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.estimation.iod	This package provides initial orbit determination methods.
org.orekit.files.ccsds	This package provides a parser for elements data stored in CCSDS Navigation Data Message format.
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.orbits	This package provides classes to represent orbits.
org.orekit.propagation.analytical.gnss	This package provides classes to propagate GNSS orbits.
org.orekit.propagation.analytical.tle	This package provides classes to read and extrapolate tle's.
org.orekit.propagation.numerical	Top level package for numerical propagators.
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 and 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 and Description
FieldGeodeticPoint<DerivativeStructure>	OneAxisEllipsoid.transform(PVCoordinates point, Frame frame, AbsoluteDate date) Transform a Cartesian point to a surface-relative point.

Uses of PVCoordinates in org.orekit.estimation.iod

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

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

Uses of PVCoordinates in org.orekit.files.ccsds

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

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

Uses of PVCoordinates in org.orekit.files.sp3

Subclasses of PVCoordinates in org.orekit.files.sp3

Modifier and Type	Class and Description
static class	SP3File.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 and Description
PVCoordinates	Transform.getCartesian() Get the underlying elementary Cartesian part.
PVCoordinates	Transform.transformPVCoordinates(PVCoordinates pva) Transform PVCoordinates including kinematic effects.

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

Modifier and Type	Method and 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.
abstract Rotation	LOFType.rotationFromInertial(PVCoordinates pv) Get the rotation from inertial frame to local orbital frame.
Transform	LOFType.transformFromInertial(AbsoluteDate date, PVCoordinates pv) Get the transform from an inertial frame defining position-velocity and the local orbital frame.
FieldPVCoordinates<T>	FieldTransform.transformPVCoordinates(PVCoordinates pv) Transform TimeStampedPVCoordinates including kinematic effects.
PVCoordinates	Transform.transformPVCoordinates(PVCoordinates pva) Transform PVCoordinates including kinematic effects.

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

Constructor and Description
Transform(AbsoluteDate date, PVCoordinates cartesian) Build a translation transform, with its first time derivative.

Uses of PVCoordinates in org.orekit.orbits

Methods in org.orekit.orbits that return PVCoordinates

Modifier and Type	Method and Description
protected PVCoordinates	HaloOrbit.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.
protected abstract PVCoordinates	LibrationOrbit.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(STMEquations stm) 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.

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

Modifier and Type	Method and Description
protected static boolean	Orbit.hasNonKeplerianAcceleration(PVCoordinates pva, double mu) Check if Cartesian coordinates include non-Keplerian acceleration.

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

Constructor and 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.
CR3BPDifferentialCorrection(PVCoordinates firstguess, CR3BPSystem syst, double orbitalPeriod) Simple Constructor.
CR3BPDifferentialCorrection(PVCoordinates firstguess, CR3BPSystem syst, double orbitalPeriod, AttitudeProvider attitudeProvider, TimeScale utc) Simple Constructor.
EquinoctialOrbit(PVCoordinates pvCoordinates, Frame frame, AbsoluteDate date, double mu) Constructor from Cartesian parameters.
HaloOrbit(CR3BPSystem syst, PVCoordinates pv, double orbitalPeriod) Simple Constructor.
KeplerianOrbit(PVCoordinates pvCoordinates, Frame frame, AbsoluteDate date, double mu) Constructor from Cartesian parameters.
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 and Description
PVCoordinates	SBASPropagator.propagateInEcef(AbsoluteDate date) Gets the PVCoordinates of the GNSS SV in ECEF frame.
PVCoordinates	GLONASSAnalyticalPropagator.propagateInEcef(AbsoluteDate date) Gets the PVCoordinates of the GLONASS SV in ECEF frame.
PVCoordinates	AbstractGNSSPropagator.propagateInEcef(AbsoluteDate date) Gets the PVCoordinates of the GNSS SV in ECEF frame.

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

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

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

Uses of PVCoordinates in org.orekit.propagation.numerical

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

Modifier and Type	Method and Description
PVCoordinates	GLONASSNumericalPropagator.getPVInPZ90(SpacecraftState state) This method transforms the PV coordinates obtained after the numerical integration in the ECEF PZ-90.

Uses of PVCoordinates in org.orekit.utils

Subclasses of PVCoordinates in org.orekit.utils

Modifier and Type	Class and Description
class	AbsolutePVCoordinates Position - Velocity - Acceleration linked to a date and a frame.
class	TimeStampedPVCoordinates time-stamped version of PVCoordinates.

Fields in org.orekit.utils declared as PVCoordinates

Modifier and Type	Field and Description
static 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 and Description
PVCoordinates	AngularCoordinates.applyTo(PVCoordinates pv) Apply the rotation to a pv coordinates.
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 and Description
FieldPVCoordinates<T>	FieldAngularCoordinates.applyTo(PVCoordinates pv) Apply the rotation to a pv coordinates.
PVCoordinates	AngularCoordinates.applyTo(PVCoordinates pv) Apply the rotation to a pv coordinates.
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

Constructor and 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