Uses of Class
org.orekit.utils.PVCoordinates

Packages that use PVCoordinates

Package	Description
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.boundary	This package provides classes relative to the boundary conditions for indirect shooting.
org.orekit.estimation.iod	This package provides initial orbit determination methods.
org.orekit.estimation.measurements.model	This package contains physical models for measurement prediction.
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.frames	This package provides classes to handle frames and transforms between them.
org.orekit.frames.encounter	Package specific to encounter local orbital frame.
org.orekit.orbits	This package provides classes to represent orbits.
org.orekit.orbits.cr3bp	This package provides classes to compute orbits in the three-body problem.
org.orekit.propagation.analytical.gnss	This package provides classes to propagate GNSS orbits.
org.orekit.propagation.analytical.intelsat	This package provides classes to propagate Intelsat's 11 elements.
org.orekit.propagation.analytical.tle	This package provides classes to read and extrapolate tle's.
org.orekit.propagation.events	This package provides interfaces and classes dealing with events occurring during propagation.
org.orekit.propagation.events.handlers	This package provides an interface and classes dealing with events occurrence only.
org.orekit.ssa.collision.shorttermencounter.probability.twod	Package specific to calculus assuming a 2D short-term encounter model.
org.orekit.utils	This package provides useful objects.

Uses of PVCoordinates in org.orekit.bodies

Methods in org.orekit.bodies that return PVCoordinates

Modifier and Type	Method	Description
PVCoordinates	JPLEphemeridesLoader.RawPVProvider.getRawPV(AbsoluteDate date)	Get the position-velocity at date.

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

Modifier and Type	Method	Description
FieldGeodeticPoint<UnivariateDerivative2>	OneAxisEllipsoid.transform(PVCoordinates point, Frame frame, AbsoluteDate date)	Transform a Cartesian point to a surface-relative point.

Uses of PVCoordinates in org.orekit.control.indirect.shooting.boundary

Methods in org.orekit.control.indirect.shooting.boundary with parameters of type PVCoordinates

Modifier and Type	Method	Description
boolean	CartesianBoundaryConditionChecker.isConverged(PVCoordinates targetPV, PVCoordinates actualPV)	Asserts convergence.
boolean	NormBasedCartesianConditionChecker.isConverged(PVCoordinates targetPV, PVCoordinates actualPV)	Asserts convergence.

Uses of PVCoordinates in org.orekit.estimation.iod

Methods in org.orekit.estimation.iod with parameters of type PVCoordinates

Modifier and Type	Method	Description
Orbit	IodLaplace.estimate(Frame outputFrame, PVCoordinates obsPva, AbsoluteDate obsDate1, Vector3D los1, AbsoluteDate obsDate2, Vector3D los2, AbsoluteDate obsDate3, Vector3D los3)	Estimate orbit from three line of sight angles at the same location.

Uses of PVCoordinates in org.orekit.estimation.measurements.model

Methods in org.orekit.estimation.measurements.model with parameters of type PVCoordinates

Modifier and Type	Method	Description
double	TwoLeggedRangeRateModel.value(Frame frame, PVCoordinates receiverPV, AbsoluteDate receptionDate, PVCoordinatesProvider relay, AbsoluteDate approxRelayDate, PVCoordinatesProvider emitter, AbsoluteDate approxEmissionDate)	Compute measurement.
double	TwoLeggedRangeRateModel.value(Frame frame, PVCoordinates receiverPV, AbsoluteDate receptionDate, PVCoordinatesProvider relay, PVCoordinatesProvider emitter)	Compute measurement without guess.

Uses of PVCoordinates in org.orekit.files.iirv

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

Modifier and Type	Method	Description
PVCoordinates	IIRVVector.getPVCoordinates()	Gets the state vector as a PVCoordinates instance.

Uses of PVCoordinates in org.orekit.files.ilrs

Subclasses of PVCoordinates 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.

Uses of PVCoordinates in org.orekit.files.sp3

Subclasses of PVCoordinates 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 PVCoordinates in org.orekit.frames

Methods in org.orekit.frames that return PVCoordinates

Modifier and Type	Method	Description
PVCoordinates	Transform.getCartesian()	Get the underlying elementary Cartesian part.
default PVCoordinates	KinematicTransform.transformOnlyPV(PVCoordinates pv)	Transform PVCoordinates, without the acceleration vector.
PVCoordinates	Transform.transformPVCoordinates(PVCoordinates pva)	Transform PVCoordinates including kinematic effects.

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

Modifier and Type	Method	Description
double	TopocentricFrame.getRangeRate(PVCoordinates extPV, Frame frame, AbsoluteDate date)	Get the range rate of a point with regards to the topocentric frame center point.
static KinematicTransform	KinematicTransform.of(AbsoluteDate date, PVCoordinates pvCoordinates)	Create a new kinematic transform from a translation and its rate.
static KinematicTransform	KinematicTransform.of(AbsoluteDate date, PVCoordinates pvCoordinates, Rotation rotation, Vector3D rotationRate)	Create a new kinematic transform from a translation and rotation.
Rotation	LocalMagneticFieldFrame.rotationFromInertial(AbsoluteDate date, PVCoordinates pv)	Get the rotation from inertial frame to local orbital frame.
Rotation	LOF.rotationFromInertial(AbsoluteDate date, PVCoordinates pv)	Get the rotation from inertial frame to local orbital frame.
Rotation	LOFType.rotationFromInertial(AbsoluteDate date, PVCoordinates pv)	Get the rotation from inertial frame to local orbital frame.
abstract Rotation	LOFType.rotationFromInertial(PVCoordinates pv)	Get the rotation from inertial frame to local orbital frame.
default Rotation	LOF.rotationFromLOF(LOF fromLOF, AbsoluteDate date, PVCoordinates pv)	Get the rotation from input local orbital frame to the instance.
Rotation	LOFType.rotationFromLOF(LOFType fromLOF, PVCoordinates pv)	Get the rotation from input local orbital frame to the instance.
static Rotation	LOF.rotationFromLOFInToLOFOut(LOF in, LOF out, AbsoluteDate date, PVCoordinates pv)	Get the rotation from input to output local orbital frame.
default Rotation	LOF.rotationToInertial(AbsoluteDate date, PVCoordinates pv)	Get the rotation from local orbital frame to inertial frame.
Rotation	LOFType.rotationToInertial(PVCoordinates pv)	Get the rotation from local orbital frame to inertial frame.
default Transform	LOF.transformFromInertial(AbsoluteDate date, PVCoordinates pv)	Get the transform from an inertial frame defining position-velocity and the local orbital frame.
default Transform	LOF.transformFromLOF(LOF fromLOF, AbsoluteDate date, PVCoordinates pv)	Get the rotation from input local orbital frame to the instance.
static Transform	LOF.transformFromLOFInToLOFOut(LOF in, LOF out, AbsoluteDate date, PVCoordinates pv)	Get the transform from input to output local orbital frame.
default PVCoordinates	KinematicTransform.transformOnlyPV(PVCoordinates pv)	Transform PVCoordinates, without the acceleration vector.
FieldPVCoordinates<T>	FieldTransform.transformPVCoordinates(PVCoordinates pv)	Transform TimeStampedPVCoordinates including kinematic effects.
PVCoordinates	Transform.transformPVCoordinates(PVCoordinates pva)	Transform PVCoordinates including kinematic effects.
default Transform	LOF.transformToInertial(AbsoluteDate date, PVCoordinates pv)	Get the transform from the local orbital frame to the inertial frame.

Constructors in org.orekit.frames with parameters of type PVCoordinates

Modifier	Constructor	Description
	Transform(AbsoluteDate date, PVCoordinates cartesian)	Build a translation transform, with its first time derivative.
	Transform(AbsoluteDate date, PVCoordinates cartesian, AngularCoordinates angular)	Build a transform from its primitive operations.

Uses of PVCoordinates in org.orekit.frames.encounter

Methods in org.orekit.frames.encounter that return PVCoordinates

Modifier and Type	Method	Description
PVCoordinates	AbstractEncounterLOF.getOther()	Get the normal version of other's position and velocity coordinates.
PVCoordinates	EncounterLOF.getOther()	Get other's position and velocity coordinates.

Methods in org.orekit.frames.encounter with parameters of type PVCoordinates

Modifier and Type	Method	Description
abstract EncounterLOF	EncounterLOFType.getFrame(PVCoordinates other)	Get encounter local orbital frame associated to this enum.
Rotation	AbstractEncounterLOF.rotationFromInertial(PVCoordinates origin)	Get the rotation from inertial to this encounter local orbital frame.
Rotation	DefaultEncounterLOF.rotationFromInertial(PVCoordinates origin, PVCoordinates other)	Get the rotation from inertial to this encounter local orbital frame.
default Rotation	EncounterLOF.rotationFromInertial(AbsoluteDate date, PVCoordinates pv)	Get the rotation from inertial frame to local orbital frame.
default Rotation	EncounterLOF.rotationFromInertial(PVCoordinates origin)	Get the rotation from inertial to this encounter local orbital frame.
Rotation	EncounterLOF.rotationFromInertial(PVCoordinates origin, PVCoordinates other)	Get the rotation from inertial to this encounter local orbital frame.
Rotation	ValsecchiEncounterFrame.rotationFromInertial(PVCoordinates origin, PVCoordinates other)	Get the rotation from inertial to this encounter local orbital frame.

Constructors in org.orekit.frames.encounter with parameters of type PVCoordinates

Modifier	Constructor	Description
protected	AbstractEncounterLOF(PVCoordinates other)	Constructor with PVCoordinates.
	DefaultEncounterLOF(PVCoordinates other)	Constructor.
	ValsecchiEncounterFrame(PVCoordinates other)	Constructor.

Uses of PVCoordinates in org.orekit.orbits

Methods in org.orekit.orbits that return PVCoordinates

Modifier and Type	Method	Description
static PVCoordinates	KeplerianMotionCartesianUtility.predictPositionVelocity(double dt, Vector3D position, Vector3D velocity, double mu)	Method to propagate position and velocity according to Keplerian dynamics.
protected PVCoordinates	Orbit.shiftNonKeplerian(PVCoordinates keplerianShifted, double dt)	Compute corrected shift from non-Keplerian part.
PVCoordinates	KeplerianParametersConverter.toCartesian(KeplerianParameters elements)	Convert Keplerian elements to Cartesian coordinates.

Methods in org.orekit.orbits with parameters of type PVCoordinates

Modifier and Type	Method	Description
protected static boolean	Orbit.hasNonKeplerianAcceleration(PVCoordinates pva, double mu)	Check if Cartesian coordinates include non-Keplerian acceleration.
protected PVCoordinates	Orbit.shiftNonKeplerian(PVCoordinates keplerianShifted, double dt)	Compute corrected shift from non-Keplerian part.
KeplerianParameters	KeplerianParametersConverter.toParameters(PVCoordinates cartesian, PositionAngleType positionAngleType)	Convert Cartesian coordinates to Keplerian elements.

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

Modifier	Constructor	Description
	CartesianOrbit(PVCoordinates pvaCoordinates, Frame frame, AbsoluteDate date, double mu)	Constructor from Cartesian parameters.
	CircularOrbit(PVCoordinates pvCoordinates, Frame frame, AbsoluteDate date, double mu)	Constructor from Cartesian parameters.
	EquinoctialOrbit(PVCoordinates pvCoordinates, Frame frame, AbsoluteDate date, double mu)	Constructor from Cartesian parameters.
	KeplerianOrbit(PVCoordinates pvCoordinates, Frame frame, AbsoluteDate date, double mu)	Constructor from Cartesian parameters.

Uses of PVCoordinates in org.orekit.orbits.cr3bp

Methods in org.orekit.orbits.cr3bp that return PVCoordinates

Modifier and Type	Method	Description
protected PVCoordinates	HaloOrbit.applyCorrectionOnPV(CR3BPDifferentialCorrection diff)	Apply the differential correction to compute more accurate initial PV.
protected abstract PVCoordinates	LibrationOrbit.applyCorrectionOnPV(CR3BPDifferentialCorrection diff)	Apply the differential correction to compute more accurate initial PV.
protected PVCoordinates	LyapunovOrbit.applyCorrectionOnPV(CR3BPDifferentialCorrection diff)	Apply the differential correction to compute more accurate initial PV.
PVCoordinates	CR3BPDifferentialCorrection.compute(LibrationOrbitType type)	Return the real starting PVCoordinates on the Libration orbit type after differential correction from a first guess.
PVCoordinates	RichardsonExpansion.computeHaloFirstGuess(double azr, LibrationOrbitFamily type, double t, double phi)	Calculate first Guess.
PVCoordinates	CR3BPDifferentialCorrection.computeLyapunov()	Return the real starting PVCoordinates on the Lyapunov orbit after differential correction from a first guess.
PVCoordinates	RichardsonExpansion.computeLyapunovFirstGuess(double ayr, double t, double phi)	Calculate first Guess.
PVCoordinates	LibrationOrbit.getInitialPV()	Return the initialPV on the libration orbit.
PVCoordinates	LibrationOrbit.getManifolds(SpacecraftState s, boolean isStable)	Return a manifold direction from one position on a libration Orbit.

Constructors in org.orekit.orbits.cr3bp with parameters of type PVCoordinates

Modifier	Constructor	Description
	CR3BPDifferentialCorrection(PVCoordinates firstguess, CR3BPSystem syst, double orbitalPeriod)	Simple Constructor.
	HaloOrbit(CR3BPSystem syst, PVCoordinates pv, double orbitalPeriod)	Simple Constructor.
protected	LibrationOrbit(CR3BPSystem system, PVCoordinates initialPV, double orbitalPeriod)	Constructor.
	LyapunovOrbit(CR3BPSystem syst, PVCoordinates pv, double orbitalPeriod)	Simple Constructor.

Uses of PVCoordinates in org.orekit.propagation.analytical.gnss

Methods in org.orekit.propagation.analytical.gnss that return PVCoordinates

Modifier and Type	Method	Description
PVCoordinates	GLONASSAnalyticalPropagator.propagateInEcef(AbsoluteDate date)	Gets the PVCoordinates of the GLONASS SV in ECEF frame.
PVCoordinates	GNSSPropagator.propagateInEcef(AbsoluteDate date)	Gets the PVCoordinates of the GNSS SV in ECEF frame.
PVCoordinates	SBASPropagator.propagateInEcef(AbsoluteDate date)	Gets the PVCoordinates of the GNSS SV in ECEF frame.

Uses of PVCoordinates in org.orekit.propagation.analytical.intelsat

Methods in org.orekit.propagation.analytical.intelsat that return PVCoordinates

Modifier and Type	Method	Description
PVCoordinates	IntelsatElevenElementsPropagator.propagateInEcef(AbsoluteDate date)	Converts the Intelsat's 11 elements into Position/Velocity coordinates in ECEF.

Uses of PVCoordinates in org.orekit.propagation.analytical.tle

Methods in org.orekit.propagation.analytical.tle that return PVCoordinates

Modifier and Type	Method	Description
PVCoordinates	TLEPropagator.getPVCoordinates(AbsoluteDate date)	Get the extrapolated position and velocity from an initial TLE.

Uses of PVCoordinates in org.orekit.propagation.events

Methods in org.orekit.propagation.events that return PVCoordinates

Modifier and Type	Method	Description
PVCoordinates	ExtremumApproachDetector.computeDeltaPV(SpacecraftState s)	Compute the relative PV between primary and secondary objects.

Uses of PVCoordinates in org.orekit.propagation.events.handlers

Methods in org.orekit.propagation.events.handlers that return types with arguments of type PVCoordinates

Modifier and Type	Method	Description
List<Pair<AbsolutePVCoordinates,PVCoordinates>>	SecondaryEventLogger.copyLogs()	Method to copy logs.

Uses of PVCoordinates in org.orekit.ssa.collision.shorttermencounter.probability.twod

Methods in org.orekit.ssa.collision.shorttermencounter.probability.twod that return PVCoordinates

Modifier and Type	Method	Description
PVCoordinates	ShortTermEncounter2DDefinition.computeOtherRelativeToReferencePVInReferenceInertial()	Compute the other collision position and velocity relative to the reference collision object.

Uses of PVCoordinates in org.orekit.utils

Subclasses of PVCoordinates in org.orekit.utils

Modifier and Type	Class	Description
class	TimeStampedPVCoordinates	time-stamped version of PVCoordinates.

Fields in org.orekit.utils declared as PVCoordinates

Modifier and Type	Field	Description
static final PVCoordinates	PVCoordinates.ZERO	Fixed position/velocity at origin (both p, v and a are zero vectors).

Methods in org.orekit.utils that return PVCoordinates

Modifier and Type	Method	Description
PVCoordinates	AngularCoordinates.applyTo(PVCoordinates pv)	Apply the rotation to a pv coordinates.
PVCoordinates	PVCoordinates.blendArithmeticallyWith(PVCoordinates other, double blendingValue)
static PVCoordinates	PVCoordinates.crossProduct(PVCoordinates pv1, PVCoordinates pv2)	Compute the cross-product of two instances.
PVCoordinates	PVCoordinates.negate()	Get the opposite of the instance.
PVCoordinates	PVCoordinates.normalize()	Normalize the position part of the instance.
PVCoordinates	PVCoordinates.shiftedBy(double dt)	Get a time-shifted state.
PVCoordinates	FieldPVCoordinates.toPVCoordinates()	Convert to a constant position-velocity.

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

Modifier and Type	Method	Description
PVCoordinates	AngularCoordinates.applyTo(PVCoordinates pv)	Apply the rotation to a pv coordinates.
FieldPVCoordinates<T>	FieldAngularCoordinates.applyTo(PVCoordinates pv)	Apply the rotation to a pv coordinates.
PVCoordinates	PVCoordinates.blendArithmeticallyWith(PVCoordinates other, double blendingValue)
static PVCoordinates	PVCoordinates.crossProduct(PVCoordinates pv1, PVCoordinates pv2)	Compute the cross-product of two instances.

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

Modifier	Constructor	Description
	AbsolutePVCoordinates(Frame frame, AbsoluteDate date, PVCoordinates pva)	Build from frame, date and PVA coordinates.
	AngularCoordinates(PVCoordinates u, PVCoordinates v)	Build one of the rotations that transform one pv coordinates into another one.
	AngularCoordinates(PVCoordinates u1, PVCoordinates u2, PVCoordinates v1, PVCoordinates v2, double tolerance)	Build the rotation that transforms a pair of pv coordinates into another one.
	FieldPVCoordinates(Field<T> field, PVCoordinates pv)	Builds a FieldPVCoordinates from a field and a regular PVCoordinates.
	FieldPVCoordinates(T a, PVCoordinates pv)	Multiplicative constructor.
	FieldPVCoordinates(T a1, PVCoordinates pv1, T a2, PVCoordinates pv2)	Linear constructor.
	FieldPVCoordinates(T a1, PVCoordinates pv1, T a2, PVCoordinates pv2, T a3, PVCoordinates pv3)	Linear constructor.
	FieldPVCoordinates(T a1, PVCoordinates pv1, T a2, PVCoordinates pv2, T a3, PVCoordinates pv3, T a4, PVCoordinates pv4)	Linear constructor.
	PVCoordinates(double a, PVCoordinates pv)	Multiplicative constructor.
	PVCoordinates(double a1, PVCoordinates pv1, double a2, PVCoordinates pv2)	Linear constructor.
	PVCoordinates(double a1, PVCoordinates pv1, double a2, PVCoordinates pv2, double a3, PVCoordinates pv3)	Linear constructor.
	PVCoordinates(double a1, PVCoordinates pv1, double a2, PVCoordinates pv2, double a3, PVCoordinates pv3, double a4, PVCoordinates pv4)	Linear constructor.
	PVCoordinates(PVCoordinates start, PVCoordinates end)	Subtractive constructor.
	TimeStampedAngularCoordinates(AbsoluteDate date, PVCoordinates u, PVCoordinates v)	Build one of the rotations that transform one pv coordinates into another one.
	TimeStampedAngularCoordinates(AbsoluteDate date, PVCoordinates u1, PVCoordinates u2, PVCoordinates v1, PVCoordinates v2, double tolerance)	Build the rotation that transforms a pair of pv coordinates into another pair.
	TimeStampedFieldPVCoordinates(AbsoluteDate date, T a, PVCoordinates pv)	Multiplicative constructor
	TimeStampedFieldPVCoordinates(AbsoluteDate date, T a1, PVCoordinates pv1, T a2, PVCoordinates pv2)	Linear constructor
	TimeStampedFieldPVCoordinates(AbsoluteDate date, T a1, PVCoordinates pv1, T a2, PVCoordinates pv2, T a3, PVCoordinates pv3)	Linear constructor
	TimeStampedFieldPVCoordinates(AbsoluteDate date, T a1, PVCoordinates pv1, T a2, PVCoordinates pv2, T a3, PVCoordinates pv3, T a4, PVCoordinates pv4)	Linear constructor
	TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, T a, PVCoordinates pv)	Multiplicative constructor
	TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, T a1, PVCoordinates pv1, T a2, PVCoordinates pv2)	Linear constructor
	TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, T a1, PVCoordinates pv1, T a2, PVCoordinates pv2, T a3, PVCoordinates pv3)	Linear constructor
	TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T> date, T a1, PVCoordinates pv1, T a2, PVCoordinates pv2, T a3, PVCoordinates pv3, T a4, PVCoordinates pv4)	Linear constructor
	TimeStampedPVCoordinates(AbsoluteDate date, double a, PVCoordinates pv)	Multiplicative constructor
	TimeStampedPVCoordinates(AbsoluteDate date, double a1, PVCoordinates pv1, double a2, PVCoordinates pv2)	Linear constructor
	TimeStampedPVCoordinates(AbsoluteDate date, double a1, PVCoordinates pv1, double a2, PVCoordinates pv2, double a3, PVCoordinates pv3)	Linear constructor
	TimeStampedPVCoordinates(AbsoluteDate date, double a1, PVCoordinates pv1, double a2, PVCoordinates pv2, double a3, PVCoordinates pv3, double a4, PVCoordinates pv4)	Linear constructor
	TimeStampedPVCoordinates(AbsoluteDate date, PVCoordinates pv)	Build from position velocity acceleration coordinates.
	TimeStampedPVCoordinates(AbsoluteDate date, PVCoordinates start, PVCoordinates end)	Subtractive constructor