{"title":"Design of a fuzzy variable structure controller for controlling satellite attitude suffering from sensor data delay","authors":"B. Erkal, O. Kaynak","doi":"10.1109/RAST.2011.5966900","DOIUrl":null,"url":null,"abstract":"Time delays in sensor data is one of the main issues in controlling the attitude of a satellite. Although, there exists methods to alleviate the problem, it is preferable to have a robust controller which can handle delays in sensor data well. In this study, a new method is proposed in the literature which uses an enhanced fuzzy variable structure controller that can handle delays in sensor data well. However it displays a steady state error. The novelty in this study is that the steady state error is handled using an integral term so that an acceptable performance is obtained.","PeriodicalId":285002,"journal":{"name":"Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011","volume":"12 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2011-06-09","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"6","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/RAST.2011.5966900","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 6
Abstract
Time delays in sensor data is one of the main issues in controlling the attitude of a satellite. Although, there exists methods to alleviate the problem, it is preferable to have a robust controller which can handle delays in sensor data well. In this study, a new method is proposed in the literature which uses an enhanced fuzzy variable structure controller that can handle delays in sensor data well. However it displays a steady state error. The novelty in this study is that the steady state error is handled using an integral term so that an acceptable performance is obtained.