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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 is directed to a process of program in the air a moment of initiation of a component (17) of the projectile (3) from a driving range (9) of a gun (1), a process characterized by the following steps:we measure the initial speed vo of the projectile (3), the rate of removal of the projectile (3) and at least one other point of the path from the outlet of the gun tube.it is determined from the measured values of a second trigger element (17) is optimal for the projectile so as to minimize the difference between the actual and the impact with the ground to the desired projectile impact with the ground or a payload to release its trajectory.we send the projectile or a correction of the programming programming taking into account the time optimal activation.
机译:本发明涉及一种从枪(1)的射程(9)起射弹(3)的部件(17)的瞬间在空中编程的过程,该过程的特征在于以下步骤:我们测量弹丸(3)的初始速度vo,弹丸(3)的清除率以及从枪管出口的路径的至少另一个点,这是根据第二秒的测量值确定的触发元件(17)对于弹丸是最佳的,以便将实际与地面的撞击与所需的弹丸对地面或有效载荷的撞击之间的差异最小化,以释放其轨迹。编程时要考虑到最佳激活时间。

著录项

  • 公开/公告号EP0887613B1

    专利类型

  • 公开/公告日2003-08-20

    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 GERARD;BREDY THIERRY;

    申请日1998-03-14

  • 分类号F41G7/30;

  • 国家 EP

  • 入库时间 2022-08-21 23:53:48

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