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Aircraft Control Surface Fault Stepwise Diagnosis Method Based on Deep Learning

  • Beihang University
  • China Special Vehicle Research Institute

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

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.

源语言英语
主期刊名Advances in Guidance, Navigation and Control - Proceedings of 2024 International Conference on Guidance, Navigation and Control Volume 3
编辑Liang Yan, Haibin Duan, Yimin Deng
出版商Springer Science and Business Media Deutschland GmbH
81-90
页数10
ISBN(印刷版)9789819622078
DOI
出版状态已出版 - 2025
活动International Conference on Guidance, Navigation and Control, ICGNC 2024 - Changsha, 中国
期限: 9 8月 202411 8月 2024

出版系列

姓名Lecture Notes in Electrical Engineering
1339 LNEE
ISSN(印刷版)1876-1100
ISSN(电子版)1876-1119

会议

会议International Conference on Guidance, Navigation and Control, ICGNC 2024
国家/地区中国
Changsha
时期9/08/2411/08/24

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