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in - flight - programming techniques for auslu00f6sungsmoment a geschosselements, fire control and device to implement this method

机译:在空中飞行的编程技术,火力发电厂,火控装置和实现该方法的装置

摘要

A process for the in-flight programming of a trigger time for an element of a projectile by a fire control system of a weapon, wherein the muzzle velocity (Vo) of the projectile is measured and the distancing velocity of the projectile at at least one other point during its trajectory after exiting the weapon barrel it measured. Based on these measured values an optimal trigger time is determined for the element so as to minimize the difference between the actual ground impact point and the desired ground impact point for the projectile or for a payload released during the payload's trajectory, and a programming or corrective programming is transmitted to the projectile which takes this optimal trigger time into account.
机译:一种通过武器的火控系统对弹丸要素的触发时间进行飞行中编程的方法,其中,测量弹丸的枪口速度(Vo),使弹丸的分离速度至少为一个离开它所测量的武器桶后的轨迹中的其他点。基于这些测量值,为元件确定最佳触发时间,以使弹丸或有效载荷轨迹期间释放的有效载荷的实际地面冲击点与所需地面冲击点之间的差异最小,并进行编程或修正程序将传输到射弹,并考虑到最佳触发时间。

著录项

  • 公开/公告号DE69817267D1

    专利类型

  • 公开/公告日2003-09-25

    原文格式PDF

  • 申请/专利权人 GIAT INDUSTRIES VERSAILLES;

    申请/专利号DE1998617267T

  • 发明设计人 LAMORLETTE GERARD;BREDY THIERRY;

    申请日1998-03-14

  • 分类号F41G7/30;

  • 国家 DE

  • 入库时间 2022-08-21 23:38:41

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