Research of Attitude Decouple Control of the Multiple Satellites System Based on Predictive Control
In this paper, we base on the analysis of kinetics and kinematics equations of the multiple satellites system. Using the theory of predictive control, we realize the decouple control method when the system has large movement of euler angles under the condition of inertia coupling, control moment coupling and angular velocity coupling. Through the simulation results, it can prove that the method is high precision, high robust and low quantity of computation.
attitude control decouple predictive control
Liu Zhijian Wu Meiping
Department of Automatic Control, National University of Defence Technology, Changsha, 410073
国际会议
北京
英文
314-319
2007-11-04（万方平台首次上网日期，不代表论文的发表时间）