MISSILE SYSTEM WITH NAVIGATION CAPABILITY BASED ON IMAGE PROCESSING
    1.
    发明公开
    MISSILE SYSTEM WITH NAVIGATION CAPABILITY BASED ON IMAGE PROCESSING 审中-公开
    UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG UNG

    公开(公告)号:EP3033584A1

    公开(公告)日:2016-06-22

    申请号:EP14835900.3

    申请日:2014-06-15

    IPC分类号: F42B15/01 G05D1/00

    摘要: The present invention relates to electro-optic guided missile systems and, in particular, it concerns systems and methods providing enhanced navigation capabilities based on ego-motion processing of seeker images. The missile system comprising: a missile;a seeker located at a nose portion of said missile, said seeker comprising an electro-optic imaging sensor; and a control arrangement for steering the missile along a flight path to a target, characterized in that the missile system further comprises: a navigation subsystem receiving images from said imaging sensor, said navigation subsystem being configured to: co-process a plurality of said images from said imaging sensor to derive ego-motion of said missile relative to a region viewed by said imaging sensor;derive from said ego-motion a calculated target direction from said missile to a target.

    摘要翻译: 本发明涉及电光导弹系统,特别涉及提供基于探测器图像的自动运动处理的增强导航能力的系统和方法。 导弹系统包括:导弹; 位于所述导弹的鼻部的探测器,所述探测器包括电光成像传感器; 以及用于将导弹沿着飞行路径转向目标的控制装置,其特征在于,所述导弹系统还包括:导航子系统,从所述成像传感器接收图像,所述导航子系统被配置为:协同处理多个所述图像 从所述成像传感器导出所述导弹相对于由所述成像传感器观察的区域的自身运动; 从所述自我运动导出从所述导弹到目标的计算目标方向。