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�������պ����ѧѧ�� 2010, Vol. 36 Issue (7) :767-770    DOI:
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1. �������պ����ѧ �ѧԺ, ���� 100191;
2. ��������ҵ��ѧ �ռ�����ϵͳ�о���, ������ 153001
Micro-satellite attitude control real-time simulation based on mono-axis air-bearing table
Wang Xinsheng1, Han Jianbin1, Liang Bin2, Li Jiyong2*
1. School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
2. Space Intelligence System Institute, Harbin Institute of Technology, Harbin 153001, China

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Abstract�� 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.
Keywords�� attitude control   mono-axis air-bearing table   real-time simulation   micro-satellite     
Received 2009-05-10;
Fund:

����863�ƻ�������Ŀ(2007AA704340,2007AA704115)

About author: ������(1973-),��,������������,��ʦ,xswang@buaa.edu.cn.
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������, ������, ����, �����.��������̨��΢С������̬����ʵʱ����[J]  �������պ����ѧѧ��, 2010,V36(7): 767-770
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
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