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.control.indirect.shooting.boundary	This package provides classes relative to the boundary conditions for indirect shooting.
org.orekit.propagation	Propagation
org.orekit.propagation.conversion	This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
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	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	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.control.indirect.shooting.boundary

Methods in org.orekit.control.indirect.shooting.boundary that return AbsolutePVCoordinates

Modifier and Type	Method	Description
AbsolutePVCoordinates	FixedTimeCartesianBoundaryStates.getInitialCartesianState()	Getter for the initial Cartesian condition.
AbsolutePVCoordinates	FixedTimeCartesianBoundaryStates.getTerminalCartesianState()	Getter for the terminal Cartesian condition.

Constructors in org.orekit.control.indirect.shooting.boundary with parameters of type AbsolutePVCoordinates

Constructor	Description
FixedTimeCartesianBoundaryStates(AbsolutePVCoordinates initialCartesianState, AbsolutePVCoordinates terminalCartesianState)	Constructor.

Uses of AbsolutePVCoordinates in org.orekit.propagation

Methods in org.orekit.propagation that return AbsolutePVCoordinates

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

Methods in org.orekit.propagation that return types with arguments of type AbsolutePVCoordinates

Modifier and Type	Method	Description
Optional<TimeInterpolator<AbsolutePVCoordinates>>	SpacecraftStateInterpolator.getAbsPVAInterpolator()	Get absolute position-velocity-acceleration interpolator.

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

Constructor	Description
SpacecraftState(AbsolutePVCoordinates absPva)	Build a spacecraft state from position-velocity-acceleration only.
SpacecraftState(AbsolutePVCoordinates absPva, double mass)	Create a new instance from position-velocity-acceleration and mass.
SpacecraftState(AbsolutePVCoordinates absPva, double mass, DoubleArrayDictionary additional)	Create a new instance from position-velocity-acceleration, mass and additional states.
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, 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, DoubleArrayDictionary additional)	Build a spacecraft state from position-velocity-acceleration, attitude and additional states.
SpacecraftState(AbsolutePVCoordinates absPva, DoubleArrayDictionary additional)	Build a spacecraft state from position-velocity-acceleration and additional states.

Uses of AbsolutePVCoordinates in org.orekit.propagation.conversion

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

Modifier and Type	Method	Description
default AbstractIntegrator	ODEIntegratorBuilder.buildIntegrator(AbsolutePVCoordinates absolutePVCoordinates)	Build a first order integrator.

Uses of AbsolutePVCoordinates in org.orekit.propagation.numerical

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

Modifier and Type	Method	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	Description
protected AbsolutePVCoordinates	AbsolutePVCoordinatesHermiteInterpolator.interpolate(AbstractTimeInterpolator.InterpolationData interpolationData)	Interpolate instance from given interpolation data.
AbsolutePVCoordinates	AbsolutePVCoordinates.shiftedBy(double dt)	Get a time-shifted state.
AbsolutePVCoordinates	FieldAbsolutePVCoordinates.toAbsolutePVCoordinates()	Converts to an AbsolutePVCoordinates instance.

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

Constructor	Description
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
AbsolutePVCoordinates(AbsoluteDate date, AbsolutePVCoordinates start, AbsolutePVCoordinates end)	Subtractive constructor
FieldAbsolutePVCoordinates(Field<T> field, AbsolutePVCoordinates pva)	Build from Field and non-Fielded object.