횡방향 기동을 하는 위성발사체의 3차원 궤적최적화와 직접식 유도기법 3-Dimensional Trajectory Optimization and Explicit Guidance for a Satellite Launch Vehicle with Yaw Maneuver

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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
URI
http://hdl.handle.net/10203/82551
Appears in Collection
AE-Journal Papers(저널논문)
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