Volume 36 Issue 7
Jul.  2010
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Wang Xinsheng, Han Jianbin, Liang Bin, et al. Micro-satellite attitude control real-time simulation based on mono-axis air-bearing table[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(7): 767-770. (in Chinese)
Citation: Wang Xinsheng, Han Jianbin, Liang Bin, et al. Micro-satellite attitude control real-time simulation based on mono-axis air-bearing table[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(7): 767-770. (in Chinese)

Micro-satellite attitude control real-time simulation based on mono-axis air-bearing table

  • Received Date: 10 May 2009
  • Publish Date: 30 Jul 2010
  • 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.

     

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