Agile and Precise Attitude Switching Maneuver of Flexible Spacecraft based on Nonstationary Frequency-Shaped Robust Control-Reference-Cited by-同舟云学术

Agile and Precise Attitude Switching Maneuver of Flexible Spacecraft based on Nonstationary Frequency-Shaped Robust Control

Published:2011 Issue:5 Volume:5 Page:805-818
ISSN:1881-3046
Container-title:Journal of System Design and Dynamics
language:en
Short-container-title:JSDD

Author:

IKEDA Ryota¹,TAKAHASHI Masaki²

Affiliation:

1. Keio University, School of Science for Open and Environmental Systems

2. Keio University, Department of System Design Engineering

Publisher

Japan Society of Mechanical Engineers

Link

http://www.jstage.jst.go.jp/article/jsdd/5/5/5_5_805/_pdf

Reference13 articles.

1. Active control of flexible systems

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

3. (3) Nakamura, T., Bando, N., Sakai, S., Saito, H., Agile and robust attitude control system for VSOP-2 satellite “ASTRO-G”, 10th IEEE International Workshop on Advanced Motion Control, (2008), pp.578-583.

4. (4) Nakamura, T., Bando, N., Sakai, S., Saito, H., Design of Reference for High-Speed and Vibration-Less Attitude Maneuvering of Flexible Satellite, Journal of The Japan Society for Aeronautical and Space Sciences, Vol. 58, No. 682 (2010), pp.309-315.

5. (5) Kida, T., Yamaguchi, I., Chida, Y. and Sekiguchi, T., On-orbit Robust Control Experiment of Flexible Spacecraft ETS-VI, AIAA Journal of Guidance, Control, and Dynamics, Vol. 20, No. 5 (1997), pp. 865-872.

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