{"title":"基于优化自适应Thau观测器的四旋翼无人机鲁棒故障估计","authors":"Zhaohui Cen, H. Noura, Younes Al Younes","doi":"10.1109/ICUAS.2013.6564732","DOIUrl":null,"url":null,"abstract":"As a result of modeling uncertainties, data decade unbalanceand noise, Fault Estimation (FE) for real quadrotor is rough with low accuracy when model observer based FE scheme-Adaptive Thau Observer(ATO) is applied. Based on these issues, this paper proposes a comprehensive optimization approach on FE accuracy for quadrotor using ATO. First, the ATO observer is improved by adding unmolded terms with parameters derived from identification. Secondly, a data adjustment based on amplifying and reducing is introduced to overcome the data decade unbalance. Thirdly, the Infinite Impulse Response (IIR) filter is utilized to decrease the noise in measurement signals. Finally, experiments for injecting the rotor fault have been carried out to show the effectiveness of the proposed optimization method and the results are discussed.","PeriodicalId":322089,"journal":{"name":"2013 International Conference on Unmanned Aircraft Systems (ICUAS)","volume":"8 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2013-05-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"16","resultStr":"{\"title\":\"Robust Fault Estimation on a real quadrotor UAV using optimized Adaptive Thau Observer\",\"authors\":\"Zhaohui Cen, H. Noura, Younes Al Younes\",\"doi\":\"10.1109/ICUAS.2013.6564732\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"As a result of modeling uncertainties, data decade unbalanceand noise, Fault Estimation (FE) for real quadrotor is rough with low accuracy when model observer based FE scheme-Adaptive Thau Observer(ATO) is applied. Based on these issues, this paper proposes a comprehensive optimization approach on FE accuracy for quadrotor using ATO. First, the ATO observer is improved by adding unmolded terms with parameters derived from identification. Secondly, a data adjustment based on amplifying and reducing is introduced to overcome the data decade unbalance. Thirdly, the Infinite Impulse Response (IIR) filter is utilized to decrease the noise in measurement signals. Finally, experiments for injecting the rotor fault have been carried out to show the effectiveness of the proposed optimization method and the results are discussed.\",\"PeriodicalId\":322089,\"journal\":{\"name\":\"2013 International Conference on Unmanned Aircraft Systems (ICUAS)\",\"volume\":\"8 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2013-05-28\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"16\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2013 International Conference on Unmanned Aircraft Systems (ICUAS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICUAS.2013.6564732\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2013 International Conference on Unmanned Aircraft Systems (ICUAS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICUAS.2013.6564732","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Robust Fault Estimation on a real quadrotor UAV using optimized Adaptive Thau Observer
As a result of modeling uncertainties, data decade unbalanceand noise, Fault Estimation (FE) for real quadrotor is rough with low accuracy when model observer based FE scheme-Adaptive Thau Observer(ATO) is applied. Based on these issues, this paper proposes a comprehensive optimization approach on FE accuracy for quadrotor using ATO. First, the ATO observer is improved by adding unmolded terms with parameters derived from identification. Secondly, a data adjustment based on amplifying and reducing is introduced to overcome the data decade unbalance. Thirdly, the Infinite Impulse Response (IIR) filter is utilized to decrease the noise in measurement signals. Finally, experiments for injecting the rotor fault have been carried out to show the effectiveness of the proposed optimization method and the results are discussed.