Package org.orekit.propagation.relative.yamanakaankersen

package org.orekit.propagation.relative.yamanakaankersen

This package provides an implementation of the equations of Yamanaka and Ankersen.

Yamanaka-Ankersen equations are analytical equations extending the equations of Clohessy and Wiltshire to any eccentric orbits. These equations are only valid under the assumption of Keplerian dynamics.

In this package:

• YamanakaAnkersenProvider implements AdditionalDataProvider to propagate the chaser state together with the target state as an AdditionalData.
• YamanakaAnkersenRendezVous computes a TwoImpulseTransfer to realize a rendezvous with the target in a chosen duration.

All the references for the equations in the code come from :
NEW STATE TRANSITION MATRIX FOR RELATIVE MOTION ON AN ARBITRARY ELLIPTICAL ORBIT
Koji Yamanaka, Finn Ankersen
Journal of Guidance, Control, and Dynamics, Vol. 25, No. 1
January-February 2002.

Related Packages

Package	Description
org.orekit.propagation.relative	Top level package for relative motion propagation.
org.orekit.propagation.relative.clohessywiltshire	This package provides an implementation of the equations of Clohessy and Wiltshire.
org.orekit.propagation.relative.maneuver	This package implements relative impulse maneuver of a chaser spacecraft in regard to a target by extending EventDetector interface.

Classes

Class	Description
FieldYamanakaAnkersenEquations<T extends CalculusFieldElement<T>>	This class implements the state transition matrices of the Yamanaka-Ankersen equations of relative motion between two spacecrafts.
FieldYamanakaAnkersenMatrices<T extends CalculusFieldElement<T>>	This class stores the 2 matrices (in plane: xz, out of plane: y, in local LVLH CCSDS frame) of the Yamanaka Ankersen equations.
FieldYamanakaAnkersenProvider<T extends CalculusFieldElement<T>>	This additional state provider implements the Yamanaka-Ankersen equations of relative motion to propagate the relative orbit of a chaser spacecraft around the target spacecraft whose orbit is being propagated.
FieldYamanakaAnkersenRendezVous<T extends CalculusFieldElement<T>>	This class implements the solution to the Yamanaka-Ankersen equations for a two-impulse rendez-vous as presented in the Ankersen thesis.
YamanakaAnkersenEquations	This class implements the state transition matrices of the Yamanaka-Ankersen equations of relative motion between two spacecrafts.
YamanakaAnkersenMatrices	This class stores the 2 matrices (in plane: xz, out of plane: y, in Local LVLH CCSDS frame) of the Yamanaka Ankersen equations.
YamanakaAnkersenProvider	This additional state provider implements the Yamanaka-Ankersen equations of relative motion to propagate the relative orbit of a chaser spacecraft around the target spacecraft whose orbit is being propagated.
YamanakaAnkersenRendezVous	This class implements the solution to the Yamanaka-Ankersen equations for a two-impulse rendez-vous as presented in the Ankersen thesis.