관성모멘트 분포특성을 이용한 피치 바이어스 모멘텀 위성의 자세제어기 특성 해석Analysis on the Attitude Controller for Pitch Bias Momentum Satellite Using Moment of Inertia Distribution
- Publisher
- 한국항공우주학회
- Issue Date
- 1998-04
- Language
- Korean
- Citation
한국항공우주학회지, v.26, no.8, pp.74 - 82
- 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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