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Fault Diagnosis in Dynamic Systems Via Kalman Filter Innovation Sequence

机译:通过卡尔曼滤波创新序列动态系统的故障诊断

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In this paper, a real-time approach to detect and isolate the faults affecting the mean, and the covariance matrix of the Kalman filter innovation sequence, is presented. As monitoring statistics, the ratio of two quadratic forms of which matrices are theoretic and selected covariance matrices is used. A theorem is given to show that the arguments of the optimal quadratic form maximize the above statistics, and thus they are determined to detect and isolate faults in the sensors rapidly. Thelongitudinal dynamics of an aircraft control system, as an example, is considered, and detection and isolation of pitch rate gyro faults affecting the mean and covariance matrix is addressed. A fault isolation technique based on the partition ofs-dimensional innovation sequence into s one-dimensional innovation sequences, is presented, and the structure of a fault tolerant system is given.
机译:本文介绍了检测和隔离影响平均值的故障的实时方法,以及卡尔曼滤波创新序列的协方差矩阵。作为监视统计,使用哪种矩阵的二次形式的比率是使用理论和选择的协方差矩阵。给出定理表明,最佳二次形式的参数最大化上述统计数据,因此确定它们快速地检测和隔离传感器中的故障。作为示例,考虑了飞机控制系统的重点动力学,并解决了影响均值和协方差矩阵的俯仰速率陀螺故障的检测和隔离。提出了一种基于划分的划分的分区的故障隔离技术,给出了一维创新序列的局限性创新序列,给出了容错系统的结构。

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