Attitude dynamics of a spacecraft with deploying flexible appendages

被引：0

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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D O I：

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学科分类号：

摘要：

(Edited Abstract)

引用

页码：35 / 40

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[1] TRANSIENT ATTITUDE DYNAMICS OF SATELLITES WITH DEPLOYING FLEXIBLE APPENDAGES
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