FieldClohessyWiltshireManeuver.java
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*
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package org.orekit.propagation.relative.maneuver;
import org.hipparchus.CalculusFieldElement;
import org.hipparchus.geometry.euclidean.threed.FieldVector3D;
import org.orekit.propagation.events.FieldEventDetector;
import org.orekit.propagation.relative.clohessywiltshire.FieldClohessyWiltshireProvider;
/**
* Implements an impulse maneuver for a chaser spacecraft whose relative orbit is defined by the Clohessy-Wiltshire
* equations.
*
* @param <T> Any scalar field.
* @author Romain Cuvillon
* @since 14.0
*/
public class FieldClohessyWiltshireManeuver<T extends CalculusFieldElement<T>>
extends FieldAbstractRelativeManeuver<T, FieldClohessyWiltshireProvider<T>> {
/**
* Creates a new FieldClohessyWiltshireManeuver object from a trigger event, a ΔV vector, and an associated frame.
*
* @param trigger Trigger event that triggers the maneuver of the chaser spacecraft.
* @param deltaV ΔV vector in the target's QSW LOF.
* @param chaserAdditionalEquations Chaser's additional equations provider
*/
public FieldClohessyWiltshireManeuver(final FieldEventDetector<T> trigger,
final FieldVector3D<T> deltaV,
final FieldClohessyWiltshireProvider<T> chaserAdditionalEquations) {
super(trigger, deltaV, chaserAdditionalEquations);
}
}