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A method and device for supporting the inertial navigation of a missile heading autonomously to a remote target.

机译:一种用于支持自主地飞向远程目标的导弹的惯性导航的方法和设备。

摘要

P A method for supporting the inertial navigation of a missile heading autonomously to a distant target using a sensor producing images, grasping the terrain overflown, looking at a finite angle laterally to the aiming direction, delivering field data from which, in comparison with known terrain data, a position of the missile is derived, which position in turn is compared to the position determined by the inertial navigation, and the inertial navigation system is corrected in proportion to this comparison. BR/ A method characterized in that images of the terrain overflown to produce a sequence of images are continuously taken from different positions of the missile by the sensor, producing images, during the movement of the missile over the terrain , these images being stored electronically. / P
机译:

一种方法,该方法使用产生图像的传感器来支持导弹的惯性自主导航,该传感器产生图像,掌握溢出的地形,横向于瞄准方向以有限角度注视,并提供野外数据,与在已知的地形数据中,得出导弹的位置,该位置又与惯性导航确定的位置进行比较,并且惯性导航系统与该比较成比例地进行校正。
一种方法,其特征在于,传感器连续从导弹的不同位置拍摄溢出来产生一系列图像的地形图像,从而在导弹在地形上运动期间产生图像,这些图像被存储电子地。

著录项

  • 公开/公告号FR2719920A1

    专利类型

  • 公开/公告日1995-11-17

    原文格式PDF

  • 申请/专利权人 BODENSEEWERK GERATETECHNIK GMBH;

    申请/专利号FR19950005188

  • 发明设计人 KLAUS HESSE;

    申请日1995-04-26

  • 分类号G05D1/12;G06F19/00;H04N7/18;

  • 国家 FR

  • 入库时间 2022-08-22 03:40:40

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