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基于故障状态检测的惯性/卫星信息融合技术
引用本文:方凌,赖际舟,张小山,郑智明.基于故障状态检测的惯性/卫星信息融合技术[J].江苏大学学报(自然科学版),2011,32(1):94-98.
作者姓名:方凌  赖际舟  张小山  郑智明
作者单位:南京航空航天大学,导航研究中心,江苏,南京,210016
基金项目:航空科学基金资助项目(20080852011)
摘    要:为了提高惯性/卫星组合导航系统的可靠性及导航信息的精度,设计了SINS/GPS/Galileo/RDSS组合导航多信息融合方案,采用基于概率分布的残差χ2故障检测方法提高组合导航系统的容错性和可靠性.在此基础上采用了基于故障状态检测的新型自适应信息分配算法,并建立导航系统的数学模型,给出其状态方程、测量方程.最后将新算...

关 键 词:飞机导航  卫星导航  数据融合  卡尔曼滤波  数字仿真

Information fusion technology of INS/GNSS based on fault state detection
Fang Ling,Lai Jizhou,Zhang Xiaoshan,Zhang Zhiming.Information fusion technology of INS/GNSS based on fault state detection[J].Journal of Jiangsu University:Natural Science Edition,2011,32(1):94-98.
Authors:Fang Ling  Lai Jizhou  Zhang Xiaoshan  Zhang Zhiming
Institution:Fang Ling,Lai Jizhou,Zhang Xiaoshan,Zheng Zhiming(Navigation Research Center,Nanjing University of Aeronautics and Astronautics,Nanjing,Jiangsu 210016,China)
Abstract:To improve the reliability and accuracy of INS/GNSS integrated navigation system,an information fusion scheme of SINS/GPS/Galileo/RDSS integrated navigation system was designed,and the chi-square testing method based on probability distribution was adopted to improve the fault tolerance and the reliability of the system.On this condition,a new self-adaption distribution algorithm based on the fault state detection was adopted,and the model of navigation system was established.The states function and measure...
Keywords:aircraft navigation  satellite navigation  data fusion  Kalman filters  digital simulation  
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