| 注册
首页|期刊导航|航空学报|融合数据自适应BPNN的倾转旋翼机回转颤振边界预测

融合数据自适应BPNN的倾转旋翼机回转颤振边界预测

ZHENG Lixiong CHEN Zhe WANG Xin ZHAO Qijun

航空学报2025,Vol.46Issue(z1):1-14,14.
航空学报2025,Vol.46Issue(z1):1-14,14.DOI:10.7527/S1000-6893.2025.32159

融合数据自适应BPNN的倾转旋翼机回转颤振边界预测

Prediction of whirl flutter boundary for tiltrotor aircraft based on BPNN with adaptive data

ZHENG Lixiong 1CHEN Zhe 1WANG Xin 1ZHAO Qijun1

作者信息

  • 1. National Key Laboratory of Helicopter Aeromechanics,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China||Helicopter Research Institute,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
  • 折叠

摘要

Abstract

To address the aeroelastic instability issues of tiltrotor aircraft,a prediction method for whirl flutter boundary of tiltrotor aircraft based on Back-Propagation Neural Network(BPNN)was proposed.Firstly,a multi-modal coupled aeroelastic stability analysis model for tiltrotor aircraft was established based on Hamilton's principle and multi-body dy-namics methods.Secondly,minimal modal damping ratio data under strongly correlated parameters characterizing system stability were generated,and an artificial neural network prediction model was constructed.Finally,an adap-tive data refinement method was proposed to enhance the prediction accuracy of the neural network model.The re-sults show that within the training range,the maximum error between the calculated and predicted values is 3.24%,with an average relative error of 0.031%;outside the training range,the maximum error is 6.51%,and the average relative error is 0.089%.The trained BPNN model exhibits good generalization and high fitting accuracy,enabling effi-cient and high-precision predictions with fewer sample data,both within and outside the training range.The refinement method effectively improves prediction accuracy,particularly excelling in the prediction of the critical point of whirl flut-ter,significantly mitigating the peak-to-peak fluctuation effects.Moreover,BPNN provides new tools and methods for handling large-scale complex data,offering new perspectives for the research and application of aeroelastic dynamics in tiltrotor aircraft.

关键词

BP神经网络/倾转旋翼机/回转颤振/数据自适应/边界预测

Key words

BP neural network/tiltrotor aircraft/whirl flutter/adaptive data/boundary prediction

分类

航空航天

引用本文复制引用

ZHENG Lixiong,CHEN Zhe,WANG Xin,ZHAO Qijun..融合数据自适应BPNN的倾转旋翼机回转颤振边界预测[J].航空学报,2025,46(z1):1-14,14.

基金项目

国家自然科学基金(12032012) (12032012)

江苏省研究生科研与实践创新计划项目(KYCX25_0563) (KYCX25_0563)

江苏高校优势学科建设工程资助项目 National Natural Science Foundation of China(12032012) (12032012)

Postgraduate Research&Practice Innovation Program of Jiangsu Province(KYCX25_0563) (KYCX25_0563)

the Priority Academic Program Development of Jiangsu Higher Education Institutions ()

航空学报

OA北大核心

1000-6893

访问量0
|
下载量0
段落导航相关论文