{"title":"滑模控制:一种控制四旋翼飞行器的方法","authors":"M. Herrera, A. Gómez, W. Chamorro, O. Camacho","doi":"10.1109/APCASE.2015.62","DOIUrl":null,"url":null,"abstract":"This paper describes the synthesis and application of controller based on sliding mode theory to a quad rotor. A PD sliding surface is considered for vertical take-off and landing aircraft, also changes in angles are done, and some disturbances are included. Therefore, the controller can be implemented using a PD controller as the sliding surface, and adding some algebra the complete controller algorithm is presented. The controller is tested by simulations.","PeriodicalId":235698,"journal":{"name":"2015 Asia-Pacific Conference on Computer Aided System Engineering","volume":"38 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2015-07-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"51","resultStr":"{\"title\":\"Sliding Mode Control: An Approach to Control a Quadrotor\",\"authors\":\"M. Herrera, A. Gómez, W. Chamorro, O. Camacho\",\"doi\":\"10.1109/APCASE.2015.62\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper describes the synthesis and application of controller based on sliding mode theory to a quad rotor. A PD sliding surface is considered for vertical take-off and landing aircraft, also changes in angles are done, and some disturbances are included. Therefore, the controller can be implemented using a PD controller as the sliding surface, and adding some algebra the complete controller algorithm is presented. The controller is tested by simulations.\",\"PeriodicalId\":235698,\"journal\":{\"name\":\"2015 Asia-Pacific Conference on Computer Aided System Engineering\",\"volume\":\"38 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2015-07-14\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"51\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2015 Asia-Pacific Conference on Computer Aided System Engineering\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/APCASE.2015.62\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2015 Asia-Pacific Conference on Computer Aided System Engineering","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/APCASE.2015.62","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Sliding Mode Control: An Approach to Control a Quadrotor
This paper describes the synthesis and application of controller based on sliding mode theory to a quad rotor. A PD sliding surface is considered for vertical take-off and landing aircraft, also changes in angles are done, and some disturbances are included. Therefore, the controller can be implemented using a PD controller as the sliding surface, and adding some algebra the complete controller algorithm is presented. The controller is tested by simulations.