Spacecraft control method for fast attitude maneuver and stabilization

被引：0
|
作者：
Lei, Yongjun [1 ,2 ]
Tan, Shuping [1 ,2 ]
Liu, Yiwu [1 ,2 ]
机构：
[1] Beijing Institute of Control Engineering, Beijing 100190, China
[2] National Laboratory of Space Intelligent Control, Beijing 100190, China
来源：
Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology | 2010年 / 30卷 / 05期
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页码：48 / 53
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