Neglecting the time canstants, axial accelerations and the control overflow, the optimal strategy is reduced to the conventional proportional navigation guidance law.
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。
Finally, the computer numerical simulation of interceptions adopting optimal guidance law and proportional navigation is processed respectively. The result of simulation shows the perfect...
最后，采用新型最优制导律和传统比例导引律分别进行了拦截过程的计算机数值仿真，仿真结果表明了这种新型最优制导律的有效性。
When targets fly with non-maneuvering, the optimal guidance law is the proportional guidance law with a changeable factor.
当目标作非机动飞行时，最优制导律是一种变比例系数的比例制导。
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