A. Martinez-Vasquez, A. Rodriguez-mata, I. González-Hernández, S. Salazar, Alejandro Montiel-Varela, R. Lozano
{"title":"无人机阵风估计的线性观测器","authors":"A. Martinez-Vasquez, A. Rodriguez-mata, I. González-Hernández, S. Salazar, Alejandro Montiel-Varela, R. Lozano","doi":"10.1109/ICEEE.2015.7357983","DOIUrl":null,"url":null,"abstract":"This paper deals with the problem of estimating the disturbances due a wind gust in a Quadrotor rotorcraft. A linear observer with integral action for estimating the disturbance due a wind is presented. Simulation and real-time result are presented for test performance of control law proposed. The real-time test was ralized in hover fly mode based on GPS sensor signal.","PeriodicalId":285783,"journal":{"name":"2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)","volume":"119 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2015-12-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"10","resultStr":"{\"title\":\"Linear observer for estimating wind gust in UAV's\",\"authors\":\"A. Martinez-Vasquez, A. Rodriguez-mata, I. González-Hernández, S. Salazar, Alejandro Montiel-Varela, R. Lozano\",\"doi\":\"10.1109/ICEEE.2015.7357983\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper deals with the problem of estimating the disturbances due a wind gust in a Quadrotor rotorcraft. A linear observer with integral action for estimating the disturbance due a wind is presented. Simulation and real-time result are presented for test performance of control law proposed. The real-time test was ralized in hover fly mode based on GPS sensor signal.\",\"PeriodicalId\":285783,\"journal\":{\"name\":\"2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)\",\"volume\":\"119 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2015-12-17\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"10\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICEEE.2015.7357983\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2015 12th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICEEE.2015.7357983","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
This paper deals with the problem of estimating the disturbances due a wind gust in a Quadrotor rotorcraft. A linear observer with integral action for estimating the disturbance due a wind is presented. Simulation and real-time result are presented for test performance of control law proposed. The real-time test was ralized in hover fly mode based on GPS sensor signal.