航天器工程2019，Vol.28Issue(1)：35-41,7.DOI:10.3969/j.issn.1673-8748.2019.01.005
框架型柔性太阳电池阵展开机构动力学分析
Dynamic Analysis of Deployable Strut-mechanism for Flexible Solar Array
杨淑利 1刘志全 1黎彪 1刘颖 1陈艳平2
作者信息
- 1. 北京空间飞行器总体设计部,北京 100094
- 2. 北京卫星制造厂有限公司,北京 100094.
- 折叠
摘要
Abstract
With Kane dynamic theory,the multi-body dynamic models of deployable strut-mecha-nism have been established.The deployable style and deployable process of the struts have been studied,and compared with the calculation results by ADAMS software.The dynamic perform-ance of struts’deployment has been analyzed such as geometric position,velocity,and accelera-tion,and the inherent regularity of the forces of each hinge have been gained for deployable strut-mechanism.The results show that the rotation regularity of root-hinge calculated by the Kane method is basically the same as that of the ADAMS analysis for the single-module strut-mecha-nism,which illustrates the validity and correctness of the Kane method.For the four-module strut-mechanism,the farther away from the fixed root-hinge,the greater the amplitudes of the velocity and the acceleration change at the end of strut deployment.The force perpendicular to the deployment plane for the intermediate hinge is maximal in the initial state of deployment,and gradually decreases during the deployable process.The reasonable control of the driving torque of each hinge is the necessary condition for ensuring that the strut-mechanism is deployed according to the definite rule.The research results provide guidance for the detailed design of strut-mecha- nism for spacial flexible solar array.关键词
多模块框架型柔性太阳电池阵/展开机构/Kane方法/展开过程/动力学分析Key words
strut-type solar array with multiple models/deployable mechanism/Kane method/deployment process/dynamic analysis分类
航空航天引用本文复制引用
杨淑利,刘志全,黎彪,刘颖,陈艳平..框架型柔性太阳电池阵展开机构动力学分析[J].航天器工程,2019,28(1):35-41,7.
