Uses of Interface
org.orekit.propagation.relative.maneuver.RelativeManeuver

Packages that use RelativeManeuver

Package	Description
org.orekit.control.relative	Package relative provides classes to compute typical maneuvers of relative proximity operations (RPO).
org.orekit.propagation.relative.maneuver	This package implements relative impulse maneuver of a chaser spacecraft in regard to a target by extending EventDetector interface.

Uses of RelativeManeuver in org.orekit.control.relative

Methods in org.orekit.control.relative that return types with arguments of type RelativeManeuver

Modifier and Type	Method	Description
List<RelativeManeuver>	RPO.computeForcedManeuvers(List<TimeStampedPVCoordinates> waypoints, Vector3D initialVelocity, Orbit targetOrbit, RelativeProvider provider)	Compute relative maneuvers to realize a forced trajectory defined by the waypoints (ForcedLinear/ForcedCircular).
List<RelativeManeuver>	RPO.computeTeardropManeuvers(List<TimeStampedPVCoordinates> waypoints, RelativeProvider relativeProvider)	Computes the relative maneuvers of the teardrop relative orbit in the RPOModel Local Orbital Frame.

Method parameters in org.orekit.control.relative with type arguments of type RelativeManeuver

Modifier and Type	Method	Description
default List<ImpulseManeuver>	RPO.convertToImpulseManeuver(List<RelativeManeuver> maneuvers, Orbit targetOrbit, double isp)	Convert the relative maneuvers into Impulse maneuvers in the targetOrbit frame.

Uses of RelativeManeuver in org.orekit.propagation.relative.maneuver

Classes in org.orekit.propagation.relative.maneuver that implement RelativeManeuver

Modifier and Type	Class	Description
class	AbstractRelativeManeuver<P extends RelativeProvider>	Abstract class for implementing an impulse maneuver for a chaser spacecraft.
class	ClohessyWiltshireManeuver	Implements an impulse maneuver for a chaser spacecraft whose relative orbit is defined by the Clohessy-Wiltshire equations.
class	YamanakaAnkersenManeuver	Implements an impulse maneuver for a chaser spacecraft whose relative orbit is defined by the Yamanaka-Ankersen equations.