{"title":"四旋翼直升机参数动力学建模与实验辨识","authors":"L. Derafa, T. Madani, A. Benallegue","doi":"10.1109/ICIT.2006.372515","DOIUrl":null,"url":null,"abstract":"In this paper an experimental identification of dynamic parameters of a four rotors mini helicopter is presented. An appropriate model for identification and control synthesis is obtained via modelization procedure where several phenomena are included like gyroscopic effects, aerodynamic friction. A comparison between simulated and real system is made in closed loop system using a same controller. The obtained results show the good estimation of the dynamic model.","PeriodicalId":103105,"journal":{"name":"2006 IEEE International Conference on Industrial Technology","volume":"29 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2006-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"129","resultStr":"{\"title\":\"Dynamic Modelling and Experimental Identification of Four Rotors Helicopter Parameters\",\"authors\":\"L. Derafa, T. Madani, A. Benallegue\",\"doi\":\"10.1109/ICIT.2006.372515\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this paper an experimental identification of dynamic parameters of a four rotors mini helicopter is presented. An appropriate model for identification and control synthesis is obtained via modelization procedure where several phenomena are included like gyroscopic effects, aerodynamic friction. A comparison between simulated and real system is made in closed loop system using a same controller. The obtained results show the good estimation of the dynamic model.\",\"PeriodicalId\":103105,\"journal\":{\"name\":\"2006 IEEE International Conference on Industrial Technology\",\"volume\":\"29 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2006-12-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"129\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2006 IEEE International Conference on Industrial Technology\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICIT.2006.372515\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2006 IEEE International Conference on Industrial Technology","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICIT.2006.372515","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Dynamic Modelling and Experimental Identification of Four Rotors Helicopter Parameters
In this paper an experimental identification of dynamic parameters of a four rotors mini helicopter is presented. An appropriate model for identification and control synthesis is obtained via modelization procedure where several phenomena are included like gyroscopic effects, aerodynamic friction. A comparison between simulated and real system is made in closed loop system using a same controller. The obtained results show the good estimation of the dynamic model.