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显示多体动力学方程自动编制技术.

Authors :
李瑾岳
胡权
张景瑞
Source :
Chinese Space Science & Technology / Zhongguo Kongjian Kexue Jishu. 2017, Vol. 37 Issue 1, p49-56. 8p.
Publication Year :
2017

Abstract

The development of the complex multibody spacecraft raises higher requirement to multi-body dynamics modeling and control technology. The explicit dynamics equations of the system are always needed to analyze system's characteristics and design controllers, but the complexity of system brings difficulty to deriving the equations. In order to solve this problem, the explicit form of dynamics equations' analytical expression was inferred by using Kane's method, the chain structure system's explicit dynamics equations; then, by analyzing this equation, physical meaning and regularities of distribution of each equation item were established; using those regularities, a program that can output the explicit dynamics equations of spacecraft system with tree structure was developed. This program reduces the workload of modeling this type of spacecraft significantly. [ABSTRACT FROM AUTHOR]

Details

Language :
Chinese
ISSN :
1000758X
Volume :
37
Issue :
1
Database :
Academic Search Index
Journal :
Chinese Space Science & Technology / Zhongguo Kongjian Kexue Jishu
Publication Type :
Periodical
Accession number :
123924622
Full Text :
https://doi.org/10.16708/j.cnki.1000-758X.2017.0005