Closed-loop feedback control of spacecraft based on the component synthesis method

被引：0
|
作者：
Zhang, Jian-Ying [1 ]
Liu, Tun [1 ]
Zheng, Li-Wei [2 ]
机构：
[1] School of Aeronautics, Harbin Institute of Technology, Harbin 150001, China
[2] Beijing Institute of Astronautical Systems Engineering, Beijing 100076, China
来源：
Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology | 2010年 / 42卷 / 03期
关键词：
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摘要：
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页码：384 / 388
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