{"title":"无人机在湍流中的卡尔曼滤波","authors":"Zhou Jian, Xie Rong, Gu Xiao-jie, Li Wen-chao","doi":"10.1109/ICCIAUTOM.2011.6183981","DOIUrl":null,"url":null,"abstract":"This paper describes a method for generating the turbulent wind field which accords with the characteristics of atmospheric turbulence model. The model of turbulent wind with colored noise is presented and then the whitening model of the UAV state is obtained by the state augmentation. This paper also designs a Kalman filter based on the colored noisey flight speed of the UAV which can solve the problem that the classic Kalman filter only can be applied in the white color model. The simulation demostrates that this filter can reduce the influence of the wind turbulence on the UAV flight speed, and thus the accuracy of the flight speed control can be satisfied.","PeriodicalId":177039,"journal":{"name":"2011 2nd International Conference on Control, Instrumentation and Automation (ICCIA)","volume":"62 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2011-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"The Kalman filter for UAV in the turbulent flow\",\"authors\":\"Zhou Jian, Xie Rong, Gu Xiao-jie, Li Wen-chao\",\"doi\":\"10.1109/ICCIAUTOM.2011.6183981\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper describes a method for generating the turbulent wind field which accords with the characteristics of atmospheric turbulence model. The model of turbulent wind with colored noise is presented and then the whitening model of the UAV state is obtained by the state augmentation. This paper also designs a Kalman filter based on the colored noisey flight speed of the UAV which can solve the problem that the classic Kalman filter only can be applied in the white color model. The simulation demostrates that this filter can reduce the influence of the wind turbulence on the UAV flight speed, and thus the accuracy of the flight speed control can be satisfied.\",\"PeriodicalId\":177039,\"journal\":{\"name\":\"2011 2nd International Conference on Control, Instrumentation and Automation (ICCIA)\",\"volume\":\"62 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2011-12-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2011 2nd International Conference on Control, Instrumentation and Automation (ICCIA)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICCIAUTOM.2011.6183981\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2011 2nd International Conference on Control, Instrumentation and Automation (ICCIA)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICCIAUTOM.2011.6183981","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
This paper describes a method for generating the turbulent wind field which accords with the characteristics of atmospheric turbulence model. The model of turbulent wind with colored noise is presented and then the whitening model of the UAV state is obtained by the state augmentation. This paper also designs a Kalman filter based on the colored noisey flight speed of the UAV which can solve the problem that the classic Kalman filter only can be applied in the white color model. The simulation demostrates that this filter can reduce the influence of the wind turbulence on the UAV flight speed, and thus the accuracy of the flight speed control can be satisfied.