Uses of Class
org.orekit.utils.PVCoordinates

Packages that use PVCoordinates

fr.cnes.sirius.patrius.assembly.models
fr.cnes.sirius.patrius.forces
fr.cnes.sirius.patrius.groundstation
fr.cnes.sirius.patrius.propagation.numerical.multi
fr.cnes.sirius.patrius.propagation.precomputed.multi
fr.cnes.sirius.patrius.stela.bodies
fr.cnes.sirius.patrius.stela.forces.radiation
fr.cnes.sirius.patrius.stela.orbits
fr.cnes.sirius.patrius.stela.propagation
fr.cnes.sirius.patrius.tools.ephemerisComparator
fr.cnes.sirius.patrius.tools.force.validation
fr.cnes.sirius.patrius.utils
fr.cnes.sirius.validate.mocks.ephemeris
org.orekit.attitudes.directions
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.general	This package provides interfaces for orbit file representations and corresponding parsers.
org.orekit.forces.drag
org.orekit.forces.gravity
org.orekit.forces.gravity.tides
org.orekit.forces.gravity.variations
org.orekit.frames	This package provides classes to handle frames and transforms between them.
org.orekit.frames.transformations
org.orekit.orbits	This package provides classes to represent orbits.
org.orekit.orbits.orbitalparameters
org.orekit.propagation	This package provides tools to propagate orbital states with different methods.
org.orekit.propagation.analytical.tle	This package provides classes to read and extrapolate tle's.
org.orekit.propagation.numerical
org.orekit.propagation.precomputed
org.orekit.utils	This package provides useful objects.

Uses of PVCoordinates in fr.cnes.sirius.patrius.assembly.models

Methods in fr.cnes.sirius.patrius.assembly.models that return PVCoordinates

PVCoordinates

SensorModel.getPVCoordinates(AbsoluteDate date, Frame frame) Get the PVCoordinates of the sensor part in the selected frame.

Uses of PVCoordinates in fr.cnes.sirius.patrius.forces

Methods in fr.cnes.sirius.patrius.forces with parameters of type PVCoordinates

Vector3D	EmpiricalForce.computeAcceleration(PVCoordinates pv, LocalOrbitalFrame localFrameValidation, Vector3D vectorS, Frame frame, SpacecraftState state) Method to compute the acceleration.
double[]	EmpiricalForce.computeCosSin(PVCoordinates pv, Vector3D vectorS) Private method to compute the cos(nwt) and sin(nwt) values.

Uses of PVCoordinates in fr.cnes.sirius.patrius.groundstation

Methods in fr.cnes.sirius.patrius.groundstation that return PVCoordinates

PVCoordinates	RFStationAntenna.getPVCoordinates(AbsoluteDate date, Frame frame)
PVCoordinates	GeometricStationAntenna.getPVCoordinates(AbsoluteDate date, Frame frame) Get the PVCoordinates of the station antenna in the selected frame.

Uses of PVCoordinates in fr.cnes.sirius.patrius.propagation.numerical.multi

Methods in fr.cnes.sirius.patrius.propagation.numerical.multi that return PVCoordinates

PVCoordinates

MultiNumericalPropagator.getPVCoordinates(AbsoluteDate date, Frame frame, String satId) Get the PVCoordinates of the body in the selected frame.

Uses of PVCoordinates in fr.cnes.sirius.patrius.propagation.precomputed.multi

Methods in fr.cnes.sirius.patrius.propagation.precomputed.multi that return PVCoordinates

PVCoordinates

MultiIntegratedEphemeris.getPVCoordinates(AbsoluteDate date, Frame frame) Get the PVCoordinates of the body in the selected frame.

Uses of PVCoordinates in fr.cnes.sirius.patrius.stela.bodies

Methods in fr.cnes.sirius.patrius.stela.bodies that return PVCoordinates

PVCoordinates	MeeusSunStela.getPVCoordinates(AbsoluteDate date, Frame frame) Deprecated.
PVCoordinates	MeeusMoonStela.getPVCoordinates(AbsoluteDate date, Frame frame)

Uses of PVCoordinates in fr.cnes.sirius.patrius.stela.forces.radiation

Methods in fr.cnes.sirius.patrius.stela.forces.radiation with parameters of type PVCoordinates

Vector3D	SRPSquaring.computeAcceleration(StelaEquinoctialOrbit orbit, PVCoordinates satSunVector) Compute the acceleration due to the force.
protected double[]	SRPSquaring.computeInOutTrueAnom(StelaEquinoctialOrbit orbit, PVCoordinates sunPV) Computation of in and out true anomalies of the shadowed part of the orbit.
protected double[]	SRPSquaring.computeSunBetaPhi(StelaEquinoctialOrbit orbit, PVCoordinates sunPV) Computation of Sun's right ascension (φ) and declination (β) wrt the orbit plane.

Uses of PVCoordinates in fr.cnes.sirius.patrius.stela.orbits

Methods in fr.cnes.sirius.patrius.stela.orbits that return PVCoordinates

PVCoordinates	StelaEquinoctialOrbit.getPVCoordinates(AbsoluteDate otherDate, Frame otherFrame)
protected PVCoordinates	StelaEquinoctialOrbit.initPVCoordinates()

Constructors in fr.cnes.sirius.patrius.stela.orbits with parameters of type PVCoordinates

StelaEquinoctialOrbit(PVCoordinates pvCoordinates, Frame frame, AbsoluteDate date, double mu)
Constructor from cartesian parameters.

Uses of PVCoordinates in fr.cnes.sirius.patrius.stela.propagation

Methods in fr.cnes.sirius.patrius.stela.propagation that return PVCoordinates

PVCoordinates

StelaAbstractPropagator.getPVCoordinates(AbsoluteDate date, Frame frame) Get the PVCoordinates of the body in the selected frame.

Uses of PVCoordinates in fr.cnes.sirius.patrius.tools.ephemerisComparator

Subclasses of PVCoordinates in fr.cnes.sirius.patrius.tools.ephemerisComparator

class

PVCoordinatesDPFacade This class is a facade for the use of PVCoordinates.

Uses of PVCoordinates in fr.cnes.sirius.patrius.tools.force.validation

Methods in fr.cnes.sirius.patrius.tools.force.validation that return PVCoordinates

PVCoordinates

BasicPVCoordinatesProvider.getPVCoordinates(AbsoluteDate date, Frame inFrame) Get the PVCoordinates of the body in the selected frame.

Methods in fr.cnes.sirius.patrius.tools.force.validation that return types with arguments of type PVCoordinates

List<PVCoordinates>

PVEphemerisLoader.getEphemeris() Give the list of PV coordinates which have been read.

Constructors in fr.cnes.sirius.patrius.tools.force.validation with parameters of type PVCoordinates

BasicPVCoordinatesProvider(PVCoordinates inCoordinates, Frame inFrame)
Build a direction from an origin and a target described by their PVCoordinatesProvider

Uses of PVCoordinates in fr.cnes.sirius.patrius.utils

Methods in fr.cnes.sirius.patrius.utils that return PVCoordinates

PVCoordinates

AlmanacPVCoordinates.getPVCoordinates(AbsoluteDate date, Frame frame) Geometric computation of the position to a date.

Uses of PVCoordinates in fr.cnes.sirius.validate.mocks.ephemeris

Methods in fr.cnes.sirius.validate.mocks.ephemeris that return PVCoordinates

PVCoordinates	UserCelestialBody.getPVCoordinates(AbsoluteDate date, Frame frame) Computes the PV coordinates at a date using linear interpolator.
PVCoordinates	UserCelestialBody.getPVCoordinatesLagrange4(AbsoluteDate date, Frame frame) Computes the PV coordinates at a date using Lagrange 4 interpolator.

Methods in fr.cnes.sirius.validate.mocks.ephemeris that return types with arguments of type PVCoordinates

Map<AbsoluteDate,PVCoordinates>	UserEphemeris.getEphemeris()
Map<AbsoluteDate,PVCoordinates>	IUserEphemeris.getEphemeris()

Uses of PVCoordinates in org.orekit.attitudes.directions

Methods in org.orekit.attitudes.directions that return PVCoordinates

PVCoordinates	ITargetDirection.getTargetPVCoordinates(AbsoluteDate date, Frame frame) Provides the target point at a given date in a given frame, represented by the associated PVCoordinates object
PVCoordinates	EarthToCelestialBodyCenterDirection.getTargetPVCoordinates(AbsoluteDate date, Frame frame) Provides the target point at a given date in a given frame, represented by the associated PVCoordinates object
PVCoordinates	GenericTargetDirection.getTargetPVCoordinates(AbsoluteDate date, Frame frame) Provides the target point at a given date in a given frame, represented by the associated PVCoordinates object
PVCoordinates	EarthCenterDirection.getTargetPVCoordinates(AbsoluteDate date, Frame frame) Provides the target point at a given date in a given frame, represented by the associated PVCoordinates object
PVCoordinates	ToCelestialBodyCenterDirection.getTargetPVCoordinates(AbsoluteDate date, Frame frame) Provides the target point at a given date in a given frame, represented by the associated PVCoordinates object

Uses of PVCoordinates in org.orekit.bodies

Methods in org.orekit.bodies that return PVCoordinates

PVCoordinates	PosVelChebyshev.getPositionVelocity(AbsoluteDate date) Get the position-velocity at a specified date.
PVCoordinates	MeeusMoon.getPVCoordinates(AbsoluteDate date, Frame frame)
PVCoordinates	ExtendedOneAxisEllipsoid.getPVCoordinates(AbsoluteDate date, Frame frame)
PVCoordinates	MeeusSun.getPVCoordinates(AbsoluteDate date, Frame frame)
abstract PVCoordinates	AbstractCelestialBody.getPVCoordinates(AbsoluteDate date, Frame frame) Get the PVCoordinates of the body in the selected frame.

Uses of PVCoordinates in org.orekit.files.general

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

PVCoordinates

SatelliteTimeCoordinate.getCoordinate() Returns the coordinate of this entry.

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

void	SatelliteTimeCoordinate.setCoordinate(PVCoordinates coordinate) Set the coordinate for this entry.

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

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.forces.drag

Methods in org.orekit.forces.drag with parameters of type PVCoordinates

static Vector3D

DragForce.computeAcceleration(PVCoordinates pv, Frame frame, Atmosphere atm, AbsoluteDate date, double kD, double mass) Method to compute the acceleration.

Uses of PVCoordinates in org.orekit.forces.gravity

Methods in org.orekit.forces.gravity with parameters of type PVCoordinates

Vector3D	BalminoAttractionModel.computeAcceleration(PVCoordinates pv) Acceleration in body frame.
Vector3D	DrozinerAttractionModel.computeAcceleration(PVCoordinates pv, AbsoluteDate date) Method to compute the acceleration.
Vector3D	CunninghamAttractionModel.computeAcceleration(PVCoordinates pv, AbsoluteDate date) Method to compute the acceleration.
Vector3D	ThirdBodyAttraction.computeAcceleration(PVCoordinates pv, Frame frame, AbsoluteDate date) Method to compute the acceleration.
Vector3D	NewtonianAttraction.computeAcceleration(PVCoordinates pv, Frame frame, AbsoluteDate date) Method to compute the acceleration.
static Vector3D	GravityToolbox.computeBalminoAcceleration(PVCoordinates pv, double[][] coefficientsC, double[][] coefficientsS, double muc, double eqRadius, int degree, int order, HelmholtzPolynomial helm) Method to compute the acceleration, from Balmino algorithm (see BalminoAttractionModel).
static Vector3D	GravityToolbox.computeCunninghamAcceleration(PVCoordinates pv, double equatorialRadius, double[][] coefC, double[][] coefS, int degree, int order, double mu) Method to compute the acceleration.
static double[][]	GravityToolbox.computeDAccDPos(PVCoordinates pv, AbsoluteDate date, double equatorialRadius, double mu, double[][] C, double[][] S) Compute the partial derivatives of the acceleration (Cunningham algorithm) with respect to the position.
static Vector3D	GravityToolbox.computeDrozinerAcceleration(PVCoordinates pv, Frame frame, double[][] coefficientsC, double[][] coefficientsS, double muc, double eqRadius, double threshold, int degree, int order) Method to compute the acceleration, from Droziner algorithm (see DrozinerAttractionModel).

Uses of PVCoordinates in org.orekit.forces.gravity.tides

Methods in org.orekit.forces.gravity.tides with parameters of type PVCoordinates

Vector3D

AbstractTides.computeAcceleration(PVCoordinates pv, Frame frame, AbsoluteDate date) Method to compute the acceleration, from Balmino algorithm (see BalminoAttractionModel class).

Uses of PVCoordinates in org.orekit.forces.gravity.variations

Methods in org.orekit.forces.gravity.variations with parameters of type PVCoordinates

Vector3D

VariablePotentialAttractionModel.computeAcceleration(AbsoluteDate date, PVCoordinates pv) Compute acceleration in rotating frame

Uses of PVCoordinates in org.orekit.frames

Methods in org.orekit.frames that return PVCoordinates

PVCoordinates	SpacecraftFrame.getPVCoordinates(AbsoluteDate date, Frame frame) Deprecated. Get the PVCoordinates of the spacecraft frame origin in the selected frame.
PVCoordinates	TopocentricFrame.getPVCoordinates(AbsoluteDate date, Frame frame) Get the PVCoordinates of the topocentric frame origin in the selected frame.
PVCoordinates	TopocentricFrame.transformFromCardanToPV(CardanMountPV cardan) Transform a Cardan mounting into Cartesian coordinates (position and velocity) expressed in this local topocentric frame.
PVCoordinates	TopocentricFrame.transformFromTopocentricToPV(TopocentricPV topoCoord) Transform topocentric set of coordinates into Cartesian position and velocity coordinates expressed in this local topocentric frame .

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

double	TopocentricFrame.getAzimuthRate(PVCoordinates extPV, Frame frame, AbsoluteDate date) Get the azimuth rate of a point.
double	TopocentricFrame.getElevationRate(PVCoordinates extPV, Frame frame, AbsoluteDate date) Get the elevation rate of a point.
double	TopocentricFrame.getRangeRate(PVCoordinates extPV, Frame frame, AbsoluteDate date) Get the range rate of a point with regards to the topocentric frame center point.
double	TopocentricFrame.getXangleCardanRate(PVCoordinates extPV, Frame frame, AbsoluteDate date) Get the Cardan x angle rate.
double	TopocentricFrame.getYangleCardanRate(PVCoordinates extPV, Frame frame, AbsoluteDate date) Get the Cardan y angle rate.
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.
Transform	LOFType.transformFromInertial(AbsoluteDate date, PVCoordinates pv, boolean computeSpinDerivatives) Get the transform from an inertial frame defining position-velocity and the local orbital frame.
CardanMountPV	TopocentricFrame.transformFromPVToCardan(PVCoordinates extPV, Frame frame, AbsoluteDate date) Transform a Cartesian position coordinates into Cardan mounting in this local topocentric frame.
TopocentricPV	TopocentricFrame.transformFromPVToTopocentric(PVCoordinates extPV, Frame frame, AbsoluteDate date) Transform a Cartesian position and velocity coordinates into topocentric coordinates in this local topocentric frame.

Uses of PVCoordinates in org.orekit.frames.transformations

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

PVCoordinates	Transform.getCartesian() Get the position and velocity of the "destination" frame in the "origin" one.
PVCoordinates	Transform.transformPVCoordinates(PVCoordinates pv) Transform PVCoordinates including kinematic effects from an algebraic point of view.

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

PVCoordinates

Transform.transformPVCoordinates(PVCoordinates pv) Transform PVCoordinates including kinematic effects from an algebraic point of view.

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

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.orbits

Methods in org.orekit.orbits that return PVCoordinates

PVCoordinates	Orbit.getPVCoordinates() Get the PVCoordinates in definition frame.
PVCoordinates	Orbit.getPVCoordinates(AbsoluteDate otherDate, Frame otherFrame) Get the PVCoordinates of the body in the selected frame.
PVCoordinates	Orbit.getPVCoordinates(Frame outputFrame) Get the PVCoordinates in a specified frame.
protected PVCoordinates	CircularOrbit.initPVCoordinates() Compute the position/velocity coordinates from the canonical parameters.
protected PVCoordinates	KeplerianOrbit.initPVCoordinates() Compute the position/velocity coordinates from the canonical parameters.
protected abstract PVCoordinates	Orbit.initPVCoordinates() Compute the position/velocity coordinates from the canonical parameters.
protected PVCoordinates	EquatorialOrbit.initPVCoordinates() Compute the position/velocity coordinates from the canonical parameters.
protected PVCoordinates	EquinoctialOrbit.initPVCoordinates() Compute the position/velocity coordinates from the canonical parameters.
protected PVCoordinates	ApsisOrbit.initPVCoordinates() Compute the position/velocity coordinates from the canonical parameters.
protected PVCoordinates	CartesianOrbit.initPVCoordinates() Compute the position/velocity coordinates from the canonical parameters.

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

ApsisOrbit(PVCoordinates pvCoordinates, Frame frame, AbsoluteDate date, double mu)
Constructor from cartesian parameters.

CartesianOrbit(PVCoordinates pvCoordinates, Frame frame, AbsoluteDate date, double mu)
Constructor from cartesian parameters.

CircularOrbit(PVCoordinates pvCoordinates, Frame frame, AbsoluteDate date, double mu)
Constructor from cartesian parameters.

EquatorialOrbit(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.

Orbit(PVCoordinates pvCoordinates, Frame frame, AbsoluteDate date, double mu)
Set the orbit from Cartesian parameters.

Uses of PVCoordinates in org.orekit.orbits.orbitalparameters

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

PVCoordinates

CartesianParameters.getPVCoordinates() Get the PV coordinates.

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

CartesianParameters(PVCoordinates pvCoordinates, double mu)
Constructor with PV coordinates.

Uses of PVCoordinates in org.orekit.propagation

Methods in org.orekit.propagation that return PVCoordinates

PVCoordinates	SpacecraftState.getPVCoordinates() Get the PVCoordinates in orbit definition frame.
PVCoordinates	AbstractPropagator.getPVCoordinates(AbsoluteDate date, Frame frame) Get the PVCoordinates of the body in the selected frame.
PVCoordinates	SpacecraftState.getPVCoordinates(Frame outputFrame) Get the PVCoordinates in given output frame.

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

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

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

Uses of PVCoordinates in org.orekit.propagation.numerical

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

PVCoordinates

NumericalPropagator.getPVCoordinates(AbsoluteDate date, Frame frame) Get the PVCoordinates of the body in the selected frame.

Uses of PVCoordinates in org.orekit.propagation.precomputed

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

PVCoordinates	IntegratedEphemeris.getPVCoordinates(AbsoluteDate date, Frame frame) Get the PVCoordinates of the body in the selected frame.
PVCoordinates	Ephemeris.getPVCoordinates(AbsoluteDate date, Frame frame) Get the PVCoordinates of the body in the selected frame.

Uses of PVCoordinates in org.orekit.utils

Subclasses of PVCoordinates in org.orekit.utils

class

TimeStampedPVCoordinates time-stamped version of PVCoordinates.

Fields in org.orekit.utils declared as PVCoordinates

protected PVCoordinates[]	AbstractBoundedPVProvider.tPVCoord Position velocity coordinates table
static PVCoordinates	PVCoordinates.ZERO Fixed position/velocity/acceleration at origin (both p, v and a are zero vectors).

Methods in org.orekit.utils that return PVCoordinates

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	PVCoordinatesProvider.getPVCoordinates(AbsoluteDate date, Frame frame) Get the PVCoordinates of the body in the selected frame.
PVCoordinates	EphemerisPvLagrange.getPVCoordinates(AbsoluteDate date, Frame frame) Frame can be null : by default the frame of expression is the frame used at instantiation (which is the frame of the first spacecraft state when instantiation is done from a table of spacecraft states).
PVCoordinates	EphemerisPvHermite.getPVCoordinates(AbsoluteDate date, Frame frame) Get the PVCoordinates of the body in the selected frame.
static PVCoordinates	PVCoordinates.interpolate(AbsoluteDate date, boolean useVelocities, Collection<Pair<AbsoluteDate,PVCoordinates>> sample) Deprecated. since 3.1 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.

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

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

static PVCoordinates

PVCoordinates.interpolate(AbsoluteDate date, boolean useVelocities, Collection<Pair<AbsoluteDate,PVCoordinates>> sample) Deprecated. since 3.1 replaced with TimeStampedPVCoordinates.interpolate(AbsoluteDate, CartesianDerivativesFilter, Collection)

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

AbstractBoundedPVProvider(PVCoordinates[] tabPV, Frame frame, AbsoluteDate[] tabDate, ISearchIndex algo)
Instantiation of AbstractBoundedPVProvider attributes.

AngularCoordinates(PVCoordinates u1, PVCoordinates u2, PVCoordinates v1, PVCoordinates v2, double tolerance)
Build the rotation that transforms a pair of pv coordinates into another one.

AngularCoordinates(PVCoordinates u1, PVCoordinates u2, PVCoordinates v1, PVCoordinates v2, double tolerance, boolean spinDerivativesComputation)
Build the rotation that transforms a pair of pv coordinates into another one.

EphemerisPvHermite(PVCoordinates[] tabPV, Vector3D[] tabAcc, Frame frame, AbsoluteDate[] tabDate, ISearchIndex algo)
Creates an instance of EphemerisPvHermite.

EphemerisPvLagrange(PVCoordinates[] tabPV, int order, Frame frame, AbsoluteDate[] tabDate, ISearchIndex algo)
Creates an instance of EphemerisPvLagrange

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 u1, PVCoordinates u2, PVCoordinates v1, PVCoordinates v2, double tolerance)
Build the rotation that transforms a pair of pv coordinates into another pair.

TimeStampedAngularCoordinates(AbsoluteDate date, PVCoordinates u1, PVCoordinates u2, PVCoordinates v1, PVCoordinates v2, double tolerance, boolean spinDerivativesComputation)
Build the rotation that transforms a pair of pv coordinates into another pair.

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