비선형 힌지를 갖는 접는 미사일 조종날개에 대한 모델 수립 및 동적 특성 = Dynamic characteristics and model establishment of deployable missile control fin with nonlinear hinge

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dc.contributor.advisor이인-
dc.contributor.advisorLee, In-
dc.contributor.author김대관-
dc.contributor.authorKim, Dae-Kwan-
dc.date.accessioned2011-12-12T07:21:40Z-
dc.date.available2011-12-12T07:21:40Z-
dc.date.issued2003-
dc.identifier.urihttp://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=230901&flag=dissertation-
dc.identifier.urihttp://hdl.handle.net/10203/26924-
dc.description학위논문(석사) - 한국과학기술원 : 항공우주공학전공, 2003.8, [ xi, 90 p. ]-
dc.languagekor-
dc.publisher한국과학기술원-
dc.subject모델 개선-
dc.subject부구조물 합성-
dc.subject시스템 식별-
dc.subject미사일 조종날개-
dc.subject비선형 진동-
dc.subjectnonlinear vibration-
dc.subjectmodel improvement-
dc.subjectsubstructure synthesis-
dc.subjectsystem identification-
dc.subjectmissile control fin-
dc.title비선형 힌지를 갖는 접는 미사일 조종날개에 대한 모델 수립 및 동적 특성 = Dynamic characteristics and model establishment of deployable missile control fin with nonlinear hinge-
dc.typeThesis(Master)-
dc.identifier.CNRN230901/325007 -
dc.description.department한국과학기술원 : 항공우주공학전공, -
dc.identifier.uid020013055-
dc.contributor.localauthor이인-
dc.contributor.localauthorLee, In-
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AE-Theses_Master(석사논문)
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