Flexible spacecraft attitude control system design using wheels

被引:0
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作者
Geng, Y. [1 ]
Cui, H. [1 ]
Cui, H. [1 ]
Yang, D. [1 ]
机构
[1] School of Astronautics, Harbin Institute of Technology, Harbin 150001, China
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6
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页码:55 / 58
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