{"title":"基于模糊控制器的飞机滑行横向控制研究","authors":"Yang Li, Z. Jiao, Yaoxing Shang","doi":"10.1109/FPM.2011.6045830","DOIUrl":null,"url":null,"abstract":"Aircraft anti-skid braking system is modeled, and the traditional anti-skid braking control algorithm is analyzed. A lateral fuzzy controller is designed, based on the original structure of the controller, whose key variable is the reference velocity, Two more inputs of aircraft drift angel and its derivation are introduced to compensate the reference velocities of two wheel braking control loops respectively. The simulation results demonstrate the performance of the lateral fuzzy controller on this principle.","PeriodicalId":241423,"journal":{"name":"Proceedings of 2011 International Conference on Fluid Power and Mechatronics","volume":"28 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2011-10-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"3","resultStr":"{\"title\":\"Research on aircraft taxiing lateral control based on fuzzy controller\",\"authors\":\"Yang Li, Z. Jiao, Yaoxing Shang\",\"doi\":\"10.1109/FPM.2011.6045830\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Aircraft anti-skid braking system is modeled, and the traditional anti-skid braking control algorithm is analyzed. A lateral fuzzy controller is designed, based on the original structure of the controller, whose key variable is the reference velocity, Two more inputs of aircraft drift angel and its derivation are introduced to compensate the reference velocities of two wheel braking control loops respectively. The simulation results demonstrate the performance of the lateral fuzzy controller on this principle.\",\"PeriodicalId\":241423,\"journal\":{\"name\":\"Proceedings of 2011 International Conference on Fluid Power and Mechatronics\",\"volume\":\"28 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2011-10-17\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"3\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of 2011 International Conference on Fluid Power and Mechatronics\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/FPM.2011.6045830\",\"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 of 2011 International Conference on Fluid Power and Mechatronics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/FPM.2011.6045830","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Research on aircraft taxiing lateral control based on fuzzy controller
Aircraft anti-skid braking system is modeled, and the traditional anti-skid braking control algorithm is analyzed. A lateral fuzzy controller is designed, based on the original structure of the controller, whose key variable is the reference velocity, Two more inputs of aircraft drift angel and its derivation are introduced to compensate the reference velocities of two wheel braking control loops respectively. The simulation results demonstrate the performance of the lateral fuzzy controller on this principle.
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