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基于重抽样加权的飞行器多源数据融合方法

崔榕峰 王祥云 刘哲 李鸿岩 郭承鹏

航空科学技术2024,Vol.35Issue(7):111-119,9.
航空科学技术2024,Vol.35Issue(7):111-119,9.DOI:10.19452/j.issn1007-5453.2024.07.012

基于重抽样加权的飞行器多源数据融合方法

Multi-Fidelity Data Fusion Method for Aircraft based on Resampling and Weighting

崔榕峰 1王祥云 1刘哲 1李鸿岩 1郭承鹏1

作者信息

  • 1. 中国航空工业空气动力研究院 高速高雷诺数气动力航空科技重点实验室 辽宁 沈阳 110034
  • 折叠

摘要

Abstract

The wind tunnel test method and CFD simulation method can provide accurate analysis for the aerodynamic performance in the initial development stage of the aircraft,which plays an important role in the optimization of the aerodynamic shape of the aircraft.However,wind tunnel tests and CFD methods inevitably have the problem of high costs.In order to achieve low cost and efficient analysis on aircraft aerodynamic performance,this paper uses machine learning methods to analyze wind tunnel test data and aims to obtain the relationship between the CFD data with lower accuracy and the wind tunnel test data with higher accuracy through repeated sampling and combine the multiple relationship through the weighted method based on mean square error to obtain the final prediction.The results show that the data fusion mode based on repeated sampling and weighting method can effectively improve the accuracy and goodness of fit of wind tunnel test data prediction.The results demonstrate that the data fusion model based on resampling and weighting can effectively enhance the precision and reliability of wind tunnel test data prediction and assist wind tunnel test personnel to handle relevant research work.

关键词

数据融合/重抽样加权法/风洞试验/CFD/机器学习

Key words

data fusion/repeated sampling and weighting method/wind tunnel test/CFD/machine learning

分类

航空航天

引用本文复制引用

崔榕峰,王祥云,刘哲,李鸿岩,郭承鹏..基于重抽样加权的飞行器多源数据融合方法[J].航空科学技术,2024,35(7):111-119,9.

基金项目

航空科学基金(2022Z006026004,2023M071027001) Aeronautical Science Foundation of China(2022Z006026004,2023M071027001) (2022Z006026004,2023M071027001)

航空科学技术

1007-5453

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