具有非线性扰动的非最小相位系统的输出反馈滑模控制

Xing-gang Yan, Christopher Edwards *, S. Spurgeon
{"title":"具有非线性扰动的非最小相位系统的输出反馈滑模控制","authors":"Xing-gang Yan, Christopher Edwards *, S. Spurgeon","doi":"10.1080/00207170412331317440","DOIUrl":null,"url":null,"abstract":"In this paper, robust stabilization for a class of systems with a nonlinear disturbance is considered. The nonlinear disturbance is mismatched with a nonlinear bound and the nominal system is allowed to be nonminimum phase. A dynamical compensator is designed to estimate the system state and a sliding surface, in the augmented space formed by the system output and the estimated state, is proposed. The stability of the corresponding sliding mode is analysed using the equivalent control approach. Based on the estimated state variables and system output, a variable structure control scheme is developed such that the system is driven to the sliding surface and maintained on it thereafter. Finally, a simulation study of a nonminimum phase HIRM aircraft model is presented to illustrate the effectiveness of the results.","PeriodicalId":169932,"journal":{"name":"2004 5th Asian Control Conference (IEEE Cat. No.04EX904)","volume":"9 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2004-07-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"58","resultStr":"{\"title\":\"Output feedback sliding mode control for nonminimum phase systems with nonlinear disturbances\",\"authors\":\"Xing-gang Yan, Christopher Edwards *, S. Spurgeon\",\"doi\":\"10.1080/00207170412331317440\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this paper, robust stabilization for a class of systems with a nonlinear disturbance is considered. The nonlinear disturbance is mismatched with a nonlinear bound and the nominal system is allowed to be nonminimum phase. A dynamical compensator is designed to estimate the system state and a sliding surface, in the augmented space formed by the system output and the estimated state, is proposed. The stability of the corresponding sliding mode is analysed using the equivalent control approach. Based on the estimated state variables and system output, a variable structure control scheme is developed such that the system is driven to the sliding surface and maintained on it thereafter. Finally, a simulation study of a nonminimum phase HIRM aircraft model is presented to illustrate the effectiveness of the results.\",\"PeriodicalId\":169932,\"journal\":{\"name\":\"2004 5th Asian Control Conference (IEEE Cat. No.04EX904)\",\"volume\":\"9 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2004-07-20\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"58\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2004 5th Asian Control Conference (IEEE Cat. No.04EX904)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1080/00207170412331317440\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2004 5th Asian Control Conference (IEEE Cat. No.04EX904)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1080/00207170412331317440","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 58

摘要

研究一类具有非线性扰动的系统的鲁棒镇定问题。非线性扰动与非线性界失匹配,允许系统为非最小相位。设计了一个动态补偿器来估计系统状态,并在系统输出和估计状态形成的增广空间中提出了一个滑动面。采用等效控制方法分析了相应滑模的稳定性。根据估计的状态变量和系统输出,提出了一种将系统驱动到滑模表面并保持在滑模表面的变结构控制方案。最后,以非最小相位HIRM飞机模型为例进行了仿真研究,验证了结果的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Output feedback sliding mode control for nonminimum phase systems with nonlinear disturbances
In this paper, robust stabilization for a class of systems with a nonlinear disturbance is considered. The nonlinear disturbance is mismatched with a nonlinear bound and the nominal system is allowed to be nonminimum phase. A dynamical compensator is designed to estimate the system state and a sliding surface, in the augmented space formed by the system output and the estimated state, is proposed. The stability of the corresponding sliding mode is analysed using the equivalent control approach. Based on the estimated state variables and system output, a variable structure control scheme is developed such that the system is driven to the sliding surface and maintained on it thereafter. Finally, a simulation study of a nonminimum phase HIRM aircraft model is presented to illustrate the effectiveness of the results.
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
×
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