{"title":"存在外部扰动时柔性机翼的主动控制","authors":"Yun Fu, Yunpeng Liu, Zuoxuan Gan","doi":"10.1109/YAC57282.2022.10023596","DOIUrl":null,"url":null,"abstract":"This paper investigates the problem of vibration reduction for a flexible aircraft wing with store. Active boundary control is developed to reduce the bending and twisting deflections of a flexible aircraft wing subjected to external disturbances. To handle the impact of the external disturbance, two extended state observers are designed under the active disturbance rejection control (ADRC) method. The developed control strategy guarantee the practical stability of flexible aircraft wing.","PeriodicalId":272227,"journal":{"name":"2022 37th Youth Academic Annual Conference of Chinese Association of Automation (YAC)","volume":"3 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2022-11-19","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Active control for a flexible aircraft wing in the presence of external disturbances\",\"authors\":\"Yun Fu, Yunpeng Liu, Zuoxuan Gan\",\"doi\":\"10.1109/YAC57282.2022.10023596\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper investigates the problem of vibration reduction for a flexible aircraft wing with store. Active boundary control is developed to reduce the bending and twisting deflections of a flexible aircraft wing subjected to external disturbances. To handle the impact of the external disturbance, two extended state observers are designed under the active disturbance rejection control (ADRC) method. The developed control strategy guarantee the practical stability of flexible aircraft wing.\",\"PeriodicalId\":272227,\"journal\":{\"name\":\"2022 37th Youth Academic Annual Conference of Chinese Association of Automation (YAC)\",\"volume\":\"3 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2022-11-19\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2022 37th Youth Academic Annual Conference of Chinese Association of Automation (YAC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/YAC57282.2022.10023596\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2022 37th Youth Academic Annual Conference of Chinese Association of Automation (YAC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/YAC57282.2022.10023596","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Active control for a flexible aircraft wing in the presence of external disturbances
This paper investigates the problem of vibration reduction for a flexible aircraft wing with store. Active boundary control is developed to reduce the bending and twisting deflections of a flexible aircraft wing subjected to external disturbances. To handle the impact of the external disturbance, two extended state observers are designed under the active disturbance rejection control (ADRC) method. The developed control strategy guarantee the practical stability of flexible aircraft wing.