Package org.orekit.propagation.relative.maneuver

Class FieldYamanakaAnkersenManeuver<T extends CalculusFieldElement<T>>

java.lang.Object

org.orekit.propagation.relative.maneuver.FieldAbstractRelativeManeuver<T,FieldYamanakaAnkersenProvider<T>>

org.orekit.propagation.relative.maneuver.FieldYamanakaAnkersenManeuver<T>

Type Parameters:

T - Any scalar field.

All Implemented Interfaces:

FieldDetectorModifier<T>, FieldEventDetector<T>, FieldRelativeManeuver<T>

public class FieldYamanakaAnkersenManeuver<T extends CalculusFieldElement<T>>
extends FieldAbstractRelativeManeuver<T,FieldYamanakaAnkersenProvider<T>>

Implements an impulse maneuver for a chaser spacecraft whose relative orbit is defined by the Yamanaka-Ankersen equations.

Since:

14.0

Author:

Romain Cuvillon

Constructor Summary

Constructors

Constructor	Description
FieldYamanakaAnkersenManeuver(FieldEventDetector<T> trigger, FieldVector3D<T> deltaV, FieldYamanakaAnkersenProvider<T> chaserAdditionalEquations)	Creates a new YamanakaAnkersenManeuver object from a trigger event, a ΔV vector, and an associated frame.

Method Summary

Modifier and Type	Method	Description
void	resetTrueAnomalyAtManeuver(FieldOrbit<T> orbit)	Reset True Anomaly of the target orbit in the provider to the true anomaly of the last target state.

Methods inherited from class org.orekit.propagation.relative.maneuver.FieldAbstractRelativeManeuver

getDeltaV, getDetector, getForward, getHandler, getRelativeProvider, init

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Methods inherited from interface org.orekit.propagation.events.FieldDetectorModifier

finish, g, getDetectionSettings, getEventFunction, reset

Methods inherited from interface org.orekit.propagation.events.FieldEventDetector

getMaxCheckInterval, getMaxIterationCount, getThreshold

Constructor Details

FieldYamanakaAnkersenManeuver

public FieldYamanakaAnkersenManeuver(FieldEventDetector<T> trigger,
 FieldVector3D<T> deltaV,
 FieldYamanakaAnkersenProvider<T> chaserAdditionalEquations)

Creates a new YamanakaAnkersenManeuver object from a trigger event, a ΔV vector, and an associated frame.

Parameters:

trigger - Trigger event that triggers the maneuver of the chaser spacecraft.

deltaV - ΔV vector in the target's LVLH CCSDS LOF.

chaserAdditionalEquations - Chaser's additional equations provider

Method Details

resetTrueAnomalyAtManeuver

public void resetTrueAnomalyAtManeuver(FieldOrbit<T> orbit)

Reset True Anomaly of the target orbit in the provider to the true anomaly of the last target state. It keeps the same orbit but modifies the true anomaly. Useful only for Yamanaka-Ankersen model. Do nothing if CW.

Parameters:

orbit - orbit of the target.