Calculation and simulation of the space manipulator experiment
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 selfservicing 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.
component dynamic model the self-servicing system the air bearing simulation
Lu Ji-ping Tang Shui-yuan Yan Yan Miao Ke-fei
School of Mechanical and Vehicular Engineering Beijing Institute of Technology Beijing,China School of Mechanical and Vehicular Engineering Beijing Institute of Technology Beijing, China
国际会议
厦门
英文
74-78
2010-10-29（万方平台首次上网日期，不代表论文的发表时间）