Autopilot design synthesis for highly maneuverable STT(Skid-To-Turn) missiles = 고기동 STT 유도탄의 오토파일롯 설계기법 연구

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Advisors
Tahk, Min-Jearesearcher탁민제
Description
한국과학기술원 : 항공우주공학전공,
Publisher
한국과학기술원
Issue Date
2012
Identifier
487162/325007  / 020085243
Language
eng
Description

학위논문(박사) - 한국과학기술원 : 항공우주공학전공, 2012.2, [ vi, 126 p. ]

Keywords

autopilot design; Highly maneuverable STT missile; nonlinear dynamic control; aerodynamic coupling modeling; 고기동 STT 미사일; 오토파일롯 설계; 비선형 동적제어기; 공력학적 커플링 모델링; 새로운 구조의 구동제어시스템; new structure of actuation control system

URI
http://hdl.handle.net/10203/179633
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=487162&flag=dissertation
Appears in Collection
AE-Theses_Ph.D.(박사논문)
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