摘要
随着中国深空探测的发展,在月球表面进行着陆探测成为新的关注热点,因此月球着陆器的着陆稳定性研究成为一项重要课题。文章利用ADAMS软件及其用户子程序,对一种可展开四腿式月球着陆器的着陆稳定性进行了研究,研究结论为着陆器的着陆缓冲机构及总体设计提供参考。
With the development of deep space exploration,China has focused on lunar surface exploration after landing,and landing stability of lunar Lander turns to be an important task.In this paper,landing stability of lunar Lander with a type of deployable four-legged landing gear was studied by simulation with ADAMS software and its subroutine,which could supply references to the soft-landing gear of lunar lander and overall design.
出处
《航天返回与遥感》
2010年第6期16-22,共7页
Spacecraft Recovery & Remote Sensing
基金
国家重大科技专项工程
