Touchdown dynamic modeling and simulation of lunar lander

摘要：

In this paper, the key influences of lunar lander landing model are illuminated systematic. Then the touchdown dynamic model of lunar module is built. And the simulation model for lunar landing described on ADAMS is discussed. As an example, one kind of lunar module model with four cantilever truss style landing gear is built by ADAMS and the simulations are focused on the influences on landing by the characteristics of buffers in primary and secondary struts of the landing gear. The conclusions can be used for the design of lunar lander.

作者: Yi Sun Yabing Hu Rongqiang Liu Zongquan Den

作者单位: Department of Astronautic Science and Mechanics,Harbin Institute of Technology,Harbin 150001 People School of Mechatronics Engineering,Harbin Institute of Technology,Harbin 150001 Peoples Republic of

会议类型: 国际会议

会议名称: The 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(第三届航空航天系统与控制国际会议 ISSCAA 2010)

会议地点: 哈尔滨

会议语种:英文

页码: 1308-1312

在线出版日期: 2010-01-08（万方平台首次上网日期，不代表论文的发表时间）