首页> 外国专利> Electronic decoy technique for electromagnetically guided missiles - involves creating fictitious targets using several coherent transmission sources and program calculator

Electronic decoy technique for electromagnetically guided missiles - involves creating fictitious targets using several coherent transmission sources and program calculator

机译:电磁制导导弹的电子诱饵技术-涉及使用多个相干传输源和程序计算器创建虚拟目标

摘要

The electronic decoy technique is suitable for use with electromagnetic autopilots on missiles. It consists essentially in creating fictitious targets by means of several coherent transmission sources separated from each other but able to be positioned totally or partially inside the danger zone for the objective being defended. The practical implementation involves setting up two or more decoy stations which are geographically separated. Each station is provided with transmission and reception equipments which operate alternately. The stations are linked with a programming calculator unit which measures the frequencies and relative phases of the radiations received from the missiles at the stations. The frequency, phase, and power necessary are then computed and an appropriate decoy signal is transmitted which creates a fictitious target, shifted azimuthally. The calculator unit may measure also the differential Doppler effect.
机译:电子诱饵技术适用于导弹上的电磁自动驾驶仪。它的本质在于通过相互分离但可以完全或部分地放置在危险区域内的多个相干传输源来创建虚拟目标,以保护目标。实际的实现涉及建立两个或更多个在地理上分开的诱饵站。每个站都设有交替工作的发送和接收设备。这些电台与一个编程计算器单元链接,该计算器计算在该电台从导弹接收的辐射的频率和相对相位。然后计算所需的频率,相位和功率,并发送适当的诱饵信号,该信号会创建一个虚拟目标,并进行方位角偏移。计算器单元还可以测量差分多普勒效应。

著录项

  • 公开/公告号FR2328203B3

    专利类型

  • 公开/公告日1979-06-29

    原文格式PDF

  • 申请/专利权人 AERO ETUDES CONSEILS;

    申请/专利号FR19750031294

  • 发明设计人

    申请日1975-10-13

  • 分类号G01S7/38;F41H13/00;F41J9/12;

  • 国家 FR

  • 入库时间 2022-08-22 19:37:09

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