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METHOD AND SYSTEM FOR DETERMINING EFFECTIVE APPROACH ANGLE AND PREDICTING AIRCRAFT LANDING DISTANCE

机译:确定有效接近角度和预测飞机着陆距离的方法和系统

摘要

A method of predicting a parameter for an aircraft includes detecting an actual approach profile of the aircraft. The actual approach profile includes an actual approach angle. The method also includes comparing, by a processor, the actual approach profile to a predetermined approach profile to determine a difference between the actual and predetermined approach profiles. The predetermined approach profile includes a predetermined approach angle. The method further includes determining, by the processor, an effective approach angle by combining the actual approach angle and the predetermined approach angle according to a factor that varies based on the difference between the actual and predetermined approach profiles. Moreover, the method includes determining, by the processor, the predicted parameter based on the effective approach angle.
机译:一种预测飞机参数的方法包括检测飞机的实际方法轮廓。实际方法轮廓包括实际接近角度。该方法还包括将实际方法分布与预定方法分布进行比较,以确定实际和预定的方法轮廓之间的差异。预定的方法轮廓包括预定的接近角度。该方法还包括通过根据基于实际和预定方法轮廓之间的差异变化的因子来通过组合实际接近角度和预定接近角度来确定有效接近角度。此外,该方法包括通过处理器基于有效接近角度来确定预测参数。

著录项

  • 公开/公告号EP3306593B1

    专利类型

  • 公开/公告日2021-04-14

    原文格式PDF

  • 申请/专利权人

    申请/专利号EP20170194654

  • 发明设计人 HE GANG;JOHNSON STEVE;

    申请日2017-10-03

  • 分类号G08G5;G08G5/02;G05D1/06;

  • 国家 EP

  • 入库时间 2022-08-24 18:13:33

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