计算机科学
残余物
深度学习
断层(地质)
人工智能
频域
分类器(UML)
时域
模式识别(心理学)
频道(广播)
领域(数学分析)
故障检测与隔离
数据挖掘
实时计算
算法
计算机视觉
执行机构
电信
数学
地质学
数学分析
地震学
作者
Zhen Jia,Yang Li,Shengdong Wang,Zhenbao Liu
标识
DOI:10.1088/1361-6501/aca219
摘要
Abstract The effectiveness and safety of an aircraft’s flight depend heavily on the flight control system. Since the attitude sensor is the weakest link, identifying its failure modes is crucial. To overcome the shortcomings of a single diagnosis model and a single input signal, this paper proposes a hybrid deep fault diagnosis model based on multi-data fusion. First, the normal and fault models of the sensor are established, and the residual timing signals of the sensor in different fault states are obtained. The frequency domain and timefrequency domain representations of the original timing signals are collected by means of fast Fourier transform and S-transform, and they are used as the input of the hybrid deep diagnosis model. The deep model is designed for the three inputs to mine the characteristics of the input data. These three deep features are concatenated and dimensionally reduced to obtain more comprehensive and representative features. Finally, the classifier is used to classify and obtain the diagnosis results. Through experiments, the advantages of the proposed method are verified by comparing it with several other methods.
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