Attitude dynamics of a spacecraft with tip mass attached deploying flexible appendage

被引：0
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作者：
Shen, Shao-Ping [1 ]
Li, Zhi-Bin [1 ]
机构：
[1] Beijing Institute of Control Engineering, Beijing 100080, China
来源：
Zhendong yu Chongji/Journal of Vibration and Shock | 2008年 / 27卷 / 05期
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页码：115 / 118
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