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Aircraft Control Surface Fault Stepwise Diagnosis Method Based on Deep Learning

  • Beihang University
  • China Special Vehicle Research Institute

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The fault diagnosis system for aircraft control surface is significant for f light safety. In this paper, an aircraft control surface fault stepwise diagnosis (FSD) method based on deep learning is proposed. The fault type, location and degree are step-by-step diagnosed. The fault feature parameter extraction (FFPE) equations that best reflect specific faults feature are extracted based on flight dynamics analysis, and the input and output of the neural network are determined. The fault rule base is established based on the multiple Long Short Term Memory (LSTM) classification neural network to detect the fault type and location respectively. Then the fault feature parameter equations are simplified and calculated to obtain the fault degree. The results of simulations validate the effectiveness and superiority of the FSD method compared with other methods.

Original languageEnglish
Title of host publicationAdvances in Guidance, Navigation and Control - Proceedings of 2024 International Conference on Guidance, Navigation and Control Volume 3
EditorsLiang Yan, Haibin Duan, Yimin Deng
PublisherSpringer Science and Business Media Deutschland GmbH
Pages81-90
Number of pages10
ISBN (Print)9789819622078
DOIs
StatePublished - 2025
EventInternational Conference on Guidance, Navigation and Control, ICGNC 2024 - Changsha, China
Duration: 9 Aug 202411 Aug 2024

Publication series

NameLecture Notes in Electrical Engineering
Volume1339 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceInternational Conference on Guidance, Navigation and Control, ICGNC 2024
Country/TerritoryChina
CityChangsha
Period9/08/2411/08/24

Keywords

  • Control Surface
  • Fault Feature Parameter Extraction
  • Fault Stepwise Diagnosis
  • LSTM

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