Nutational Stability of a Satellite Equipped with an Active Magnetic Momentum Wheel
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概要
- 論文の詳細を見る
This paper deals with an influence of the magnetically suspended rotor on the satellite motion; although cross-feedbacks in the magnetic bearing provide stability margin to the rotor gyroscopic motion, they may destabilize the satellite nutation. Stability analyses about the dynamical interaction between the satellite and the magnetically suspended rotor whose controller used three types of (proportional, integral and derivative) cross-feedbacks were performed. The results indicated that they had significant effects on the rotor and the satellite motion.
- 宇宙航空研究開発機構の論文
著者
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NAKAJIMA Atsushi
National Aerospace Laboratory of Japan
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Nakajima A
National Aerospace Lab. Japan
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INOUE Masao
Mitsubishi Electric Corporation
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TSUCHIYA Kazuo
Mitsubishi Electric Corporation
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MURAKAMI Chikara
Tokyo Metropolitan Institute of Technology
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Murakami C
Univ. Tsukuba Ibaraki
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Inoue M
Mitsubishi Electric Corporation
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Nakajima Atsushi
National Aerospace Laboratory
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MURAKAMI Chikara
Department of Physics, University of Kyoto
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