{"title":"Attitude control of a satellite using sliding mode","authors":"M. Benenia, M. Benslama","doi":"10.1109/ICEMIS.2017.8273046","DOIUrl":null,"url":null,"abstract":"This paper is dedicated to the problem of a satellite attitude control. The control method is based upon a robust sliding mode control. A sliding mode controller has been designed in such a way that the state variables of the system converge to the desired values. Where the controller parameters can drive the state to hit the sliding surface. The steps of the control design are presented.","PeriodicalId":117908,"journal":{"name":"2017 International Conference on Engineering & MIS (ICEMIS)","volume":"3 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2017-05-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2017 International Conference on Engineering & MIS (ICEMIS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICEMIS.2017.8273046","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 is dedicated to the problem of a satellite attitude control. The control method is based upon a robust sliding mode control. A sliding mode controller has been designed in such a way that the state variables of the system converge to the desired values. Where the controller parameters can drive the state to hit the sliding surface. The steps of the control design are presented.