首页> 外国专利> Method and device for determining a final approach path for aircraft for a non-precision approach during landing of aircraft

Method and device for determining a final approach path for aircraft for a non-precision approach during landing of aircraft

机译:用于确定飞机着陆过程中非精确进近的飞机最终进近路径的方法和装置

摘要

The process involves determining a mode of approach to select a characteristic segment (6) of a trajectory of arrival. The direction of the projection to the ground of the segment with respect to axis of a runway (5) is determined. An anchorage point of a final approach axis and direction in a horizontal plane from the final axis is determined based on the projection direction to obtain the slope of the final axis. An independent claim is also included for an aircraft including a device for determining an approach axis of an aircraft for a non-precision approach in view of a landing of the aircraft on a runway.
机译:该过程包括确定接近模式以选择到达轨迹的特征段(6)。确定相对于跑道(5)轴线的投影到分段的地面的方向。根据投影方向确定最终进近轴的锚固点和在距最终轴的水平面中的方向,以获得最终轴的斜率。还包括一种飞机的独立权利要求,该飞机包括一种装置,该装置用于根据飞机在跑道上的着陆来确定用于非精确进近的飞机进近轴。

著录项

  • 公开/公告号EP1459978B1

    专利类型

  • 公开/公告日2006-05-17

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号EP20040290356

  • 发明设计人 COUSSAT OLIVIER;ROUQUETTE PATRICE;

    申请日2004-02-11

  • 分类号B64D45/04;G05D1/06;

  • 国家 EP

  • 入库时间 2022-08-21 21:30:15

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号