Guided missile control systems
    1.
    发明授权
    Guided missile control systems 失效
    导弹控制系统

    公开(公告)号:US3883091A

    公开(公告)日:1975-05-13

    申请号:US60085856

    申请日:1956-07-30

    Inventor: SCHAEFER JACOB W

    CPC classification number: F41G7/30

    Abstract: 1. In an antiaircraft system, target tracking means for continuously establishing the position of a target aircraft in space, missile tracking means for similarly establishing the position of a missile, computing means responsive to position information from both said target and missile tracking means to produce control signals for said missile to insure interception of the target thereby and means for substituting the target tracking means for said missile tracking means as a source of missile position information for said computing means during the final phases of an engagement.

    Abstract translation: 1.在防空系统中,用于连续建立目标飞机在太空中的位置的目标跟踪装置,用于类似地建立导弹位置的导弹跟踪装置,响应于来自所述目标和导弹跟踪装置的位置信息产生的计算装置 用于所述导弹的控制信号以确保目标的截取,以及用于将所述导弹跟踪装置的目标跟踪装置替换为在接合的最后阶段期间所述计算装置的导弹位置信息源的装置。

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