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

关键词：

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：555 / 562

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