Volume 32 Issue 10
Oct.  2006
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Zhao Tingdi, Tian Jin. Integrated flexible reliability and fault diagnosis design technique[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(10): 1205-1208. (in Chinese)
Citation: Zhao Tingdi, Tian Jin. Integrated flexible reliability and fault diagnosis design technique[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(10): 1205-1208. (in Chinese)

Integrated flexible reliability and fault diagnosis design technique

  • Received Date: 12 Jun 2006
  • Publish Date: 31 Oct 2006
  • In order to meet the demand that modern satellite be high-reliability and long-life, flexible restructuring was executed among the components insides atellite or among the satellites in a mission group, by means of grid and multi-disciplinary technology, based on characteristics of digitalized system or equipment of satellite and over-all properties of system. Thus system reliability ofsatellite or satellite group could be increased. A technique that integrates flexible reliability design, testing and fault diagnosis/recovery processing was put forward, and design & analysis to reliability, testability and fault diagnosis/recovery was combined with design to function/performance of products. The corresponding integrated design & analysis model was established, and simulation for application was carried on. Therefore, the digitalized system or equipment of satellite could be ensured simple-structured, low-cost and reliable.

     

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