충돌각 제약조건을 고려한 순간낙하점 기반의 중기 유도 기법Midcourse Guidance laws based on Instantaneous Impact Point considering Final Impact Angle Constraint

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Publisher
한국항공우주학회
Issue Date
2021-07-09
Language
Korean
Citation

한국항공우주학회 2021년도 춘계학술대회

URI
http://hdl.handle.net/10203/286798
Appears in Collection
AE-Conference Papers(학술회의논문)
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