학위논문(박사) - 한국과학기술원 : 항공우주공학과, 2021.2,[vi, 97 p. :]
Closed-Form▼aMaximum Terminal Speed▼aNose-dive Missile▼aImpact Angle Control▼aGuidance; 닫힌 해▼a탄착속력 최대화▼a기수하강 유도탄▼a탄착각 제어▼a유도법칙
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