단거리 공대공 유도탄의 180도 회전기동 해석을 위한 제어입력 이산화 및 최적화 기법Control Input Discretization and Optimization Method for Half-Turn Maneuver Analysis of Short Range Air-to-Air Missile
- Publisher
- 한국항공우주학회
- Issue Date
- 2009-04-16
- Language
- Korean
- Citation
한국항공우주학회 2009년도 춘계학술대회
- Appears in Collection
- AE-Conference Papers(학술회의논문)
- Files in This Item
- There are no files associated with this item.
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