TimeStampedPVCoordinates	TimeStampedFieldPVCoordinates.toTimeStampedPVCoordinates()	Convert to a constant position-velocity.

Methods in org.orekit.utils with parameters of type TimeStampedPVCoordinates

Modifier and Type	Method	Description
TimeStampedPVCoordinates	AngularCoordinates.applyTo(TimeStampedPVCoordinates pv)	Apply the rotation to a pv coordinates.
TimeStampedFieldPVCoordinates<T>	FieldAngularCoordinates.applyTo(TimeStampedPVCoordinates pv)	Apply the rotation to a pv coordinates.

Constructors in org.orekit.utils with parameters of type TimeStampedPVCoordinates

Modifier	Constructor	Description
	AbsolutePVCoordinates(Frame frame, TimeStampedPVCoordinates pva)	Build from frame and TimeStampedPVCoordinates.
	TimeStampedFieldPVCoordinates(Field<T> field, TimeStampedPVCoordinates pv)	Constructor from Field and TimeStampedPVCoordinates.