An optimum ATBM seeker fuze time delay algorithm and the azimuthal angle for the directional warhead in the missile coordinate system are deduced. The corresponding optimum burst time is equal to missile time to go deducting fragments flying time.

• 本文推导了 ATBM寻的引信最佳炸点控制算法 ,及使用定向战斗部时所需的弹体坐标系中的脱靶方位 ,其中对应于最佳炸点的最佳延时为剩余飞行时间减去破片飞行时间。