Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University  Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University
Research on Sinusoidal Load Identification Method under Structural Natural Frequency Excitation Based on LSTM-CNN
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Civil Aviation University of China

Clc Number:

v215.1

Fund Project:

1.Tianjin Aviation Equipment Safety and Airworthiness Technology Innovation Center Open Fund2.Open Fund of the Key Laboratory of Civil Aviation Aircraft Airworthiness Certification Technology at Civil Aviation University of China

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    Abstract:

    Addressing the challenge of low identification accuracy in traditional load identification methods based on the truncated singular value decomposition (TSVD) method, especially when the external load frequency approaches or reaches the natural frequency of the structure, we propose the LSTM-CNN load identification model. This model combines the feature extraction capabilities of the convolutional neural network (CNN) with the long-term memory function of the long short-term memory network (LSTM). The load identification method based on the LSTM-CNN model is then applied to research load time domain waveform identification on the GARTEUR aircraft model. For model training and load identification, we collect response data and excitation data from the structure. The identification results are compared with the TSVD method, LSTM method, and DCNN method. The findings demonstrate that the load identification method based on the LSTM-CNN model proves effective for sinusoidal load identification problems, especially under the natural frequency excitation of the structure. The method exhibits high identification accuracy and robust noise resistance capabilities.

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he wen bo, sunhanyu, xiejiang, zhangxiaoqiang. Research on Sinusoidal Load Identification Method under Structural Natural Frequency Excitation Based on LSTM-CNN[J]. Advances in Aeronautical Science and Engineering,2024,15(5):48-57

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History
  • Received:September 25,2023
  • Revised:December 13,2023
  • Adopted:February 01,2024
  • Online: September 13,2024
  • Published:
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