{"title":"基于螺旋桨差动推力的全翼太阳能无人机滑行控制","authors":"Ma Zhenyu, Zhuang Xiaoping, Zhou Zhou","doi":"10.1109/GNCC42960.2018.9018983","DOIUrl":null,"url":null,"abstract":"To solve the taxiing control problem under lack of nose wheel steering system and rudder, a control approach which uses differential propeller thrust to control taxiing is proposed, with full-wing solar-powered UAV (FSUAV) as the research model. This study gives the taxiing mathematical model of FSUAV and designs a taxiing controller based on linear active disturbance rejection control method (LADRC). Simulations are conducted to demonstrate the effectiveness and robustness of the designed controller and compare with PID controller.","PeriodicalId":6623,"journal":{"name":"2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC)","volume":"46 1","pages":"1-5"},"PeriodicalIF":0.0000,"publicationDate":"2018-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Taxiing Control of Full-wing Solar-powered UAV by Using Differential Propeller Thrust\",\"authors\":\"Ma Zhenyu, Zhuang Xiaoping, Zhou Zhou\",\"doi\":\"10.1109/GNCC42960.2018.9018983\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"To solve the taxiing control problem under lack of nose wheel steering system and rudder, a control approach which uses differential propeller thrust to control taxiing is proposed, with full-wing solar-powered UAV (FSUAV) as the research model. This study gives the taxiing mathematical model of FSUAV and designs a taxiing controller based on linear active disturbance rejection control method (LADRC). Simulations are conducted to demonstrate the effectiveness and robustness of the designed controller and compare with PID controller.\",\"PeriodicalId\":6623,\"journal\":{\"name\":\"2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC)\",\"volume\":\"46 1\",\"pages\":\"1-5\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2018-08-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/GNCC42960.2018.9018983\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/GNCC42960.2018.9018983","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Taxiing Control of Full-wing Solar-powered UAV by Using Differential Propeller Thrust
To solve the taxiing control problem under lack of nose wheel steering system and rudder, a control approach which uses differential propeller thrust to control taxiing is proposed, with full-wing solar-powered UAV (FSUAV) as the research model. This study gives the taxiing mathematical model of FSUAV and designs a taxiing controller based on linear active disturbance rejection control method (LADRC). Simulations are conducted to demonstrate the effectiveness and robustness of the designed controller and compare with PID controller.
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