{"title":"飞行模拟器伺服系统的自适应非奇异快速终端滑模控制","authors":"Chao Cai, Weihong Wang","doi":"10.1109/CGNCC.2016.7828840","DOIUrl":null,"url":null,"abstract":"As for the disadvantageous influence on the flight simulator servo system caused by external disturbance, system uncertainties and model parameters fluctuating, an adaptive nonsingular fast terminal sliding mode controller is designed, and the stability of the system is proved. The fuzzy disturbance observer is used to compensate the disturbance and uncertainties. Combining nonsingular fast terminal sliding mode control with fuzzy disturbance observer, the proposed controller also has the advantage of small tracking error and good dynamic performance. Experiment results on flight simulator are presented to demonstrate the effectiveness of the proposed algorithm. The results show that compared with fast terminal sliding mode control, the proposed control algorithm has better tracking accuracy with fast respond speed, and good low-speed and high frequency characteristics in a proper frequency range.","PeriodicalId":426650,"journal":{"name":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","volume":"64 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2016-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Adaptive nonsingular fast terminal sliding mode control for flight simulator servo system\",\"authors\":\"Chao Cai, Weihong Wang\",\"doi\":\"10.1109/CGNCC.2016.7828840\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"As for the disadvantageous influence on the flight simulator servo system caused by external disturbance, system uncertainties and model parameters fluctuating, an adaptive nonsingular fast terminal sliding mode controller is designed, and the stability of the system is proved. The fuzzy disturbance observer is used to compensate the disturbance and uncertainties. Combining nonsingular fast terminal sliding mode control with fuzzy disturbance observer, the proposed controller also has the advantage of small tracking error and good dynamic performance. Experiment results on flight simulator are presented to demonstrate the effectiveness of the proposed algorithm. The results show that compared with fast terminal sliding mode control, the proposed control algorithm has better tracking accuracy with fast respond speed, and good low-speed and high frequency characteristics in a proper frequency range.\",\"PeriodicalId\":426650,\"journal\":{\"name\":\"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)\",\"volume\":\"64 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2016-08-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"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.2016.7828840\",\"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.2016.7828840","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Adaptive nonsingular fast terminal sliding mode control for flight simulator servo system
As for the disadvantageous influence on the flight simulator servo system caused by external disturbance, system uncertainties and model parameters fluctuating, an adaptive nonsingular fast terminal sliding mode controller is designed, and the stability of the system is proved. The fuzzy disturbance observer is used to compensate the disturbance and uncertainties. Combining nonsingular fast terminal sliding mode control with fuzzy disturbance observer, the proposed controller also has the advantage of small tracking error and good dynamic performance. Experiment results on flight simulator are presented to demonstrate the effectiveness of the proposed algorithm. The results show that compared with fast terminal sliding mode control, the proposed control algorithm has better tracking accuracy with fast respond speed, and good low-speed and high frequency characteristics in a proper frequency range.