Uses of Class
org.orekit.utils.AbsolutePVCoordinates

Packages that use AbsolutePVCoordinates

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.propagation	Propagation
org.orekit.propagation.numerical	Top level package for numerical propagators.
org.orekit.utils	This package provides useful objects.

Uses of AbsolutePVCoordinates in org.orekit.bodies

Methods in org.orekit.bodies that return AbsolutePVCoordinates

Modifier and Type	Method and Description
AbsolutePVCoordinates	CR3BPSystem.getRealAPV(AbsolutePVCoordinates apv0, AbsoluteDate initialDate, Frame outputFrame) Get the AbsolutePVCoordinates from normalized units to standard units in an output frame.

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

Modifier and Type	Method and Description
AbsolutePVCoordinates	CR3BPSystem.getRealAPV(AbsolutePVCoordinates apv0, AbsoluteDate initialDate, Frame outputFrame) Get the AbsolutePVCoordinates from normalized units to standard units in an output frame.

Uses of AbsolutePVCoordinates in org.orekit.propagation

Methods in org.orekit.propagation that return AbsolutePVCoordinates

Modifier and Type	Method and Description
AbsolutePVCoordinates	SpacecraftState.getAbsPVA() Get the absolute position-velocity-acceleration.

Constructors in org.orekit.propagation with parameters of type AbsolutePVCoordinates

Constructor and Description
SpacecraftState(AbsolutePVCoordinates absPva) Build a spacecraft state from position-velocity-acceleration only.
SpacecraftState(AbsolutePVCoordinates absPva, Attitude attitude) Build a spacecraft state from position-velocity-acceleration and attitude.
SpacecraftState(AbsolutePVCoordinates absPva, Attitude attitude, double mass) Build a spacecraft state from position-velocity-acceleration, attitude and mass.
SpacecraftState(AbsolutePVCoordinates absPva, Attitude attitude, DoubleArrayDictionary additional) Build a spacecraft state from position-velocity-acceleration, attitude and additional states.
SpacecraftState(AbsolutePVCoordinates absPva, Attitude attitude, double mass, DoubleArrayDictionary additional) Build a spacecraft state from position-velocity-acceleration, attitude, mass and additional states.
SpacecraftState(AbsolutePVCoordinates absPva, Attitude attitude, double mass, DoubleArrayDictionary additional, DoubleArrayDictionary additionalDot) Build a spacecraft state from position-velocity-acceleration, attitude, mass and additional states and derivatives.
SpacecraftState(AbsolutePVCoordinates absPva, Attitude attitude, double mass, Map<String,double[]> additional) Deprecated. as of 11.1, replaced by SpacecraftState.SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary)
SpacecraftState(AbsolutePVCoordinates absPva, Attitude attitude, Map<String,double[]> additional) Deprecated. as of 11.1, replaced by SpacecraftState.SpacecraftState(AbsolutePVCoordinates, Attitude, DoubleArrayDictionary)
SpacecraftState(AbsolutePVCoordinates absPva, double mass) Create a new instance from position-velocity-acceleration and mass.
SpacecraftState(AbsolutePVCoordinates absPva, DoubleArrayDictionary additional) Build a spacecraft state from position-velocity-acceleration and additional states.
SpacecraftState(AbsolutePVCoordinates absPva, double mass, DoubleArrayDictionary additional) Create a new instance from position-velocity-acceleration, mass and additional states.
SpacecraftState(AbsolutePVCoordinates absPva, double mass, Map<String,double[]> additional) Deprecated. as of 11.1, replaced by SpacecraftState.SpacecraftState(AbsolutePVCoordinates, double, DoubleArrayDictionary)
SpacecraftState(AbsolutePVCoordinates absPva, Map<String,double[]> additional) Deprecated. as of 11.1, replaced by SpacecraftState.SpacecraftState(AbsolutePVCoordinates, DoubleArrayDictionary)

Uses of AbsolutePVCoordinates in org.orekit.propagation.numerical

Methods in org.orekit.propagation.numerical with parameters of type AbsolutePVCoordinates

Modifier and Type	Method and Description
static double[][]	NumericalPropagator.tolerances(double dP, AbsolutePVCoordinates absPva) Estimate tolerance vectors for integrators when propagating in absolute position-velocity-acceleration.

Uses of AbsolutePVCoordinates in org.orekit.utils

Methods in org.orekit.utils that return AbsolutePVCoordinates

Modifier and Type	Method and Description
AbsolutePVCoordinates	AbsolutePVCoordinates.interpolate(AbsoluteDate date, Stream<AbsolutePVCoordinates> sample)
static AbsolutePVCoordinates	AbsolutePVCoordinates.interpolate(Frame frame, AbsoluteDate date, CartesianDerivativesFilter filter, Stream<AbsolutePVCoordinates> sample) Interpolate position-velocity.
AbsolutePVCoordinates	AbsolutePVCoordinates.shiftedBy(double dt) Get a time-shifted state.
AbsolutePVCoordinates	FieldAbsolutePVCoordinates.toAbsolutePVCoordinates() Converts to an AbsolutePVCoordinates instance.

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

Modifier and Type	Method and Description
AbsolutePVCoordinates	AbsolutePVCoordinates.interpolate(AbsoluteDate date, Stream<AbsolutePVCoordinates> sample)
static AbsolutePVCoordinates	AbsolutePVCoordinates.interpolate(Frame frame, AbsoluteDate date, CartesianDerivativesFilter filter, Stream<AbsolutePVCoordinates> sample) Interpolate position-velocity.

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

Constructor and Description
AbsolutePVCoordinates(AbsoluteDate date, AbsolutePVCoordinates start, AbsolutePVCoordinates end) Subtractive constructor
AbsolutePVCoordinates(AbsoluteDate date, double a, AbsolutePVCoordinates AbsPva) Multiplicative constructor
AbsolutePVCoordinates(AbsoluteDate date, double a1, AbsolutePVCoordinates absPv1, double a2, AbsolutePVCoordinates absPv2) Linear constructor
AbsolutePVCoordinates(AbsoluteDate date, double a1, AbsolutePVCoordinates absPv1, double a2, AbsolutePVCoordinates absPv2, double a3, AbsolutePVCoordinates absPv3) Linear constructor
AbsolutePVCoordinates(AbsoluteDate date, double a1, AbsolutePVCoordinates absPv1, double a2, AbsolutePVCoordinates absPv2, double a3, AbsolutePVCoordinates absPv3, double a4, AbsolutePVCoordinates absPv4) Linear constructor