Flutter boundary prediction method based on HHT and machine learning

被引:0
|
作者
Hong, Zhongxin [1 ]
Zhou, Li [1 ]
Chen, Mingfeng [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Nanjing 210016, Peoples R China
基金
中国国家自然科学基金;
关键词
Flutter boundary prediction; Machine learning; Feature extraction; Flutter pattern recognition; Flutter degree analysis;
D O I
10.1117/12.2657935
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A flutter boundary prediction method based on HHT and machine learning is proposed to predict the flutter velocity before the wind speed reaches the subcritical state. Natural excitation technique is used to extract impulse response signals. EMD ( empirical Mode decomposition method) is used to decompose the signal. Hilbert spectrum was obtained and analyzed by HHT to decompose the signal. The analysis methods included HHT spectrum and marginal spectrum analysis, so as to extract the characteristic quantity and establish the classification model according to different flight states. Then, regression models were established under different flutter modes for flutter degree analysis. During the prediction, according to the classification performance of the data to be measured, the flutter degree analysis result is weighted to obtain the flutter degree corresponding to the current wind speed, and then the flutter wind speed is calculated. In the selection of machine learning algorithm, naive Bayes algorithm, K-nearest neighbor algorithm and other machine learning algorithms are used to construct the classification model, linear regression,, Gaussian process regression and so on are used to construct the regression model. The results show that the K-nearest neighbor algorithm performs best in the classification algorithm, while the Gaussian process regression algorithm performs best in the regression algorithm. Through the cross-validation of the test data, the proposed method can accurately predict the critical flutter velocity when it is far away from the flutter boundary through flutter mode recognition and flutter degree analysis.
引用
收藏
页数:10
相关论文
共 50 条
  • [1] Composite Fins Subsonic Flutter Prediction Based on Machine Learning
    Dinulovic, Mirko
    Benign, Aleksandar
    Rasuo, Bosko
    AEROSPACE, 2024, 11 (01)
  • [2] Flutter boundary prediction method based on VMD decomposition using prediction signal
    Wu, Tongxi
    Zhou, Li
    NONDESTRUCTIVE CHARACTERIZATION AND MONITORING OF ADVANCED MATERIALS, AEROSPACE, CIVIL INFRASTRUCTURE, AND TRANSPORTATION XVII, 2023, 12487
  • [3] Prediction of thermal boundary resistance by the machine learning method
    Zhan, Tianzhuo
    Fang, Lei
    Xu, Yibin
    SCIENTIFIC REPORTS, 2017, 7
  • [4] Prediction of thermal boundary resistance by the machine learning method
    Tianzhuo Zhan
    Lei Fang
    Yibin Xu
    Scientific Reports, 7
  • [5] A classification method of flutter test signals based on CNN and HHT
    Xu, Guanghang
    Zhou, Li
    SENSORS AND SMART STRUCTURES TECHNOLOGIES FOR CIVIL, MECHANICAL, AND AEROSPACE SYSTEMS 2024, 2024, 12949
  • [6] Body freedom flutter boundary prediction method for flight flutter test
    Lei, Peng-Xuan
    Lü, Bin-Bin
    Guo, Hong-Tao
    Yu, Li
    Chen, De-Hua
    Zhendong Gongcheng Xuebao/Journal of Vibration Engineering, 2022, 35 (01): : 202 - 208
  • [7] A Stratigraphic Prediction Method Based on Machine Learning
    Zhou, Cuiying
    Ouyang, Jinwu
    Ming, Weihua
    Zhang, Guohao
    Du, Zichun
    Liu, Zhen
    APPLIED SCIENCES-BASEL, 2019, 9 (17):
  • [8] Prediction method of blade flutter boundary in a compressor stage
    Zhang, Xiao-Wei
    Wang, Yan-Rong
    Xu, Ke-Ning
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2011, 26 (02): : 392 - 396
  • [9] A stability criterion method based on neural network and its application on flutter boundary prediction
    Zheng, Hua (zhangjieOO1@mail.nwpu.edu.cn), 1600, CRL Publishing (24): : 3 - 4
  • [10] Flutter boundary prediction based on nonstationary data measurement
    Torii, H
    Matsuzaki, Y
    JOURNAL OF AIRCRAFT, 1997, 34 (03): : 427 - 432