{"title":"高超声速飞行器切换控制设计","authors":"Shuping Tan, Zhibin Li","doi":"10.1109/CCDC.2010.5498526","DOIUrl":null,"url":null,"abstract":"An adaptive switching controller is designed and analyzed for the longitudinal dynamics of a generic hypersonic air vehicle in the whole cruise phase rather than a trimmed working condition. This model is nonlinear, multivariable and unstable. The adaptive controller presented in this paper consists of a local linearization method, an adaptive switching law and a nonlinear feedback control law. Furthermore, a theorem is obtained that the closed-loop system under the adaptive switching control is stable.","PeriodicalId":227938,"journal":{"name":"2010 Chinese Control and Decision Conference","volume":"14 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2010-05-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Switching control design for a hypersonic flight vehicle\",\"authors\":\"Shuping Tan, Zhibin Li\",\"doi\":\"10.1109/CCDC.2010.5498526\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"An adaptive switching controller is designed and analyzed for the longitudinal dynamics of a generic hypersonic air vehicle in the whole cruise phase rather than a trimmed working condition. This model is nonlinear, multivariable and unstable. The adaptive controller presented in this paper consists of a local linearization method, an adaptive switching law and a nonlinear feedback control law. Furthermore, a theorem is obtained that the closed-loop system under the adaptive switching control is stable.\",\"PeriodicalId\":227938,\"journal\":{\"name\":\"2010 Chinese Control and Decision Conference\",\"volume\":\"14 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2010-05-26\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2010 Chinese Control and Decision Conference\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/CCDC.2010.5498526\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2010 Chinese Control and Decision Conference","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CCDC.2010.5498526","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Switching control design for a hypersonic flight vehicle
An adaptive switching controller is designed and analyzed for the longitudinal dynamics of a generic hypersonic air vehicle in the whole cruise phase rather than a trimmed working condition. This model is nonlinear, multivariable and unstable. The adaptive controller presented in this paper consists of a local linearization method, an adaptive switching law and a nonlinear feedback control law. Furthermore, a theorem is obtained that the closed-loop system under the adaptive switching control is stable.
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