Uses of Class
org.orekit.utils.FieldAbsolutePVCoordinates
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Packages that use FieldAbsolutePVCoordinates Package Description org.orekit.propagation Propagationorg.orekit.propagation.conversion This package provides tools to convert a given propagator or a set ofSpacecraftState
into another propagator.org.orekit.utils This package provides useful objects. -
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Uses of FieldAbsolutePVCoordinates in org.orekit.propagation
Methods in org.orekit.propagation that return FieldAbsolutePVCoordinates Modifier and Type Method Description FieldAbsolutePVCoordinates<T>
FieldSpacecraftState. getAbsPVA()
Get the absolute position-velocity-acceleration.Methods in org.orekit.propagation that return types with arguments of type FieldAbsolutePVCoordinates Modifier and Type Method Description Optional<FieldTimeInterpolator<FieldAbsolutePVCoordinates<KK>,KK>>
FieldSpacecraftStateInterpolator. getAbsPVAInterpolator()
Get absolute position-velocity-acceleration interpolator.Methods in org.orekit.propagation with parameters of type FieldAbsolutePVCoordinates Modifier and Type Method Description default <T extends CalculusFieldElement<T>>
double[][]CartesianToleranceProvider. getTolerances(FieldAbsolutePVCoordinates<T> absolutePVCoordinates)
Retrieve the integration tolerances given a reference absolute position-velocity vector.Constructors in org.orekit.propagation with parameters of type FieldAbsolutePVCoordinates Constructor Description FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva)
Build a spacecraft state from orbit only.FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva, FieldAttitude<T> attitude)
Build a spacecraft state from orbit and attitude.FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva, FieldAttitude<T> attitude, FieldArrayDictionary<T> additional)
Build a spacecraft state from orbit and attitude.FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva, FieldAttitude<T> attitude, T mass)
Build a spacecraft state from orbit, attitude and mass.FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva, FieldAttitude<T> attitude, T mass, FieldArrayDictionary<T> additional)
Build a spacecraft state from orbit, attitude and mass.FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva, FieldAttitude<T> attitude, T mass, FieldArrayDictionary<T> additional, FieldArrayDictionary<T> additionalDot)
Build a spacecraft state from orbit, attitude and mass.FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva, FieldArrayDictionary<T> additional)
Build a spacecraft state from orbit only.FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva, T mass)
Create a new instance from orbit and mass.FieldSpacecraftState(FieldAbsolutePVCoordinates<T> absPva, T mass, FieldArrayDictionary<T> additional)
Create a new instance from orbit and mass. -
Uses of FieldAbsolutePVCoordinates in org.orekit.propagation.conversion
Methods in org.orekit.propagation.conversion with parameters of type FieldAbsolutePVCoordinates Modifier and Type Method Description AbstractFieldIntegrator<T>
AbstractVariableStepFieldIntegratorBuilder. buildIntegrator(FieldAbsolutePVCoordinates<T> fieldAbsolutePVCoordinates)
Build a first order integrator.default AbstractFieldIntegrator<T>
FieldODEIntegratorBuilder. buildIntegrator(FieldAbsolutePVCoordinates<T> fieldAbsolutePVCoordinates)
Build a first order integrator.protected double[][]
AbstractVariableStepFieldIntegratorBuilder. getTolerances(FieldAbsolutePVCoordinates<T> fieldAbsolutePVCoordinates)
Computes tolerances. -
Uses of FieldAbsolutePVCoordinates in org.orekit.utils
Methods in org.orekit.utils that return FieldAbsolutePVCoordinates Modifier and Type Method Description protected FieldAbsolutePVCoordinates<KK>
FieldAbsolutePVCoordinatesHermiteInterpolator. interpolate(AbstractFieldTimeInterpolator.InterpolationData interpolationData)
Interpolate instance from given interpolation data.FieldAbsolutePVCoordinates<T>
FieldAbsolutePVCoordinates. shiftedBy(double dt)
Get a time-shifted state.FieldAbsolutePVCoordinates<T>
FieldAbsolutePVCoordinates. shiftedBy(T dt)
Get a time-shifted state.
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