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Method of controlling antiaircraft fire

机译:控制防空火的方法

摘要

A method of controlling antiaircraft fire is described in which an aircraft is tracked continuously during the flight of a burst of projectiles and the probability of a hit is continuously revised according to the latest target maneuver as the projectiles proceed to the intercept point. If, before all of the projectiles reach the aircraft, the probability of a hit falls below a specified level, another burst of projectiles is fired. As this second burst proceeds to target its computed probability of hit is combined with that of the previously fired burst to determine the cumulative probability of hit of the two bursts taken together. If, before the second burst reaches the target, the cumulative probability falls below the specified level then a third burst is fired. This activity repeats until the cumulative probability of hit is driven up and kept up above the specified level.
机译:描述了一种控制防空火力的方法,其中在弹丸的飞行期间连续跟踪飞机,并且随着弹丸前进到拦截点,根据最新的目标机动不断地改变命中的概率。如果在所有弹丸到达飞机之前,命中的可能性降到指定水平以下,则发射另一弹丸。当第二个脉冲串继续以目标为目标时,将其计算出的命中概率与先前发射的脉冲串相结合,以确定两个脉冲合在一起的累积命中概率。如果在第二个突发到达目标之前,累积概率降到指定级别以下,则触发第三个突发。重复此活动,直到累积命中概率被提高并保持在指定水平之上。

著录项

  • 公开/公告号US4449041A

    专利类型

  • 公开/公告日1984-05-15

    原文格式PDF

  • 申请/专利权人 RAYTHEON COMPANY;

    申请/专利号US19830457831

  • 发明设计人 DONALD D. GIRARD;

    申请日1983-01-14

  • 分类号G06F15/58;F41G3/04;

  • 国家 US

  • 入库时间 2022-08-22 08:38:44

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