Cable control model for spacecraft attitude and vibrations

被引:0
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作者
Guo, Tieneng [1 ]
Lu, Qiuhai [1 ]
Ge, Dongyun [1 ]
Ren, Gexue [1 ]
机构
[1] Department of Aerospace, School of Aerospace, Tsinghua University, Beijing 100084, China
关键词
Cable control - Flexible rigid coupling - Linear quadratic Gaussian theory - Modal superposition method - Simultaneous control;
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页码:1498 / 1501
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