巡航导弹飞行初段弹道交叉近似计算方法研究

Research on the Method of Approximate Calculation for the Early Part of Ballistic Missile fFlight Ccross

针对巡航导弹初段飞行特点,建立了解析近似计算模型和设计计算流程,可为指挥员进行火力规划提供参考。

In the early part of the flight characteristics of cruise missiles,the establishment of the approximate analytical model and the design calculation process,the fire commanders plan for reference.