Micro-satellite attitude control real-time simulation was studied based on the mono-axis air-bearing table, which was supported by a micro-satellite project. The hardware structure of the micro-satellite air-bearing table was introduced and the software architecture for the simulation system was described; Real micro-satellite attitude control system was analyzed. According to the mission requirements, the real-time simulation focused on the micro-satellite three-axis attitude stable controlling and the large angle attitude maneuver problem. The simulation results show that the micro-satellite attitude control scheme is implemented and the control precision is satisfied to meet the mission requirements. The feasibility and reliability of the micro-satellite attitude control scheme is also verified.
Wang Xinsheng, Han Jianbin, Liang Bin, Li Jiyong.Micro-satellite attitude control real-time simulation based on mono-axis air-bearing table[J] JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2010,V36(7): 767-770