유연구조 발사체의 고전구조 자세제어기 최적설계Optimal Design of the Classical-Type Attitude Controller for a Flexible Launch Vehicle
- Publisher
- 한국항공우주학회
- Issue Date
- 1998-01
- Language
- Korean
- Citation
한국항공우주학회지, v.26, no.7, pp.96 - 107
- ISSN
- 1225-1348
- Appears in Collection
- AE-Journal Papers(저널논문)
- Files in This Item
- There are no files associated with this item.
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