Package org.orekit.propagation.relative.maneuver

Interface FieldRelativeManeuver<T extends CalculusFieldElement<T>>

Type Parameters:

T - type of the field element

All Superinterfaces:

FieldDetectorModifier<T>, FieldEventDetector<T>

All Known Implementing Classes:

FieldAbstractRelativeManeuver, FieldClohessyWiltshireManeuver, FieldYamanakaAnkersenManeuver

public interface FieldRelativeManeuver<T extends CalculusFieldElement<T>>
extends FieldDetectorModifier<T>

Interface for implementing an impulse relative maneuver.

Since:

14.0

Author:

Romain Cuvillon

Method Summary

Modifier and Type	Method	Description
FieldVector3D<T>	getDeltaV()	Getter for the ΔV vector of the maneuver.
FieldRelativeProvider<T>	getRelativeProvider()	Getter for the relative provider.
default 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 interface org.orekit.propagation.events.FieldDetectorModifier

finish, g, getDetectionSettings, getDetector, getEventFunction, getHandler, init, reset

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

getMaxCheckInterval, getMaxIterationCount, getThreshold

Method Details

getDeltaV

FieldVector3D<T> getDeltaV()

Getter for the ΔV vector of the maneuver.

Returns:

The ΔV vector of the maneuver, expressed in the target spacecraft's LOF.

getRelativeProvider

FieldRelativeProvider<T> getRelativeProvider()

Getter for the relative provider.

Returns:

relative motion provider.

resetTrueAnomalyAtManeuver

default 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.