Adolfo Perrusquía, Carlos Tovar, A. Soria, Juan Carlos Martínez
{"title":"基于数据飞行参数的飞机滚转控制系统鲁棒控制器","authors":"Adolfo Perrusquía, Carlos Tovar, A. Soria, Juan Carlos Martínez","doi":"10.1109/ICEEE.2016.7751210","DOIUrl":null,"url":null,"abstract":"In this paper we present the design of an autopilot for roll angle displacement of an aircraft to a desired orientation using real flight data. Matlab Robust Control Toolbox is used for the synthesis of the stabilizing K controller. The model plant is partitioned in terms of the number of perturbations, the number of control inputs, the number of errors, and the number of outputs. Experimental results are presented for a Radio Controller Radlian Pro model aircraft.","PeriodicalId":285464,"journal":{"name":"2016 13th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)","volume":"25 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2016-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"6","resultStr":"{\"title\":\"Robust controller for aircraft roll control system using data flight parameters\",\"authors\":\"Adolfo Perrusquía, Carlos Tovar, A. Soria, Juan Carlos Martínez\",\"doi\":\"10.1109/ICEEE.2016.7751210\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this paper we present the design of an autopilot for roll angle displacement of an aircraft to a desired orientation using real flight data. Matlab Robust Control Toolbox is used for the synthesis of the stabilizing K controller. The model plant is partitioned in terms of the number of perturbations, the number of control inputs, the number of errors, and the number of outputs. Experimental results are presented for a Radio Controller Radlian Pro model aircraft.\",\"PeriodicalId\":285464,\"journal\":{\"name\":\"2016 13th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)\",\"volume\":\"25 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2016-09-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"6\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2016 13th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICEEE.2016.7751210\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2016 13th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICEEE.2016.7751210","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Robust controller for aircraft roll control system using data flight parameters
In this paper we present the design of an autopilot for roll angle displacement of an aircraft to a desired orientation using real flight data. Matlab Robust Control Toolbox is used for the synthesis of the stabilizing K controller. The model plant is partitioned in terms of the number of perturbations, the number of control inputs, the number of errors, and the number of outputs. Experimental results are presented for a Radio Controller Radlian Pro model aircraft.