{"title":"四旋翼飞行器颤振自由滑动自适应姿态控制","authors":"Zhi Li, Xin Ma, Zhigang Xu, Yafang Wang, Yibin Li","doi":"10.1109/CGNCC.2016.7828872","DOIUrl":null,"url":null,"abstract":"This paper investigates the quadrotor attitude tracking control problem in the presence of external disturbance and inertia uncertainty. An error quaternion based adaptive sliding mode control scheme is proposed in this paper. Adaptive control theory is applied to estimate inertia parameters and the upper bound of external disturbance. Lyapunov stability theory is applied to prove the stability of the controller. Simulation results are presented to demonstrate the performance and robustness of the controller.","PeriodicalId":426650,"journal":{"name":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","volume":"22 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2016-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"4","resultStr":"{\"title\":\"Chattering free sliding adaptive attitude control for quadrotor\",\"authors\":\"Zhi Li, Xin Ma, Zhigang Xu, Yafang Wang, Yibin Li\",\"doi\":\"10.1109/CGNCC.2016.7828872\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper investigates the quadrotor attitude tracking control problem in the presence of external disturbance and inertia uncertainty. An error quaternion based adaptive sliding mode control scheme is proposed in this paper. Adaptive control theory is applied to estimate inertia parameters and the upper bound of external disturbance. Lyapunov stability theory is applied to prove the stability of the controller. Simulation results are presented to demonstrate the performance and robustness of the controller.\",\"PeriodicalId\":426650,\"journal\":{\"name\":\"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)\",\"volume\":\"22 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2016-08-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"4\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/CGNCC.2016.7828872\",\"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 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CGNCC.2016.7828872","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Chattering free sliding adaptive attitude control for quadrotor
This paper investigates the quadrotor attitude tracking control problem in the presence of external disturbance and inertia uncertainty. An error quaternion based adaptive sliding mode control scheme is proposed in this paper. Adaptive control theory is applied to estimate inertia parameters and the upper bound of external disturbance. Lyapunov stability theory is applied to prove the stability of the controller. Simulation results are presented to demonstrate the performance and robustness of the controller.