{"title":"一种简化摇摆三角翼模型的控制研究","authors":"C. Chien, C. Cheng, M.D. Chen, M. Lai","doi":"10.1109/AEROCS.1993.720974","DOIUrl":null,"url":null,"abstract":"In this paper, we propose a nonlinear state feedback control law for an approximated delta wing wingrock control experiment model. The stability of the closed loop system is proved and the performance is demonstrated.","PeriodicalId":170527,"journal":{"name":"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,","volume":"519 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1993-05-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"On the Control of a Simplified Rocking Delta Wing Model\",\"authors\":\"C. Chien, C. Cheng, M.D. Chen, M. Lai\",\"doi\":\"10.1109/AEROCS.1993.720974\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this paper, we propose a nonlinear state feedback control law for an approximated delta wing wingrock control experiment model. The stability of the closed loop system is proved and the performance is demonstrated.\",\"PeriodicalId\":170527,\"journal\":{\"name\":\"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,\",\"volume\":\"519 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1993-05-25\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AEROCS.1993.720974\",\"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. The First IEEE Regional Conference on Aerospace Control Systems,","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AEROCS.1993.720974","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
On the Control of a Simplified Rocking Delta Wing Model
In this paper, we propose a nonlinear state feedback control law for an approximated delta wing wingrock control experiment model. The stability of the closed loop system is proved and the performance is demonstrated.