Gain-scheduled state feedback control design technique for flight vehicles

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dc.contributor.authorLee, CHko
dc.contributor.authorChung, Myung Jinko
dc.date.accessioned2013-03-04T01:38:45Z-
dc.date.available2013-03-04T01:38:45Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued2001-01-
dc.identifier.citationIEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.37, no.1, pp.173 - 182-
dc.identifier.issn0018-9251-
dc.identifier.urihttp://hdl.handle.net/10203/81343-
dc.description.abstractFor multi-input, multi-output (MIMO) nonlinearly parameter dependent linear parameter-varying (LPV) systems with multiple parameters, a design method of gain-scheduled state feedback control using a minimum sensitivity eigenvalue assignment of the frozen parameter closed-loop system with quadratic stability checks is proposed. The proposed design method is applied to the bank-to-turn (BTT) control of a flight vehicle, and the nonlinear 6 degree of freedom (DOF) simulations are performed to show the usefulness as a gain-scheduled state feedback control scheme.-
dc.languageEnglish-
dc.publisherIEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC-
dc.subjectPARAMETER-VARYING SYSTEMS-
dc.subjectTRANSFORMATIONS-
dc.titleGain-scheduled state feedback control design technique for flight vehicles-
dc.typeArticle-
dc.identifier.wosid000167551500013-
dc.identifier.scopusid2-s2.0-0035039951-
dc.type.rimsART-
dc.citation.volume37-
dc.citation.issue1-
dc.citation.beginningpage173-
dc.citation.endingpage182-
dc.citation.publicationnameIEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS-
dc.contributor.localauthorChung, Myung Jin-
dc.contributor.nonIdAuthorLee, CH-
dc.type.journalArticleArticle-
dc.subject.keywordPlusPARAMETER-VARYING SYSTEMS-
dc.subject.keywordPlusTRANSFORMATIONS-
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