Nonlinear Dynamic Modeling for a Flexible Laminated Composite Appendage Attached to a Spacecraft Body Undergoing Deployment and Locking Motions

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作者：
You, Bin Di [1 ]
Wen, Jian Min [1 ]
Zhang, Guang Yu [2 ]
Zhao, Yang [3 ]
机构：
[1] School of Naval Architecture and Ocean Engineering, Harbin Institute of Technology, Weihai, Shandong,264209, China
[2] School of Mechanical and Electrical Engineering, Harbin Institute of Technology, Harbin, Heilongjiang,150001, China
[3] School of Astronautics Engineering, Harbin Institute of Technology, Harbin, Heilongjiang,150001, China
来源：
Journal of Aerospace Engineering | 2016年 / 29卷 / 05期
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