{"title":"三自由度直升机全局非齐次准连续控制器","authors":"H. Ríos, A. Rosales, A. Dávila","doi":"10.1109/VSS.2010.5544716","DOIUrl":null,"url":null,"abstract":"This paper presents a practical design approach to the stabilization of a three degrees of freedom helicopter. In this paper the global non homogeneous Quasi-continuous controller is presented in order to preserve high position regulation accuracy and robustness to model uncertainties and external disturbances. The non-homogeneous differentiator is also implemented to obtain exact differentiation in the control strategy. Simulations and the obtained results on a 3DOF helicopter by Quanser are shown.","PeriodicalId":407705,"journal":{"name":"2010 11th International Workshop on Variable Structure Systems (VSS)","volume":"182 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2010-06-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"10","resultStr":"{\"title\":\"Global non-homogeneous Quasi-continuous controller for a 3-DOF helicopter\",\"authors\":\"H. Ríos, A. Rosales, A. Dávila\",\"doi\":\"10.1109/VSS.2010.5544716\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper presents a practical design approach to the stabilization of a three degrees of freedom helicopter. In this paper the global non homogeneous Quasi-continuous controller is presented in order to preserve high position regulation accuracy and robustness to model uncertainties and external disturbances. The non-homogeneous differentiator is also implemented to obtain exact differentiation in the control strategy. Simulations and the obtained results on a 3DOF helicopter by Quanser are shown.\",\"PeriodicalId\":407705,\"journal\":{\"name\":\"2010 11th International Workshop on Variable Structure Systems (VSS)\",\"volume\":\"182 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2010-06-26\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"10\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2010 11th International Workshop on Variable Structure Systems (VSS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/VSS.2010.5544716\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2010 11th International Workshop on Variable Structure Systems (VSS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/VSS.2010.5544716","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Global non-homogeneous Quasi-continuous controller for a 3-DOF helicopter
This paper presents a practical design approach to the stabilization of a three degrees of freedom helicopter. In this paper the global non homogeneous Quasi-continuous controller is presented in order to preserve high position regulation accuracy and robustness to model uncertainties and external disturbances. The non-homogeneous differentiator is also implemented to obtain exact differentiation in the control strategy. Simulations and the obtained results on a 3DOF helicopter by Quanser are shown.