CALCULATION AND SIMULATION OF THE SPACE MANIPULATOR EXPERIMENT

摘要：

A self-servicing system of satellite is one coupling system. The attitude of satellite is affected by the movements of a manipulator. According to the structure of the arm, a dynamic model of the self-servicing system is put forward. The operations of the self-servicing system are simulated in ADAMS, which result shows that different movement paths of the arm make different influence on the attitude of the satellite. In order to test the functions of the system, an experiment is done on the air-bearing platform. This paper calculates and simulates the movement path of the experiment system. The result is valuable to guide the experiment on the air-bearing platform.

关键词： dynamic model the self-servicing system the air bearing simulation.

作者: Tong Ying-xue Zuo Jian-hua Zhou Yong

作者单位: Shashi University,Shashi,China School of Mechanical Enigineering, Beijing Institute of Technology, Beijing, China

会议类型: 国际会议

会议名称: The International Conference on Advanced Technology of Design and Manufacture 2010(2010先进设计与制造技术国际研讨会)

会议地点: 北京

会议语种:英文

页码: 33-36

在线出版日期: 2010-11-23（万方平台首次上网日期，不代表论文的发表时间）