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Kalman Filter Residual-Based Integrity Monitoring Against Measurement Faults

机译:基于卡尔曼滤波器残差的完整性监测,以应对测量故障

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摘要

This paper introduces a new Kalman filter-based method for detecting sensor faults in linear dynamic systems. In contrast with existing sequential fault-detection algorithms, the proposed method enables direct evaluation of the integrity risk, which is the probability that an undetected fault causes state estimate errors to exceed predefined bounds of acceptability. The new method is also computationally efficient and straightforward to implement. The algorithm's detection test statistic is established in three steps. First, the weighted norms of current and past-time Kalman filter residuals are defined as generalized non-centrally chi-square distributed random variables. Second, these residuals are proved to be stochastically independent from the state estimate error. Third, current-time and past-time residuals are shown to be mutually independent, so that the Kalman filter-based test statistic can be recursively updated in real time by simply adding the current-time residual contribution to a previously computed weighted norm of past-time residuals. The Kalman filter-based integrity monitor is evaluated against worst-case fault profiles, which are also derived in this paper. Finally, performance analyses results are presented for an example application of aircraft precision approach navigation, where differential ranging signals from a multi-constellation satellite navigation system are filtered for positioning and carrier phase cycle ambiguity estimation.
机译:本文介绍了一种基于卡尔曼滤波器的新方法,用于检测线性动态系统中的传感器故障。与现有的顺序故障检测算法相比,所提出的方法能够直接评估完整性风险,这是未检测到的故障导致状态估计误差超过可接受范围的可能性。新方法在计算上也很有效,并且易于实现。该算法的检测测试统计量分为三个步骤。首先,将当前和过去的卡尔曼滤波器残差的加权范数定义为广义的非中心卡方分布随机变量。其次,证明了这些残差与状态估计误差是随机无关的。第三,当前时间和过去时间残差被显示为相互独立,因此可以通过简单地将当前时间残差贡献添加到先前计算的过去加权加权范数来实时递归更新基于卡尔曼滤波器的测试统计量。时间残差。基于卡尔曼滤波器的完整性监控器针对最坏情况下的故障情况进行了评估,这也是本文得出的。最后,为飞机精确进近导航的示例应用提供了性能分析结果,其中对来自多星座卫星导航系统的差分测距信号进行了滤波,以进行定位和载波相位周期模糊度估计。

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