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Method and device for determining a final approach path of an aircraft for a non-precision approach for the purpose of landing the aircraft

机译:用于以降落飞机为目的的非精确进场确定飞机最终进场路径的方法和装置

摘要

The method provides for determining an approach mode which has been selected by the pilot of the aircraft from among a plurality of predetermined approach modes, for selecting a characteristic segment (6) of an arrival path which relates to the selected approach mode thus determined, for determining the orientation of the projection on the ground of the said characteristic segment (6) with respect to the center line of the said runway (5) and, depending on this orientation, for determining an anchoring point of the said final approach path, the orientation (&agr;) in a horizontal plane of the said final approach path and the slope (&bgr;) of the said final approach path.
机译:该方法提供以下步骤:确定已经由飞机的飞行员从多个预定的进近模式中选择的进近模式,以选择与飞行器相关的到达路径的特征段( 6 )。这样确定的选择进近模式,用于确定所述特征段( 6 )上的投影相对于所述跑道( 5 )的中心线的方向),并根据该方向确定上述最终进场路径的锚点,上述最终进场路径的水平面内的方向(&agr)和上述最终进场路径的斜率(&bgr)。

著录项

  • 公开/公告号US2004183698A1

    专利类型

  • 公开/公告日2004-09-23

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号US20040775230

  • 发明设计人 OLIVIER COUSSAT;PATRICE ROUQUETTE;

    申请日2004-02-11

  • 分类号G01C21/00;

  • 国家 US

  • 入库时间 2022-08-21 23:22:10

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