{"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":"21 1","pages":"0"},"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.