A Preliminary Study on Precise Attitude Switching Maneuver of Flexible Spacecraft Using CMG

Author:

TANAKA Takaaki1,KIDA Takashi1,NAGASHIO Tomoyuki1,OHTANI Takashi2,YAMAGUCHI Isao2,KASAI Tokio2,HAMADA Yoshiro2,SAKAI Shin-ichiro3,BANDO Nobutaka3

Affiliation:

1. The University of Electro-Communications

2. Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency

3. Institute of Space and Astronautical Sciences, Japan Aerospace Exploration Agency

Publisher

Japan Society of Mechanical Engineers

Reference6 articles.

1. (1) Kamiya, T., Maeda, K. and Ogura, N., Preshaping Profiler for Flexible Spacecraft Rest-to-Rest Maneuvers, AIAA Guidance Navigation and Control Conference, AIAA-2006-6181(2006).

2. (2) Attitude Control Committee ed., Spacecraft Dynamics and Control Handbook (in Japanese), (2007), Baifukan.

3. (3) Tanaka, T., Kida, T., Nagashio, T., Switching Maneuver of Flexible Spacecraft based on H-infinity Control using CMG, Proceedings of the 16th Space Engineering Conference, (2008), pp. 19-24.

4. (4) Nagashio, T., Kida, T., Mitani, S., Ohtani, T., Yamaguchi, T., Kasai, T., Hamada, Y., Igawa, H., Sakai, S., Bando, N., Nakamura, T., A Preliminary Controller Design Study on Precise Switching Maneuver of Flexible Spacecraft ASTRO-G, Proceedings of the 25th Guidance Control Symposium, (2008), pp. 25-32.

5. Self-scheduled H∞ control of linear parameter-varying systems: a design example

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