基于预训练机器学习模型的高动态超音速飞行器系统飞行参数预测

Dengji Zhou, Dawen Huang, Xing Zhang, Ming Tie, Yulin Wang, Yaoxin Shen
{"title":"基于预训练机器学习模型的高动态超音速飞行器系统飞行参数预测","authors":"Dengji Zhou, Dawen Huang, Xing Zhang, Ming Tie, Yulin Wang, Yaoxin Shen","doi":"10.1177/09544100231209014","DOIUrl":null,"url":null,"abstract":"Given the harsh operating circumstances, hypersonic vehicles operating at high Mach number demand accurate advanced information of the flight and health state. Flight parameter prediction is a crucial foundation for achieving this requirement. This work addressed the trade-off between prediction accuracy and efficiency by proposing a flight parameter prediction model with the model pre-training and online parameter updating. To create training data, a mechanism model is established. Then, we construct and evaluate three distinct prediction models to increase prediction accuracy. Finally, we conducted comparative validation experiments to compare the prediction performance of the three models. The findings demonstrate that the suggested model greatly raises prediction accuracy without raising model complexity, better balancing prediction accuracy and efficiency. The prediction accuracy of the suggested model has increased by 81.9% when compared to the traditional model.","PeriodicalId":506990,"journal":{"name":"Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering","volume":"57 24","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2024-06-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Flight parameter prediction for high-dynamic Hypersonic vehicle system based on pre-training machine learning model\",\"authors\":\"Dengji Zhou, Dawen Huang, Xing Zhang, Ming Tie, Yulin Wang, Yaoxin Shen\",\"doi\":\"10.1177/09544100231209014\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Given the harsh operating circumstances, hypersonic vehicles operating at high Mach number demand accurate advanced information of the flight and health state. Flight parameter prediction is a crucial foundation for achieving this requirement. This work addressed the trade-off between prediction accuracy and efficiency by proposing a flight parameter prediction model with the model pre-training and online parameter updating. To create training data, a mechanism model is established. Then, we construct and evaluate three distinct prediction models to increase prediction accuracy. Finally, we conducted comparative validation experiments to compare the prediction performance of the three models. The findings demonstrate that the suggested model greatly raises prediction accuracy without raising model complexity, better balancing prediction accuracy and efficiency. The prediction accuracy of the suggested model has increased by 81.9% when compared to the traditional model.\",\"PeriodicalId\":506990,\"journal\":{\"name\":\"Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering\",\"volume\":\"57 24\",\"pages\":\"\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2024-06-14\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1177/09544100231209014\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1177/09544100231209014","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

摘要

鉴于恶劣的运行环境,在高马赫数下运行的高超音速飞行器需要准确的飞行和健康状态高级信息。飞行参数预测是实现这一要求的重要基础。这项工作通过提出一种具有模型预训练和在线参数更新功能的飞行参数预测模型,解决了预测精度和效率之间的权衡问题。为了创建训练数据,我们建立了一个机制模型。然后,我们构建并评估了三种不同的预测模型,以提高预测精度。最后,我们进行了对比验证实验,以比较三种模型的预测性能。研究结果表明,建议的模型在不增加模型复杂度的情况下大大提高了预测精度,更好地平衡了预测精度和效率。与传统模型相比,建议模型的预测准确率提高了 81.9%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
Flight parameter prediction for high-dynamic Hypersonic vehicle system based on pre-training machine learning model
Given the harsh operating circumstances, hypersonic vehicles operating at high Mach number demand accurate advanced information of the flight and health state. Flight parameter prediction is a crucial foundation for achieving this requirement. This work addressed the trade-off between prediction accuracy and efficiency by proposing a flight parameter prediction model with the model pre-training and online parameter updating. To create training data, a mechanism model is established. Then, we construct and evaluate three distinct prediction models to increase prediction accuracy. Finally, we conducted comparative validation experiments to compare the prediction performance of the three models. The findings demonstrate that the suggested model greatly raises prediction accuracy without raising model complexity, better balancing prediction accuracy and efficiency. The prediction accuracy of the suggested model has increased by 81.9% when compared to the traditional model.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
Flight parameter prediction for high-dynamic Hypersonic vehicle system based on pre-training machine learning model Numerical two-dimensional optimization of a cylindrical fuselage for bioinspired unmanned aerial vehicle based on non-dominated sorting genetic algorithm-II Dynamics and capability of along orbit debris self-collecting with rotating constant magnets Investigating the unsteady flow mechanism at the lip of a ducted fan in crosswind Control strategy for trading off solar power and control input while rendezvous and docking
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1