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LONG RANGE MISSILE GUIDANCE SYSTEM

机译:远程导弹制导系统

摘要

PROBLEM TO BE SOLVED: To solve a problem in a conventional long range missile guidance system, wherein it is difficult to make a direct data link between a communication device on the ground and the flying object due to constraint of a communication distance and the like, it is difficult to accurately recognize a meeting state with a target, and it is difficult to determine whether or not a next flying object is required to be launched.;SOLUTION: A long range missile guidance system is comprised of a flying object of a first launch, a flying object of a next launch, and a guidance control unit for guiding the flying object of the first launch and the flying object of the next launch toward a target, and the flying of object of the first launch has an imaging means for imaging a meeting state of meeting of a portion of the separated flying object and the target, and a transmission unit for transmitting image data taken by the imaging means to a relay which is similarly separated from the flying object and staying in the air, and upon receiving the image data, the relay transmits it to the guide control unit, and the guidance control unit determines whether to launch a next flying object based on the image data.;COPYRIGHT: (C)2014,JPO&INPIT
机译:要解决的问题:为了解决传统的远程导弹制导系统中的问题,在该系统中,由于通信距离等的限制,很难在地面上的通信设备与飞行物体之间进行直接数据链接,难以准确识别与目标的会合状态,并且难以确定是否需要发射下一个飞行物。解决方案:远程导弹制导系统由第一个飞行物组成发射,下一次发射的飞行物,以及用于将第一次发射的飞行物和下一次发射的飞行物朝向目标引导的引导控制单元,并且第一次发射的物体的飞行具有用于成像的成像装置。成像分离的飞行物体和目标的一部分的相遇的相遇状态,以及传输单元,用于将由成像装置获取的图像数据传输到与第飞行物体并停留在空中,并在接收到图像数据后,中继将其传输到引导控制单元,引导控制单元根据图像数据确定是否发射下一个飞行物体。 )2014,JPO&INPIT

著录项

  • 公开/公告号JP2013210122A

    专利类型

  • 公开/公告日2013-10-10

    原文格式PDF

  • 申请/专利权人 MITSUBISHI ELECTRIC CORP;

    申请/专利号JP20120079831

  • 发明设计人 SHIBATA TETSUTO;

    申请日2012-03-30

  • 分类号F42B15/01;G01S13/88;

  • 国家 JP

  • 入库时间 2022-08-21 17:01:24

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