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스마트 무인기 지상시험장치의 다물체 동역학 및 구조진동해석

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dc.contributor.author박강균-
dc.contributor.author김동현-
dc.contributor.author김동만-
dc.contributor.author최현철-
dc.contributor.author안오성-
dc.date.accessioned2022-12-27T04:53:00Z-
dc.date.available2022-12-27T04:53:00Z-
dc.date.issued2010-
dc.identifier.issn1598-9127-
dc.identifier.issn2636-0640-
dc.identifier.urihttps://scholarworks.gnu.ac.kr/handle/sw.gnu/25942-
dc.description.abstractIn this study, computational multi-body dynamics and structural vibration analyses including some impact condition have been conducted for the ground flight test system of the developed smart UAV model. Designed ground test system has four degree-of-freedom motions with limited motion control mechanism. Design safety margin designs for several structural components are tested and verified considering expected critical motions (pitching and rolling) of the test smart UAV model. Computational results for various analysis conditions are practically presented in detail. Futhermore, proper design modifications of the initially designed test equipment in order to guarantee or increase structural safety have been successfully conducted in the design stage.-
dc.format.extent8-
dc.language한국어-
dc.language.isoKOR-
dc.publisher한국군사과학기술학회-
dc.title스마트 무인기 지상시험장치의 다물체 동역학 및 구조진동해석-
dc.title.alternativeMulti-body Dynamics and Structural Vibration Analyses of Smart UAV Ground Test Equipment-
dc.typeArticle-
dc.publisher.location대한민국-
dc.identifier.bibliographicCitation한국군사과학기술학회지, v.13, no.1, pp 22 - 29-
dc.citation.title한국군사과학기술학회지-
dc.citation.volume13-
dc.citation.number1-
dc.citation.startPage22-
dc.citation.endPage29-
dc.identifier.kciidART001418691-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClasskci-
dc.subject.keywordAuthorSmart UAV(스마트 무인기)-
dc.subject.keywordAuthor지상시험장치(Ground Test Equipment)-
dc.subject.keywordAuthor다물체 동역학(Multi-body Dynamics)-
dc.subject.keywordAuthor유한요소해석(Finite Element Analysis)-
dc.subject.keywordAuthor충돌해석(Impact Analysis)-
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