摘要
利用MSCAdams软件的参数化建模和二次开发功能,建立专为航天器太阳翼展开分析设计的仿真模块,为用户提供自动、快速的建模环境,使得进行航天器太阳翼展开过程的运动学和动力学分析工作效率更高、扩展方便,通过优化设计为设计者提供最优的设计参数.
Applying the modelling parameters and secondary functions deployment of MSC Adams, the special design analysis and simulation module for spacecraft solar array deployment is established which makes the kinematic and dynamics analysis for solar array deployment efficient and expansion convenient through optimized design for designers to provide optimal design parameters.
出处
《计算机辅助工程》
2006年第B09期12-14,共3页
Computer Aided Engineering
