Suboptimal formation reconfiguration of satellites under input directional constraints

Author:

Yoshimura Yasuhiro

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference18 articles.

1. In-plane motion control of Hill–Clohessy–Wiltshire equations by single input;Bando;J. Guidance Control Dyn.,2013

2. Mathematical Methods in the Physical Sciences;Boas,2006

3. Optimal power-limited rendezvous with upper and lower bounds on thrust;Carter;J. Guidance Control Dyn.,1996

4. PROBA-3 mission;Castellani;Int. J. Space Sci. Eng.,2013

5. Analytic solution to optimal reconfigurations of satellite formation flying in circular orbit under perturbation;Cho;IEEE Trans. Aerosp. Electron. Syst.,2012

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