Guidance algorithm for ascending trajectory of supersonic engine vehicle초음속 엔진 비행체의 상승궤적 유도 알고리듬
- Advisors
- Tahk, Min-Jearesearcher; 탁민제
- 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
- Appears in Collection
- AE-Theses_Master(석사논문)
- Files in This Item
- There are no files associated with this item.
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