摘要
建立了有内导向瓣周边式对接机构的两空间飞行器对接过程中捕获阶段和缓冲阶段的对接动力学数学模型，进行了数值仿真．通过仿真计算可以验证缓冲系统的设计参数及对接策略，得到对接机构的相对位移和转角、缓冲系统的位移和转角、相互作用力等参数，从而可较全面地了解对接动力学过程，为缓冲系统的设计打下一个可信的基础．
The mathematical models of docking dynamics in the process of capture and buffering are established for two spacecraft with inner guided petal peripheral docking mechanisms. The docking shategr and design parameters of buffer , such as displacement and rotation of buffers and relative displacement and rotation of docking mechanisms, interacting forces are obtained through simulation calculation, so that docking dynamics can be undestood better and a sound basis is provided for design of buffer system.
出处
《哈尔滨工业大学学报》
EI
CAS
CSCD
北大核心
1999年第4期121-124,共4页
Journal of Harbin Institute of Technology
