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Method of piloting and/or guiding a projectile and piloting and/or guiding device implementing such a method

机译:引导和/或引导弹丸的方法以及实施这种方法的引导和/或引导装置

摘要

The method involves implementing a target detector that allows to locate a target (13) in a reference location related to a projectile (1). Components of a line of sight vector between the target and the projectile are deduced using aiming algorithms. Three components of a terrestrial magnetic field are measured in the reference location. Rotation speed of the projectile around roll, pitch and yaw axes is determined by combining two pseudo-gyrometric evaluations that are based on vector and magnetic field components. An independent claim is also included for a device for terminal piloting and/or guiding of a projectile toward a target.
机译:该方法包括实现目标检测器,该目标检测器允许将目标(13)定位在与弹丸(1)有关的参考位置中。使用瞄准算法推导目标和弹丸之间的视线矢量的分量。在参考位置测量了地磁场的三个分量。弹丸围绕侧倾,俯仰和偏航轴的旋转速度是通过组合两个基于矢量和磁场分量的伪陀螺评估来确定的。还包括一种独立权利要求,其用于将弹丸终端引导和/或引导向目标的设备。

著录项

  • 公开/公告号EP1840692A1

    专利类型

  • 公开/公告日2007-10-03

    原文格式PDF

  • 申请/专利权人 NEXTER MUNITIONS;

    申请/专利号EP20070290330

  • 发明设计人 BREDY THIERRY;

    申请日2007-03-19

  • 分类号G05D1/12;

  • 国家 EP

  • 入库时间 2022-08-21 20:38:11

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