Equations of Motion for the Automatic Balancing System of 3-DOF Spacecraft Attitude Control Simulator

摘要：

3-DOF spacecraft attitude control simulators have been used for spacecraft attitude determination and control hardware verification and software development. In this paper, a automatic balancing system to reduce the gravitational torques influencing the motion of the simulator was described. The equations of motion and balancing algorithm developed for the system was deduced. The algorithm takes sensor data from the system and gives a vector estimating the location of the center of mass of the platform. It can be shown from the simulated result that the locations of the center of mass are large at first, and begin to diminish rapidly after a 60-second test length is in the automatic balancing algorithm.

作者: Yanbin Li Youhua Gao

作者单位: School of Mechanical Engineering,Shenyang University of Technology. School of Electrical Engineering,Shenyang University of Technology.

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: 244-248

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）