학위논문(박사) - 한국과학기술원 : 항공우주공학과, 2021.2,[vi, 101 p. :]
Optimal guidance law▼aTerminal acceleration constraint▼aseudo acceleration feed-back▼aTime-to-go weighted cost function▼aDynamics error analysis; 최적유도기법▼a종말가속도 구속조건▼a의사가속도 피드백▼aTime-to-go 가중함수▼a다이나믹스 오차분석
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