当不计飞行器的响应时间、纵向加速度和控制溢出时，蜕化为常规比例导引。
Neglecting the time canstants, axial accelerations and the control overflow, the optimal strategy is reduced to the conventional proportional navigation guidance law.
在直升机、战斗机、舰船、无人机、导引头、地面车辆和航天飞行器都有应用。
In helicopters, fighter planes, ships, guides, ground vehicles and spacecraft are applied.
在直升机、战斗机、舰船、无人机、导引头、地面车辆和航天飞行器都有应用。
In helicopters, fighter planes, ships, guides, ground vehicles and spacecraft are applied.
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