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Optical huaibare - da induction missile system

机译:optical坏bare - 大induction missile system

摘要

A fiber optic radar guided missile system 10 is disclosed which includes a radar receiver 12 disposed in a missile for receiving radar reflections and providing a first optical signal in response thereto. An optical receiver 14 is disposed at a launcher for receiving the first optical signal and for providing a set of electrical signals in response thereto. A fiber optic link 32 is connected between the missile and the launcher for communicating the first optical signal from the radar receiver 12 to the optical receiver 14. In a specific embodiment, the invention 10 includes a first system 12 disposed in a missile for receiving radar reflections which includes only an antenna 16 for receiving radar reflections, a radar seeker 18 for providing a first electrical in response to the received radar reflections, and a first fiber optic transmitter 26 for converting the first electrical signal into a first optical signal. An optical receiver 14 is located at a launcher for receiving the first optical signal and for providing a set of electrical signals in response thereto. The optical receiver 14 at the launcher includes a first fiber optic receiver 48 for converting the first optical signal into a second electrical signal and a signal processor 56 for processing the second electrical signal and providing radar output data. A fiber optic link 32 is provided for communicating the first optical signal from the radar receiver 12 to the optical receiver 114 at the launcher and missile commands from the launcher to the missile.
机译:公开了一种光纤雷达制导导弹系统10,其包括布置在导弹中的雷达接收器12,用于接收雷达反射并响应于此提供第一光信号。光接收器14布置在发射器处,用于接收第一光信号并响应于此提供一组电信号。光纤链路32连接在导弹和发射器之间,用于将第一光信号从雷达接收器12传送到光接收器14。在特定实施例中,本发明10包括设置在导弹中的用于接收雷达的第一系统12。仅包括用于接收雷达反射的天线16,用于响应于所接收的雷达反射而提供第一电的雷达导引器18,以及用于将第一电信号转换为第一光信号的第一光纤发射器26的反射。光接收器14位于发射器处,用于接收第一光信号并响应于此提供一组电信号。在发射器处的光接收器14包括用于将第一光信号转换成第二电信号的第一光纤接收器48以及用于处理第二电信号并提供雷达输出数据的信号处理器56。提供了光纤链路32,用于在发射器处将来自雷达接收器12的第一光信号传送到光接收器114,以及将来自发射器的导弹命令传送到导弹。

著录项

  • 公开/公告号JPH03502834A

    专利类型

  • 公开/公告日1991-06-27

    原文格式PDF

  • 申请/专利权人

    申请/专利号JP19890500086

  • 发明设计人

    申请日1989-11-06

  • 分类号F41G7/22;F41G7/32;G01S13/87;G01S13/88;

  • 国家 JP

  • 入库时间 2022-08-22 06:02:07

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