{"title":"基于小波处理飞行试验数据的在线鲁棒气动伺服弹性稳定裕度分析","authors":"Hong-chao Li, Zhong-ke Shi, Weixian Tang","doi":"10.1109/ISSCAA.2006.1627440","DOIUrl":null,"url":null,"abstract":"An on-line method based on robust mu analysis is presented to evaluate the stability margin of multi-loop aeroservoelastic system from flight testing data. The flight data is preprocessed to remove noise by wavelet filter in time-frequency domain. The method for stability analysis is described and the classical stability margin used for single-input-single-output (SISO) system has been extended to multi-loop system. With the present definition for uncertainty, the guaranteed bounds on gain and phase margin can been calculated for a specified mu value. A nonparametric identification is applied to determine the open-loop transfer function from testing data. This method enables us to implement on-line stability evaluation without theory model. Finally, the analysis results are compared with return difference matrix method to illustrate the efficiency of the new method","PeriodicalId":275436,"journal":{"name":"2006 1st International Symposium on Systems and Control in Aerospace and Astronautics","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2006-05-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"On-line robust aeroservoelastic stability margin analysis from wavelet-processed flight testing data\",\"authors\":\"Hong-chao Li, Zhong-ke Shi, Weixian Tang\",\"doi\":\"10.1109/ISSCAA.2006.1627440\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"An on-line method based on robust mu analysis is presented to evaluate the stability margin of multi-loop aeroservoelastic system from flight testing data. The flight data is preprocessed to remove noise by wavelet filter in time-frequency domain. The method for stability analysis is described and the classical stability margin used for single-input-single-output (SISO) system has been extended to multi-loop system. With the present definition for uncertainty, the guaranteed bounds on gain and phase margin can been calculated for a specified mu value. A nonparametric identification is applied to determine the open-loop transfer function from testing data. This method enables us to implement on-line stability evaluation without theory model. Finally, the analysis results are compared with return difference matrix method to illustrate the efficiency of the new method\",\"PeriodicalId\":275436,\"journal\":{\"name\":\"2006 1st International Symposium on Systems and Control in Aerospace and Astronautics\",\"volume\":\"1 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2006-05-08\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2006 1st International Symposium on Systems and Control in Aerospace and Astronautics\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ISSCAA.2006.1627440\",\"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 1st International Symposium on Systems and Control in Aerospace and Astronautics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ISSCAA.2006.1627440","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
On-line robust aeroservoelastic stability margin analysis from wavelet-processed flight testing data
An on-line method based on robust mu analysis is presented to evaluate the stability margin of multi-loop aeroservoelastic system from flight testing data. The flight data is preprocessed to remove noise by wavelet filter in time-frequency domain. The method for stability analysis is described and the classical stability margin used for single-input-single-output (SISO) system has been extended to multi-loop system. With the present definition for uncertainty, the guaranteed bounds on gain and phase margin can been calculated for a specified mu value. A nonparametric identification is applied to determine the open-loop transfer function from testing data. This method enables us to implement on-line stability evaluation without theory model. Finally, the analysis results are compared with return difference matrix method to illustrate the efficiency of the new method