Optimized design of controller parameters for large angle spacecraft attitude maneuvers

被引:0
|
作者
Jin, Jin [1 ]
Zhang, Jingrui [1 ]
Liu, Zaozhen [1 ]
机构
[1] School of Aerospace Science and Engineering, Beijing Institute of Technology, Beijing 100081, China
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摘要
7
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页码:289 / 292
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