导弹对跑道封锁概率及进入角偏差计算方法研究

针对智能导弹对机场跑道的切割封锁模式，以概率积分的方法描述存在进入角偏差和开舱点位置偏差时的封锁效能问题。在导弹开舱点位置偏差确定的情况下，应用封锁概率反验计算进入角偏差的允许范围。由计算结果知，该方法能够体现智能导弹对跑道的封锁效果以及确定进入角偏差范围，可为智能导弹的沿途打击任务分析提供一定依据。

Study on Calculating Interdiction Probability and Entry Angle Error of Missile to Runway

The interdiction effectiveness problem was described with probability integral method for the runway cut-blanked modes of intelligence, when entry angle error and open cabin position error exist. On the condition of open cabin position error determined, the allowable range of entry angle error was inversely calculated with interdiction probability. The calculated results indicate that the method men?tioned can manifest the intelligence missile interdiction efficiency to the runway and the range of entry angle error, which provides available basis for analyzing the intelligence missile attack assignment on tne way.