횡방향 기동을 하는 위성발사체의 3차원 궤적최적화와 직접식 유도기법3-Dimensional Trajectory Optimization and Explicit Guidance for a Satellite Launch Vehicle with Yaw Maneuver
- Publisher
- 제어·로봇·시스템학회
- Issue Date
- 2002-07
- Language
- Korean
- Citation
제어.로봇.시스템학회 논문지, v.8, no.7, pp.613 - 623
- ISSN
- 1976-5622
- Appears in Collection
- AE-Journal Papers(저널논문)
- Files in This Item
- There are no files associated with this item.
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