{"title":"无人机防滑制动系统仿真","authors":"Xi Zhang, Hui Lin","doi":"10.23919/CHICC.2018.8483585","DOIUrl":null,"url":null,"abstract":"A dynamics model of UAV braking is established for simulation, and by analyzing the anti-skid braking system, a dual channel anti -skid braking system based on slip-ratio is presented. The fuzzy control theory is used in the control system, and a balance control system is added between the left wheel and right wheel of UAV. The HIL (hardware in loop) experiment results demonstrate that in different conditions, the anti-skid braking system can automatically regulate the brake pressure and keep the UAV from yawing dramatically.","PeriodicalId":158442,"journal":{"name":"2018 37th Chinese Control Conference (CCC)","volume":"35 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"8","resultStr":"{\"title\":\"UAV Anti-Skid Braking System Simulation\",\"authors\":\"Xi Zhang, Hui Lin\",\"doi\":\"10.23919/CHICC.2018.8483585\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A dynamics model of UAV braking is established for simulation, and by analyzing the anti-skid braking system, a dual channel anti -skid braking system based on slip-ratio is presented. The fuzzy control theory is used in the control system, and a balance control system is added between the left wheel and right wheel of UAV. The HIL (hardware in loop) experiment results demonstrate that in different conditions, the anti-skid braking system can automatically regulate the brake pressure and keep the UAV from yawing dramatically.\",\"PeriodicalId\":158442,\"journal\":{\"name\":\"2018 37th Chinese Control Conference (CCC)\",\"volume\":\"35 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2018-07-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"8\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2018 37th Chinese Control Conference (CCC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.23919/CHICC.2018.8483585\",\"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 37th Chinese Control Conference (CCC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23919/CHICC.2018.8483585","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
A dynamics model of UAV braking is established for simulation, and by analyzing the anti-skid braking system, a dual channel anti -skid braking system based on slip-ratio is presented. The fuzzy control theory is used in the control system, and a balance control system is added between the left wheel and right wheel of UAV. The HIL (hardware in loop) experiment results demonstrate that in different conditions, the anti-skid braking system can automatically regulate the brake pressure and keep the UAV from yawing dramatically.
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