{"title":"Missile Autopilot Design Using a Generalized Hamiltonian Formulation","authors":"Ching-Fang Lin, J. Cloutier, J. Evers","doi":"10.1109/AEROCS.1993.721027","DOIUrl":null,"url":null,"abstract":"This paper presents the application of robust multivariable control to a missile autopilot design. A synergistic algorithm based on the generalized Hamiltonian formulation is applied to robust autopilot design for the HAVE DASH II missile system. The design endures significant kinematic and inertia couplings, aerodynamic parameter variations and high frequency flexible effects.","PeriodicalId":170527,"journal":{"name":"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,","volume":"3 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1993-05-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"4","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings. The First IEEE Regional Conference on Aerospace Control Systems,","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AEROCS.1993.721027","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 4
Abstract
This paper presents the application of robust multivariable control to a missile autopilot design. A synergistic algorithm based on the generalized Hamiltonian formulation is applied to robust autopilot design for the HAVE DASH II missile system. The design endures significant kinematic and inertia couplings, aerodynamic parameter variations and high frequency flexible effects.
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