Robust Control of 2-DoF Helicopter System in Presence of Unmatched Disturbances & Actuator Faults

Keyur Rathod, Mija S.J.
{"title":"Robust Control of 2-DoF Helicopter System in Presence of Unmatched Disturbances & Actuator Faults","authors":"Keyur Rathod, Mija S.J.","doi":"10.1109/CONIT55038.2022.9848199","DOIUrl":null,"url":null,"abstract":"This paper focuses on the design of robust controllers for the stabilization of CE 150 Humusoft 2-DoF Helicopter system which represents a highly nonlinear & cross coupled system usually subject to external disturbances and parametric uncertainties. A two loop control architecture is used where the inner loop ensures stabilization, error minimization and robustness to parametric uncertainties, matched & unmatched disturbances and the outer loop ensures optimal trajectory tracking without violating actuator saturation bounds. Further, to show the performance of the proposed control scheme, simulation results are presented.","PeriodicalId":270445,"journal":{"name":"2022 2nd International Conference on Intelligent Technologies (CONIT)","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"2022-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2022 2nd International Conference on Intelligent Technologies (CONIT)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CONIT55038.2022.9848199","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1

Abstract

This paper focuses on the design of robust controllers for the stabilization of CE 150 Humusoft 2-DoF Helicopter system which represents a highly nonlinear & cross coupled system usually subject to external disturbances and parametric uncertainties. A two loop control architecture is used where the inner loop ensures stabilization, error minimization and robustness to parametric uncertainties, matched & unmatched disturbances and the outer loop ensures optimal trajectory tracking without violating actuator saturation bounds. Further, to show the performance of the proposed control scheme, simulation results are presented.
存在非匹配扰动和执行器故障的二自由度直升机系统鲁棒控制
ce150直升机系统是一个高度非线性交叉耦合系统,经常受到外界干扰和参数不确定性的影响,本文研究了该系统的鲁棒控制器设计。采用两环控制体系结构,其中内环确保稳定,误差最小化和对参数不确定性,匹配和不匹配干扰的鲁棒性,外环确保在不违反执行器饱和边界的情况下进行最佳轨迹跟踪。为了验证所提控制方案的有效性,给出了仿真结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
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:481959085
Book学术官方微信