Package org.orekit.propagation.relative.maneuver

Class YamanakaAnkersenManeuver

java.lang.Object

org.orekit.propagation.relative.maneuver.AbstractRelativeManeuver<YamanakaAnkersenProvider>

org.orekit.propagation.relative.maneuver.YamanakaAnkersenManeuver

All Implemented Interfaces:

DetectorModifier, EventDetector, RelativeManeuver

public class YamanakaAnkersenManeuver
extends AbstractRelativeManeuver<YamanakaAnkersenProvider>

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
YamanakaAnkersenManeuver(EventDetector trigger, Vector3D deltaV, YamanakaAnkersenProvider 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(Orbit 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.AbstractRelativeManeuver

getDeltaV, getDetector, getForward, getHandler, getRelativeProvider, init, toString, toString

Methods inherited from class java.lang.Object

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

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

finish, g, getDetectionSettings, getEventFunction, reset

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

getMaxCheckInterval, getMaxIterationCount, getThreshold

Constructor Details

YamanakaAnkersenManeuver

public YamanakaAnkersenManeuver(EventDetector trigger,
 Vector3D deltaV,
 YamanakaAnkersenProvider 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(Orbit 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.