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Volume 40 Issue 11
Nov.  2014
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Journal of Beijing University of Aeronautics and Astronautics  > 2014  >  40(11): 1581-1588.
Song Fei, Qin Shiyin. On-orbit real-time health assessment of satellite attitude control system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(11): 1581-1588. doi: 10.13700/j.bh.1001-5965.2014.0057(in Chinese)
Citation: Song Fei, Qin Shiyin. On-orbit real-time health assessment of satellite attitude control system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(11): 1581-1588. doi: 10.13700/j.bh.1001-5965.2014.0057(in Chinese)
shu

On-orbit real-time health assessment of satellite attitude control system

doi: 10.13700/j.bh.1001-5965.2014.0057

  • School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 12 Feb 2014
  • Publish Date: 20 Nov 2014
    Abstract
  • According to technique requirements of on-orbit autonomous intelligent management and control for spacecrafts, especially for satellite systems, an on-orbit real-time health assessment method for satellite attitude control systems was proposed based on a multi-level fuzzy comprehensive evaluation framework. In view of performance characteristics and actual capabilities, a satellite attitude control system was divided into three parts of attitude measurement, actuating mechanism and attitude control. In this way, its health level may be determined by health status of three parts so that the fuzzy evaluation for every part was carried out at first and then the integrative health performance was given through synthetically weighted integration with the ones of three parts. Therefore a synthetic integration strategy with variable weights for different health conditions of various parts was employed to complete the comprehensive evaluation of satellite attitude control systems according to variable weight synthesizing principle, in which the variable weights depended on the membership degree of health level of various parts. Simulation experiment results demonstrate that the proposed health assessment method can achieve on-orbit real-time health assessment of satellite attitude control system effectively and efficiently.

     

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