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基于SINS/GPS/CNS的机载综合导航系统故障诊断方法研究
引用本文:刘长华,傅强,宋华.基于SINS/GPS/CNS的机载综合导航系统故障诊断方法研究[J].中国民航飞行学院学报,2011,22(1):23-27.
作者姓名:刘长华  傅强  宋华
作者单位:1. 中国民航飞行学院,四川广汉,618307
2. 北京航空航天大学,北京,100191
基金项目:民航飞行技术与飞行安全科研基地开放基金
摘    要:传感器是导航系统中的重要部件,传感器故障容错性的分散化滤波,对提高系统的可靠性具有重要意义.以SINS/GPS/CNS组成的组合导航系统为研究对象,采用联邦滤波和方差交叉滤波相结合的方法,实现了对传感器故障具有容错性的分散化滤波,对导航系统的精度和容错性进行分析.仿真结果表明,将分散化滤波方法用于多个传感器组成的组合导航系统,不但具有精度高的特点,而且由于具有信息的冗余,整个系统具有较好的容错能力,可以提供更加完善、精确地反映运载体运动的导航信息.

关 键 词:组合导航系统  传感器  故障诊断

The Fault Diagnosis Method of Integrated Navigation System Based on SINS/GPS/CNS
Liu Changhua,Fu Qiang,Song Hua.The Fault Diagnosis Method of Integrated Navigation System Based on SINS/GPS/CNS[J].Journal of China Civil Aviation Flying College,2011,22(1):23-27.
Authors:Liu Changhua  Fu Qiang  Song Hua
Institution:Liu Changhua1 Fu Qiang1 Song Hua2 (1 Civil Aviation Flight University of China Guanghan 618307 Sichuan China) (2 Beijing University of Aeronautics and Astronautics Beijing 100191 China)
Abstract:Sensors are important parts of the navigation system. The decentralized filtering for sensor fault tolerance has great significance for improving system reliability. Based on SINS/GPS/CNS,the method combining federated filtering and covariance intersection filtering is adopted to achieve the decentralized filtering of sensor fault tolerance,and the navigation accuracy and tolerance are analyzed. The simulation results indicate that the implementation of decentralized filtering on integrated navigation syste...
Keywords:Integrated navigation system Sensor Fault diagnosis  
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