This paper offers relative movement equation of missile and target, deducing a formula that is a basis of picking out proportional coefficient and gravity over compensation coefficient.
本文给出了导弹与目标的相对运动方程，并推倒出选取比例系数和过重力补偿系数所依据的公式。
In order to attack the target with big impact Angle, over compensation of gravity is added to the design.
为了实现大落角攻击目标，进行了末制导过重补设计。
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