A Modeling of Aeroservoelasticity and a Design of Attitude Controller with High Aspect Ratio Flexible Wings = 고세장비 유연 날개 비행체의 서보공탄성 모델링 및 자세 추종 제어 시스템 설계

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Advisors
Shim, Hyun-Chulresearcher심현철
Description
한국과학기술원 : 항공우주공학전공,
Publisher
한국과학기술원
Issue Date
2012
Identifier
487512/325007  / 020103378
Language
eng
Description

학위논문(석사) - 한국과학기술원 : 항공우주공학전공, 2012.2, [ v, 46 p. ]

Keywords

Aeroservoelasticity; H2/H∞ controller; Mixed-objective problem; 서보공탄성; H2/H∞ 제어기; 다목적 최적 기법; 선형 행렬 부등식; Linear Matrix Inequality(LMI)

URI
http://hdl.handle.net/10203/179687
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=487512&flag=dissertation
Appears in Collection
EE-Theses_Master(석사논문)
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