基于混合辅助系统的倾转旋翼机转换模式切换自适应跟踪控制

IF 5.8 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Wen Li, Shuang Shi, Mou Chen, Qingxian Wu
{"title":"基于混合辅助系统的倾转旋翼机转换模式切换自适应跟踪控制","authors":"Wen Li,&nbsp;Shuang Shi,&nbsp;Mou Chen,&nbsp;Qingxian Wu","doi":"10.1016/j.ast.2025.110921","DOIUrl":null,"url":null,"abstract":"<div><div>An adaptive tracking control scheme for the conversion mode of twin tilt-rotor aircraft is proposed under input saturation and fixed-time prescribed performance requirements. First, due to the tilting features, a longitudinal switched nonlinear model is constructed in view of aerodynamic analysis to facilitate controller design. Second, considering the input saturation, the distribution-based multi-auxiliary systems are designed to match the requirements of time-related flexible prescribed performance. Third, a novel adaptive switching controller is designed to reduce the influences caused by modeling uncertainty. Finally, an XV-15-based simulation result verifies the effectiveness of the proposed method.</div></div>","PeriodicalId":50955,"journal":{"name":"Aerospace Science and Technology","volume":"168 ","pages":"Article 110921"},"PeriodicalIF":5.8000,"publicationDate":"2025-09-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Mixed-auxiliary systems based switching adaptive tracking control for conversion mode of tilt-rotor aircraft\",\"authors\":\"Wen Li,&nbsp;Shuang Shi,&nbsp;Mou Chen,&nbsp;Qingxian Wu\",\"doi\":\"10.1016/j.ast.2025.110921\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>An adaptive tracking control scheme for the conversion mode of twin tilt-rotor aircraft is proposed under input saturation and fixed-time prescribed performance requirements. First, due to the tilting features, a longitudinal switched nonlinear model is constructed in view of aerodynamic analysis to facilitate controller design. Second, considering the input saturation, the distribution-based multi-auxiliary systems are designed to match the requirements of time-related flexible prescribed performance. Third, a novel adaptive switching controller is designed to reduce the influences caused by modeling uncertainty. Finally, an XV-15-based simulation result verifies the effectiveness of the proposed method.</div></div>\",\"PeriodicalId\":50955,\"journal\":{\"name\":\"Aerospace Science and Technology\",\"volume\":\"168 \",\"pages\":\"Article 110921\"},\"PeriodicalIF\":5.8000,\"publicationDate\":\"2025-09-26\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Aerospace Science and Technology\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S127096382500985X\",\"RegionNum\":1,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Science and Technology","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S127096382500985X","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

摘要

针对双倾转旋翼飞机在输入饱和和固定时间规定性能要求下的转换模式,提出了一种自适应跟踪控制方案。首先,针对飞机倾斜的特点,从气动分析的角度出发,建立了纵向切换非线性模型,便于控制器设计。其次,考虑输入饱和,设计了基于分布的多辅助系统,以满足与时间相关的柔性规定性能要求。第三,设计了一种新的自适应切换控制器,以减小建模不确定性对系统的影响。最后,基于xv -15的仿真结果验证了该方法的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Mixed-auxiliary systems based switching adaptive tracking control for conversion mode of tilt-rotor aircraft
An adaptive tracking control scheme for the conversion mode of twin tilt-rotor aircraft is proposed under input saturation and fixed-time prescribed performance requirements. First, due to the tilting features, a longitudinal switched nonlinear model is constructed in view of aerodynamic analysis to facilitate controller design. Second, considering the input saturation, the distribution-based multi-auxiliary systems are designed to match the requirements of time-related flexible prescribed performance. Third, a novel adaptive switching controller is designed to reduce the influences caused by modeling uncertainty. Finally, an XV-15-based simulation result verifies the effectiveness of the proposed method.
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
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
×
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
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
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 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信