State transition matrix for long-distance formation with J2 in eccentric orbits-Reference-Cited by-同舟云学术

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State transition matrix for long-distance formation with J2 in eccentric orbits

Published:2014-08 Issue: Volume:101 Page:33-41
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Kimura Masaya,Yamada Katsuhiko

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference24 articles.

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

2. Optimal Trajectories for Space Navigation;Lawden,1963

3. Rendezvous zu einem in elliptischer bahn um laufenden ziel;Tschauner;Astronaut. Acta,1965

4. Time-explicit representation of relative motion between elliptical orbits;Melton;J. Guid. Control Dyn.,2000

5. Relative motion in highly elliptical orbits;Garrison;Adv. Astronaut. Sci.,1995

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Exact Computation of High-Order State Transition Tensors for Perturbed Orbital Motion;Journal of Guidance, Control, and Dynamics;2019-06

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