Robust Attitude Control of Large Flexible Spacecraft (Application of Input Constrained Model Predictive Control)

Author:

YAMASHITA Tetsuo1,HAMADA Yoshiro,YAMAGUCHI Isao,NAGASHIO Tomoyuki,KIDA Takashi

Affiliation:

1. University of Electro-Communications

Publisher

Japan Society of Mechanical Engineers

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials

Reference18 articles.

1. (1) Nagashio, T., Kida, T., Ohtani, T., Hamada, Y., Yamaguchi, I., Kasai, T., Igawa, T. and Mitani, S., “On-orbit Experiment Results of Robust Symmetric Attitude Controller for ETS-VIII spacecraft”, 18th IFAC Symposium on Automatic Control in Aerospace (2010).

2. (2) Hamada, Y., Ohtani, T., Kida, T. and Nagashio, T., “Gain Scheduling Controller Design for Engineering Test Satellite VIII”, 17th IFAC Symposium on Automatic Control in Aerospace (2007).

3. (3) Kamiya, T., Ogura, N., Haruma, H., K.Maeda, Sakai, S., Bando, N. and Nakamura, T., “Preshaping Profiler for ASTRO-G Rest-to-Rest Maneuvers”, Proc. of 7th International ESA Conference on Guidance, Navigation and Control Systems (2008).

4. (4) Tanaka, T., Kida, T., Nagashio, T., Ohtani, T., Yamaguchi, I., Kasai, T., Hamada, Y., Sakai, S. and Bando, N., “A Preliminary Study on Precise Attitude Switching Maneuver of Flexible Spacecraft”, Journal of Space Engineering, Vol.2, No.1 (2009), pp. 12-24.

5. (5) Mayne, D.Q., Rawlings, J.B., Rao, C.V., and Scokaert, P.O., “Constrained model predictive control: Stability and optimality”, Automatica, Vol.36, No.6 (2000) pp. 789-814.

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