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.
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美
- 本文推導了 ATBM尋的引信最佳炸點(diǎn)控制算法 ,及使用定向戰斗部時(shí)所需的彈體坐標系中的脫靶方位 ,其中對應于最佳炸點(diǎn)的最佳延時(shí)為剩余飛行時(shí)間減去破片飛行時(shí)間。