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Method and system for predicting air-to-surface target missile

机译:空对空目标导弹的预测方法和系统

摘要

A method and system for predicting a trajectory of an air-to-surface target missile is provided, including detecting a plurality of echo wave signals from the target missile through a plurality of sensors deployed at various locations relative to the target missile, extracting at least one range distance and at least one radial velocity, respectively, from the detected echo wave signals from the sensors by using a hybrid FSK/LFM unit, using a two-stage Kalman filter to filter the computed range distance and radial velocity to obtain a relative distance, a relative velocity and a relative acceleration, respectively, of the target missile, and finally applying trilateration on the relative distance, relative velocity and relative acceleration of the target missile from each two-stage Kalman filter to obtain a location, velocity and acceleration along the x, y, z directions.
机译:提供了一种用于预测空对面目标导弹的轨迹的方法和系统,包括:通过部署在相对于目标导弹的各个位置的多个传感器,检测来自目标导弹的多个回波信号,至少提取通过使用混合FSK / LFM单元,使用两级卡尔曼滤波器对计算出的距离和径向速度进行滤波,从传感器检测到的回波信号中分别获得一个距离距离和至少一个径向速度目标导弹的距离,相对速度和相对加速度,最后对来自每个两级卡尔曼滤波器的目标导弹的相对距离,相对速度和相对加速度进行三边测量,以获得位置,速度和加速度沿x,y,z方向。

著录项

  • 公开/公告号US2009085793A1

    专利类型

  • 公开/公告日2009-04-02

    原文格式PDF

  • 申请/专利权人 PO-JEN TU;JEAN-FU KIANG;

    申请/专利号US20070003090

  • 发明设计人 PO-JEN TU;JEAN-FU KIANG;

    申请日2007-12-20

  • 分类号G01S13/58;

  • 国家 US

  • 入库时间 2022-08-21 19:32:55

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