Geometric perspectives on fundamental solutions in the linearized satellite relative motion problem

Author:

Burnett Ethan R.ORCID,Schaub HanspeterORCID

Funder

U.S. Department of Defense

National Defense Science and Engineering Graduate

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Terminal guidance system for satellite rendezvous;Clohessy;J. Aerosp. Sci.,1960

2. Rendezvous zu einem in elliptischer bahn umlaufenden ziel;Tschauner;Astronaut. Acta,1965

3. Motion in general elliptic orbit with respect to a dragging and precessing coordinate frame;Kechichian;J. Astronaut. Sci.,1998

4. J2 Invariant relative orbits for spacecraft formations;Schaub;Celestial Mech. Dynam. Astronom.,2001

5. The equations of relative motion in the orbital reference frame;Casotto;Celestial Mech. Dynam. Astronom.,2016

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