Dynamics of tethered satellite system with a time-varying number of degrees-of-freedom

被引：0
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作者：
Yu, Bensong [1 ]
Wen, Hao [1 ]
Jin, Dongping [1 ]
机构：
[1] MOE Key Lab. of Mechanics and Control for Aerospace Structures, Institute of Vibration Engineering Research, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
来源：
Lixue Xuebao/Chinese Journal of Theoretical and Applied Mechanics | 2010年 / 42卷 / 05期
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页码：926 / 932
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