중력에 의한 호밍 궤적을 고려한 효과적인 종말유도 선도 각 보정 방법An Effective Methodology for Lead Angle Compensation for Terminal Guidance Accounting for Gravity-Affected Homing Trajectory
- Publisher
- 한국항공우주학회
- Issue Date
- 2014-11-20
- Language
- Korean
- Citation
한국항공우주학회 2014년도 추계학술대회
- Appears in Collection
- AE-Conference Papers(학술회의논문)
- Files in This Item
- There are no files associated with this item.
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