A sensor fault detection for aircraft using a single Kalman filter and hidden Markov models

K. Rudin, G. Ducard, R. Siegwart
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引用次数: 14

Abstract

This paper presents a new scheme for sensor fault detection and isolation. It uses a single Kalman filter and a Gaussian hidden Markov model for each of the monitored sensors. This combination is able to simultaneously detect single and multiple sensor faults, still guaranteeing optimal system state estimation. This algorithm also can run on systems with limited computational power. The efficiency of the approach is evaluated through simulation of an aircraft to detect airspeed and GPS sensor faults. The results show fast fault detection and low false-alarm rate.
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基于单卡尔曼滤波和隐马尔可夫模型的飞机传感器故障检测
本文提出了一种新的传感器故障检测与隔离方案。它使用一个卡尔曼滤波器和一个高斯隐马尔可夫模型对每个被监测的传感器。这种组合能够同时检测单个和多个传感器故障,仍然保证最优的系统状态估计。该算法也可以在计算能力有限的系统上运行。通过飞机航速和GPS传感器故障检测的仿真,验证了该方法的有效性。结果表明,该方法故障检测速度快,误报率低。
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