Generalized missile guidance law for impact angle control일반화된 충돌각 제어 유도법칙 연구
- Advisors
- Tahk, Min-Jearesearcher; 탁민제
- Description
- 한국과학기술원 : 항공우주공학전공,
- Publisher
- 한국과학기술원
- Issue Date
- 2012
- Identifier
- 487163/325007 / 020085308
- Language
- eng
- Description
학위논문(박사) - 한국과학기술원 : 항공우주공학전공, 2012.2, [ vii, 128 p. ]
- Keywords
impact angle control; guidance law; optimality; analytic solution; 유도법칙; 충돌각 제어; 최적성; 해석해; 시스템 지연; system lag
- Appears in Collection
- AE-Theses_Ph.D.(박사논문)
- Files in This Item
- There are no files associated with this item.
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