Attitude maneuvering and vibration damping of flexible spacecraft via robust adaptive backstepping technique

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作者：
Zhu, Liang-Kuan [1 ]
Ma, Guang-Fu [1 ]
Hu, Qing-Lei [1 ]
机构：
[1] Department of Control Science and Engineering, School of Astronautics, Harbin Institute of Technology, Harbin 150001, China
来源：
Zhendong yu Chongji/Journal of Vibration and Shock | 2009年 / 28卷 / 02期
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页码：132 / 136
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