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��͢��, ���*
�������պ����ѧ ����ϵͳ����ϵ, ���� 100083
Integrated flexible reliability and fault diagnosis design technique
Zhao Tingdi, Tian Jin*
Dept. of System Engineering of Engineering Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

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Abstract�� 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.
Keywords�� satellites   fault analysis   flexible design   mission reliability     
Received 2006-06-12;
About author: ��͢��(1965-), ��, ����������, ����,ztd@buaa.edu.cn.
��͢��, ���.���Կɿ����������ϴ����ۺ���Ƽ���[J]  �������պ����ѧѧ��, 2006,V32(10): 1205-1208
Zhao Tingdi, Tian Jin.Integrated flexible reliability and fault diagnosis design technique[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2006,V32(10): 1205-1208
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