首页> 外国专利> Aircraft i.e. airplane, and shifted runway distance determining method, involves combining heights and alpha angle to obtain distance from aircraft to elevation beacon, and utilizing distance to obtain location point of aircraft in runway

Aircraft i.e. airplane, and shifted runway distance determining method, involves combining heights and alpha angle to obtain distance from aircraft to elevation beacon, and utilizing distance to obtain location point of aircraft in runway

机译:飞机,即飞机,以及改变跑道的距离确定方法,包括将高度和α角相结合以获得从飞机到仰角信标的距离,并利用该距离来获得飞机在跑道上的位置点

摘要

The method involves determining a height (Ho) at which aircraft i.e. airplane (1), is found, where the height is determined with respect to a point of a shifted track and measured by a radio altimeter (2) of the aircraft. An elevation angle is determined in a microwave landing system mode by using elevation beacon information provided by an elevation beacon of a main runway. Two heights and alpha angle measured by the beacon are combined to obtain a distance from the aircraft to the beacon. The distance is utilized to obtain a location point of the aircraft in a shifted reference runway.
机译:该方法包括确定找到飞机即飞机(1)的高度(Ho),其中该高度是相对于平移轨迹的点确定的,并且由飞机的无线电高度仪(2)测量。通过使用主跑道的高程信标提供的高程信标信息,在微波着陆系统模式下确定高程角。将信标测量的两个高度和Alpha角度组合起来,以获得从飞机到信标的距离。该距离用于获得飞机在平移的参考跑道中的位置点。

著录项

  • 公开/公告号FR2939948A1

    专利类型

  • 公开/公告日2010-06-18

    原文格式PDF

  • 申请/专利权人 THALES;

    申请/专利号FR20080007062

  • 发明设计人 BOULAY THIERRY;

    申请日2008-12-16

  • 分类号G08G5/02;B64D45/04;

  • 国家 FR

  • 入库时间 2022-08-21 18:26:39

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