SPACE-BASED LEVER ARM CORRECTION IN NAVIGATIONAL SYSTEMS EMPLOYING SPOT BEAMS
    1.
    发明申请
    SPACE-BASED LEVER ARM CORRECTION IN NAVIGATIONAL SYSTEMS EMPLOYING SPOT BEAMS 有权
    采用SPOT BEAMS的导航系统中的基于空间的双臂校正

    公开(公告)号:US20070080859A1

    公开(公告)日:2007-04-12

    申请号:US11247641

    申请日:2005-10-10

    IPC分类号: H04B7/185

    摘要: A method and apparatus for estimating a lever arm correction between the wide beam antenna and the spot beam antenna in a navigational satellite system is disclosed. A prescribed satellite maneuver is used to increase the accuracy of the predicted satellite attitude in determining the lever arm, and lever arm corrections are provided to navigation receivers using curve fit coefficients to permit long range estimates and to minimize data transmission requirements.

    摘要翻译: 公开了一种用于在导航卫星系统中估计宽波束天线和点波束天线之间的杠杆臂校正的方法和装置。 使用规定的卫星机动来增加在确定杠杆臂时所预测的卫星姿态的准确度,并且使用曲线拟合系数将导轨接收器提供杠杆臂校正,以允许长距离估计并且最小化数据传输要求。

    CONTROL SEGMENT-BASED LEVER-ARM CORRECTION VIA CURVE FITTING FOR HIGH ACCURACY NAVIGATION
    3.
    发明申请
    CONTROL SEGMENT-BASED LEVER-ARM CORRECTION VIA CURVE FITTING FOR HIGH ACCURACY NAVIGATION 有权
    通过用于高精度导航的曲线拟合来控制基于分段的双向校正

    公开(公告)号:US20070080858A1

    公开(公告)日:2007-04-12

    申请号:US11247640

    申请日:2005-10-10

    IPC分类号: H04B7/185

    CPC分类号: B64G1/1014 B64G1/24

    摘要: A method and apparatus for estimating a lever arm correction between the wide beam antenna and the spot beam antenna in a navigational satellite system is disclosed. A prescribed satellite maneuver is used to increase the accuracy of the predicted satellite attitude in determining the lever arm, and lever arm corrections are provided from a ground segment to navigation receivers using curve fit coefficients to permit long range estimates and to minimize data transmission requirements.

    摘要翻译: 公开了一种用于在导航卫星系统中估计宽波束天线和点波束天线之间的杠杆臂校正的方法和装置。 在确定杠杆臂时,使用规定的卫星操作来提高预测的卫星姿态的精度,并且使用曲线拟合系数从地面段向导航接收机提供杠杆臂校正,以允许长距离估计并且最小化数据传输要求。