Flexible spacecraft attitude control system design using wheels

被引：0
|
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
来源：
Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics | 2001年 / 23卷 / 06期
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学科分类号：
摘要：
6
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页码：55 / 58
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