Dynamic modeling and orbit maneuvering response analysis for a three-axis attitude stabilized large scale flexible spacecraft installed with hinged solar arrays
出版年份 2021 全文链接
标题
Dynamic modeling and orbit maneuvering response analysis for a three-axis attitude stabilized large scale flexible spacecraft installed with hinged solar arrays
作者
关键词
Large scale flexible spacecraft, Hinged multi-panel structure, Analytical global modes, Characteristic orthogonal polynomials, Mode interchanged phenomenon, Dynamic responses
出版物
MECHANICAL SYSTEMS AND SIGNAL PROCESSING
Volume 162, Issue -, Pages 108083
出版商
Elsevier BV
发表日期
2021-06-12
DOI
10.1016/j.ymssp.2021.108083
参考文献
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