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《Journal of Beijing University of Aeronautics and Astronautics》 2006-10
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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)  
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 multidisciplinary technology,based on characteristics of digitalized system or equipment of satellite and over-all properties of system.Thus system reliability of satellite 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.
【CateGory Index】: V467
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【Co-citations】
Chinese Journal Full-text Database 1 Hits
1 Wu Tingyuan Liu Jianye Yu Feng Xiong Zhi (NUAA,Nanjing 210016,China);Satellite Attitude Determination Based on Redundant Gyro System and Star Sensor[J];Computer Measurement & Control;2008-05
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