Takagi-Sugeno 퍼지 시스템에 대한 최적 제어기 설계 및 우주 비행체의 자세제어 응용Design of the Optimal Controller for Takagi-Sugeno Fuzzy Systems and Its Application to Spacecraft control

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dc.contributor.author박연묵ko
dc.contributor.author탁민제ko
dc.date.accessioned2013-03-03T10:03:53Z-
dc.date.available2013-03-03T10:03:53Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued2001-07-
dc.identifier.citation제어자동화시스템공학논문지, v.7, no.7, pp.589 - 596-
dc.identifier.issn1225-9853-
dc.identifier.urihttp://hdl.handle.net/10203/78309-
dc.description.abstractIn this paper, a new design methodology for the optimal control of nonlinear systems described by the TS(Takagi-Sugeno) fuzzy model is proposed. First, a new theorem concerning the optimal stabilizing control of a general nonlinear dynamic system is proposed. Next, based on the proposed theorem and the inverse optimal approach, an optimal controller synthesis procedure for a TS fuzzy system is given, Also, it is shown that the optimal controller can be found by solving a linear matrix inequality problem. Finally, the proposed method is applied to the attitude control of a rigid spacecraft to demonstrate its validity.-
dc.languageKorean-
dc.publisher제어자동화시스템공학회-
dc.titleTakagi-Sugeno 퍼지 시스템에 대한 최적 제어기 설계 및 우주 비행체의 자세제어 응용-
dc.title.alternativeDesign of the Optimal Controller for Takagi-Sugeno Fuzzy Systems and Its Application to Spacecraft control-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume7-
dc.citation.issue7-
dc.citation.beginningpage589-
dc.citation.endingpage596-
dc.citation.publicationname제어자동화시스템공학논문지-
dc.contributor.localauthor탁민제-
dc.contributor.nonIdAuthor박연묵-
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AE-Journal Papers(저널논문)
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