Robust Control of Spacecraft with Mobile Appendages
Author:
Affiliation:
1. Graduate School of Electro-Communications, University of Electro-Communications
2. Department of Mechanical Engineering and Intelligent Systems, University of Electro-Communications
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/44/143/44_143_40/_pdf
Reference8 articles.
1. 1) Nagashio, T. and Kida, T.: Attitude Control of Spacecraft with Mobile Antenna by Gain Scheduled H∞ Controller, Trans. Japan Soc. Aero. Space Sci., 43 (2000), pp. 16–22.
2. 2) Yamada, K. and Yoshikawa, S.: Adaptive Attitude Control for an Artificial Satellite with Mobile Bodies, AIAA J. Guid. Control Dyn., 19 (1996), pp. 948–953.
3. 3) Apkarian, P., Gahinet, P. and Becker, G.: Self-Scheduled H∞ Control of Linear Parameter Varying Systems, Automatica, 31 (1995), pp. 1251–1261.
4. 4) Itoh, H., Kobayashi, O., Sampei, M., Liu, K. Z. and Mita, T.: H∞ Frequency Separate Control of 2 Carts System, Proc. of 21th SICE Symposium on Control Theory, Aichi, 1992, pp. 121–126.
5. 5) Likins, P. W.: Elements of Engineering Mechanics, McGraw-Hill, Tokyo, 1973.
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