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A New Anomaly Detection Method Based on Multi-dimensional Condition Monitoring Data for Aircraft Engine

机译:一种新的基于飞机发动机多维状态监测数据的异常检测方法

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Identifying the degradation state of aircraft engine accurately and carrying out suitable maintenance is significant for the safe and reliable operation of the aircraft system. In this paper, an anomaly detection system is proposed for multi-dimensional time series for aircraft engine. To represent the degradation degree of the device, the degradation index is proposed utilizing the Dynamic Time Warping algorithm (DTW) which possesses good similarity measure quality and can capture the changing characteristics of the indicator well. On the basis of the degradation index, three decision-making strategies including the Cumulative Sum algorithm (CUSUM), the Youden Index, and the Impact Factor are applied to determine the threshold values. For the threshold, two detection time points are obtained to discriminate different degradation stages in the device, in which the former refers to the initiation of degradation and the latter time point indicates that the device suffers from the anomaly. The experimental results demonstrate that all three decision strategies are able to detect system performance effectively before the device fails, which facilitates the incipient fault warning of aircraft engine in order to keep the equipment safe and reliable.
机译:精确地识别飞机发动机的降解状态,开展合适的维护对于飞机系统的安全可靠运行非常重要。本文提出了一种异常检测系统,用于飞机发动机的多维时间序列。为了表示设备的劣化程度,利用具有良好相似度测量质量的动态时间翘曲算法(DTW)来提出降级指数,并且可以捕获指示器的变化特性。在降级指数的基础上,应用了三种决策策略,包括累积和算法(CUSUM),YENEN指数和影响因子来确定阈值。对于阈值,获得两个检测时间点以区分装置中的不同劣化阶段,其中前者是指降解的启动,后一时间点表明该装置遭受异常的影响。实验结果表明,在设备故障之前,所有三种决策策略都能够有效地检测系统性能,这促进了飞机发动机的初始故障警告,以保持设备安全可靠。

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