Dynamic SLAM diagnosis method for uncontrolled fault of aircraft electronic anti slip braking system

Abstract In order to accurately diagnose the out-of-control fault of an aircraft’s electronic anti-skid braking system, a dynamic SLAM diagnosis method for the out-of-control fault of an aircraft electronic anti-skid braking system is proposed. Using an optical module, image acquisition module, power module, main control module, etc., the dynamic drawing image of aircraft taxiing is acquired. By establishing a dynamic map of aircraft taxiing, the dynamic semantic mapping results are obtained. The out-of-control fault diagnosis model of the depth residual network is constructed, and the aircraft taxiing semantic data is used as input data to output the out-of-control fault diagnosis results. The experimental results show that with the increase of Gaussian white noise intensity, the deviation factor of out-of-control fault diagnosis in the design method increases less, and the sample label misjudges less in the noise-free environment.

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Publication Details

Journal
Journal of Physics Conference Series
Published
2024-08-01
DOI
https://doi.org/10.1088/1742-6596/2820/1/012105
Primary Topic
Industrial Technology and Control Systems
Type
article
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article

Dynamic SLAM diagnosis method for uncontrolled fault of aircraft electronic anti slip braking system

Wenqian Ma, Haiguo Ma
Journal of Physics Conference Series
Industrial Technology and Control Systems
article

Dynamic SLAM diagnosis method for uncontrolled fault of aircraft electronic anti slip braking system

Wenqian Ma, Haiguo Ma
article en

Abstract

Abstract In order to accurately diagnose the out-of-control fault of an aircraft’s electronic anti-skid braking system, a dynamic SLAM diagnosis method for the out-of-control fault of an aircraft electronic anti-skid braking system is proposed. Using an optical module, image acquisition module, power module, main control module, etc., the dynamic drawing image of aircraft taxiing is acquired. By establishing a dynamic map of aircraft taxiing, the dynamic semantic mapping results are obtained. The out-of-control fault diagnosis model of the depth residual network is constructed, and the aircraft taxiing semantic data is used as input data to output the out-of-control fault diagnosis results. The experimental results show that with the increase of Gaussian white noise intensity, the deviation factor of out-of-control fault diagnosis in the design method increases less, and the sample label misjudges less in the noise-free environment.

Journal of Physics Conference SeriesVol. 2820(1)
Civil Aviation Technology College (IR)
Openalex Percentile: Top 86%
Industrial Technology and Control Systems
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