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.files.ccsds	This package provides a parser for orbit data stored in CCSDS Orbit Data Message format.
org.orekit.files.general	This package provides interfaces for orbit file representations and corresponding parsers.
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.tle	This package provides classes to read and extrapolate tle's.
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.

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.general

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

Modifier and Type	Method and Description
PVCoordinates	SatelliteTimeCoordinate.getCoordinate() Returns the coordinate of this entry.

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

Modifier and Type	Method and Description
void	SatelliteTimeCoordinate.setCoordinate(PVCoordinates coordinate) Set the coordinate for this entry.

Constructors in org.orekit.files.general with parameters of type PVCoordinates

Constructor and Description
SatelliteTimeCoordinate(AbsoluteDate time, PVCoordinates coord) Creates a new SatelliteTimeCoordinate instance with a given epoch and coordinate.
SatelliteTimeCoordinate(AbsoluteDate time, PVCoordinates coord, double clockCorr, double rateChange) Creates a new SatelliteTimeCoordinate instance with a given epoch, coordinate and clock value / rate change.

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.
protected 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.
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

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.
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.propagation.analytical.tle

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

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

Uses of PVCoordinates in org.orekit.utils

Subclasses of PVCoordinates in org.orekit.utils

Modifier and Type	Class and Description
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.
static PVCoordinates	PVCoordinates.interpolate(AbsoluteDate date, boolean useVelocities, Collection<Pair<AbsoluteDate,PVCoordinates>> sample) Deprecated. since 7.0 replaced with TimeStampedPVCoordinates.interpolate(AbsoluteDate, CartesianDerivativesFilter, Collection)
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 without derivatives.

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

Method parameters in org.orekit.utils with type arguments of type PVCoordinates

Modifier and Type	Method and Description
static PVCoordinates	PVCoordinates.interpolate(AbsoluteDate date, boolean useVelocities, Collection<Pair<AbsoluteDate,PVCoordinates>> sample) Deprecated. since 7.0 replaced with TimeStampedPVCoordinates.interpolate(AbsoluteDate, CartesianDerivativesFilter, Collection)

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

Constructor and Description
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(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
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