本发明是关于寻的制导导弹如何一面回避防空火力网,一面继续将导弹导向目标的制导方法。用寻的方式制导导弹时,为确保高的最终精度,在制导的初始段就修正导弹飞行弹道的方向误差。所以,除目标作高速机动的情况外,通常导弹的飞行弹道逐渐变成一条直线。因此,用拦截计算机计 The present invention relates to a guidance method for finding a guided missile that avoids an anti-aircraft fire net while continuing to guide a missile to a target. To guide the missile using the hunt method, in order to ensure a high final accuracy, the directional error of the missile flight trajectory is corrected in the initial stage of the guidance. Therefore, except when the target is maneuvering at high speed, the missile trajectory usually becomes a straight line. Therefore, using intercepting computers