{"title":"基于反馈线性化的直升机简化模型位置控制","authors":"S. Rebeschiess, M. Roloff","doi":"10.1109/CCA.1999.806165","DOIUrl":null,"url":null,"abstract":"In this paper we describe a method for angular pitch control with feedback linearization for a laboratory helicopter model. Linear angular control can only be applied in a small angle interval. Better control can be obtained by using a linearizing transformation. This transformation tends to be very complex. For the application in this paper it can be shown that a simplified transformation can be sufficient for achieving good control results.","PeriodicalId":325193,"journal":{"name":"Proceedings of the 1999 IEEE International Conference on Control Applications (Cat. No.99CH36328)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1999-08-22","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"3","resultStr":"{\"title\":\"Position control by feedback linearization for a simplified helicopter model\",\"authors\":\"S. Rebeschiess, M. Roloff\",\"doi\":\"10.1109/CCA.1999.806165\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this paper we describe a method for angular pitch control with feedback linearization for a laboratory helicopter model. Linear angular control can only be applied in a small angle interval. Better control can be obtained by using a linearizing transformation. This transformation tends to be very complex. For the application in this paper it can be shown that a simplified transformation can be sufficient for achieving good control results.\",\"PeriodicalId\":325193,\"journal\":{\"name\":\"Proceedings of the 1999 IEEE International Conference on Control Applications (Cat. No.99CH36328)\",\"volume\":\"1 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1999-08-22\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"3\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of the 1999 IEEE International Conference on Control Applications (Cat. No.99CH36328)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/CCA.1999.806165\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of the 1999 IEEE International Conference on Control Applications (Cat. No.99CH36328)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CCA.1999.806165","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Position control by feedback linearization for a simplified helicopter model
In this paper we describe a method for angular pitch control with feedback linearization for a laboratory helicopter model. Linear angular control can only be applied in a small angle interval. Better control can be obtained by using a linearizing transformation. This transformation tends to be very complex. For the application in this paper it can be shown that a simplified transformation can be sufficient for achieving good control results.
京公网安备 11010802042870号
京ICP备2023020795号-1
分享
求助内容：
应助结果提醒方式：
扫码关注我们
