Dynamic modeling for flexible spacecraft appendages with nonlinear deformation

被引：0
|
作者：
Deng, Fengyan [1 ]
He, Xingsuo [1 ]
Li, Liang [1 ]
Zhang, Juan [1 ]
Zhao, Chunyan [1 ]
机构：
[1] Northwestern Polytechnical University, Xi'an 710072, China
来源：
Yingyong Lixue Xuebao/Chinese Journal of Applied Mechanics | 2006年 / 23卷 / 04期
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页码：555 / 562
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