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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Advisors
이인researcherLee, Inresearcher
Description
한국과학기술원 : 항공우주공학전공,
Publisher
한국과학기술원
Issue Date
2003
Identifier
230901/325007  / 020013055
Language
kor
Description

학위논문(석사) - 한국과학기술원 : 항공우주공학전공, 2003.8, [ xi, 90 p. ]

Keywords

모델 개선; 부구조물 합성; 시스템 식별; 미사일 조종날개; 비선형 진동; nonlinear vibration; model improvement; substructure synthesis; system identification; missile control fin

URI
http://hdl.handle.net/10203/26924
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=230901&flag=dissertation
Appears in Collection
AE-Theses_Master(석사논문)
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