Attitude dynamics of a spacecraft with deploying flexible appendages

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作者：
Li, Junfeng [1 ]
Wang, Zhaolin [1 ]
机构：
[1] Tsinghua Univ, Beijing, China
来源：
Qinghua Daxue Xuebao/Journal of Tsinghua University | 1996年 / 36卷 / 10期
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(Edited Abstract)
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页码：35 / 40
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