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MISSILE GUIDANCE SYSTEM, MISSILE, MISSILE GUIDING METHOD AND GUIDING CONTROL PROGRAM

机译:导弹制导系统,导弹,导弹制导方法和制导控制程序

摘要

PROBLEM TO BE SOLVED: To provide a missile guidance system for improving guidance accuracy for a missile, a missile, a missile guiding method and a program thereof.SOLUTION: A missile guidance system comprises a missile and a command device. The missile includes an image sensor, an image analysis unit, a transmittance unit, a receiving unit and a guidance control unit. The image sensor takes an image 110 and outputs it as a taken image 110. The image analysis unit extracts a lock-on candidate from the taken image 110 with the image sensor. The transmittance unit transmits target identification information for identifying the lock-on candidate on the taken image 110 and the taken image 110 to the command device. The receiving unit receives set information from the command device. The guidance control unit, when it receives the received set information, sets a lock-on target 400 of the missile on the basis of the set information and performs an image guidance of the missile in respect to the lock-on target 400.SELECTED DRAWING: Figure 9A
机译:解决的问题:提供一种用于提高导弹的制导精度的导弹制导系统,导弹,导弹的制导方法及其程序。解决方案:导弹制导系统包括导弹和指挥装置。该导弹包括图像传感器,图像分析单元,透射单元,接收单元和制导控制单元。图像传感器拍摄图像110并将其作为拍摄图像110输出。图像分析单元利用图像传感器从拍摄图像110中提取锁定候选。透射单元将用于识别拍摄图像110和拍摄图像110上的锁定候选的目标识别信息发送到命令装置。接收单元从命令设备接收设置信息。制导控制单元在接收到所接收的设置信息时,基于设置信息设置导弹的锁定目标400,并相对于锁定目标400执行导弹的图像引导。 :图9A

著录项

  • 公开/公告号JP2016161194A

    专利类型

  • 公开/公告日2016-09-05

    原文格式PDF

  • 申请/专利权人 MITSUBISHI HEAVY IND LTD;

    申请/专利号JP20150039323

  • 发明设计人 KOMUKAI JUN;

    申请日2015-02-27

  • 分类号F41G7/22;

  • 国家 JP

  • 入库时间 2022-08-21 14:46:48

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