首页> 外国专利> In-flight programming method of the triggering moment of a projectile element, firing control and fuse for carrying out this method

In-flight programming method of the triggering moment of a projectile element, firing control and fuse for carrying out this method

机译:弹丸元件触发力矩的飞行中编程方法,射击控制和执行该方法的保险丝

摘要

The invention relates to a fly programming method of a initiation time of an element (17) of the projectile (3) from a firing control (9) of a weapon (1), method characterized by the following steps: measuring the initial velocity Vo of the projectile (3), measuring the expulsion speed of the projectile (3) into at least one other point on its trajectory after exiting the weapon barrel, is determined from these measured values ​​an optimal trigger time for the element (17) of the projectile so as to minimize the deviation between the impact to the actual soil and ground impact desired for the projectile or a payload it releases its path, is transmitted to the projectile a programming or corrective programming considering this optimal trigger time.
机译:本发明涉及一种从武器(1)的发射控制装置(9)的射弹(3)的元件(17)的启动时间的飞行编程方法,该方法的特征在于以下步骤: 测量弹丸(3)的初始速度Vo, 测量弹丸(3)离开武器枪管后进入其轨迹上至少一个点的排出速度, <从这些测量值确定ListItem>弹丸元素(17)的最佳触发时间,以最小化对弹丸或释放其路径的有效载荷所需的对实际土壤的影响与地面影响之间的偏差, 会考虑此最佳触发时间,以编程或校正编程的方式传输到弹丸。

著录项

  • 公开/公告号EP0887613A3

    专利类型

  • 公开/公告日1999-01-20

    原文格式PDF

  • 申请/专利权人 GIAT INDUSTRIES;

    申请/专利号EP19980104650

  • 发明设计人 LAMORLETTE GÉRARD;BREDY THIERRY;

    申请日1998-03-14

  • 分类号F41G7/30;

  • 国家 EP

  • 入库时间 2022-08-22 02:19:38

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