Guidance algorithm for ascending trajectory of supersonic engine vehicle = 초음속 엔진 비행체의 상승궤적 유도 알고리듬

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Advisors
Tahk, Min-Jearesearcher탁민제
Description
한국과학기술원 : 항공우주공학전공,
Publisher
한국과학기술원
Issue Date
2012
Identifier
487504/325007  / 020103068
Language
eng
Description

학위논문(석사) - 한국과학기술원 : 항공우주공학전공, 2012.2, [ vii, 58 p. ]

Keywords

Guidance; PEG Algorithm; 미사일 유도; PEG 알고리듬; 초음속 엔진 미사일; Supersoonic Engine missile

URI
http://hdl.handle.net/10203/179695
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=487504&flag=dissertation
Appears in Collection
AE-Theses_Master(석사논문)
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