Minimum cycle slip airborne differential carrier phase GPS antenna
    1.
    发明授权
    Minimum cycle slip airborne differential carrier phase GPS antenna 失效
    最小循环滑移机载差分载波相位GPS天线

    公开(公告)号:US06844856B1

    公开(公告)日:2005-01-18

    申请号:US10615364

    申请日:2003-07-08

    CPC classification number: H01Q1/18 H01Q1/28

    Abstract: An antenna system is disclosed including a GPS antenna which is driven by an articulator in an opposite direction to aircraft roll. Aircraft roll is sensed by an onboard navigation system and translation module sends a signal to a processor which provides a drive signal to the articulator. As the aircraft rolls in one direction, the antenna is driven oppositely to maintain the vertical orientation of the antenna.

    Abstract translation: 公开了一种天线系统,其包括由与所述飞机辊相反的方向由咬合器驱动的GPS天线。 飞机辊由车载导航系统感测,并且翻译模块向​​处理器发送信号,该处理器向该发音器提供驱动信号。 当飞机在一个方向上滚动时,天线被相对地驱动以保持天线的垂直方向。

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