ILS-based altitude data generation system, device, and method
    1.
    发明授权
    ILS-based altitude data generation system, device, and method 有权
    基于ILS的高度数据生成系统,设备和方法

    公开(公告)号:US08498758B1

    公开(公告)日:2013-07-30

    申请号:US13685218

    申请日:2012-11-26

    CPC classification number: G01C5/005 G01C23/005

    Abstract: Present novel and non-trivial system, device, and method for generating altitude data and/or height data are disclosed. A processor receives navigation data from an external source such as a global positioning system (“GPS”); receives navigation data from multiple internal sources; receives object data representative of terrain or surface feature elevation; determines an instant measurement of aircraft altitude as a function of these inputs; and generates aircraft altitude data responsive to such determination. In an additional embodiment, the processor receives reference point data representative of the elevation of the stationary reference point (e.g., a landing threshold point); determines an instant measurement of aircraft height as a function of this input and the instant measurement of aircraft altitude; and generates aircraft height data responsive to such determination.

    Abstract translation: 公开了用于产生高度数据和/或高度数据的新颖和非平凡的系统,装置和方法。 处理器从诸如全球定位系统(“GPS”)的外部源接收导航数据; 从多个内部来源接收导航数据; 接收表示地形或表面特征高程的物体数据; 确定飞机高度的即时测量作为这些输入的函数; 并响应于这种确定生成飞机高度数据。 在另外的实施例中,处理器接收表示静止参考点的升高的参考点数据(例如,着陆阈值点); 确定飞机高度的即时测量作为该输入和飞机高度的即时测量的函数; 并响应于这种确定产生飞机高度数据。

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