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Method for evaluating flight paths and flight path engine

机译:航迹评估方法及航迹引擎

摘要

A method of establishing a runway approach procedure for an aircraft at a selected runway, comprises, for obstacles in the final approach segment of the flightpath and having obstacle range values greater than the datum range, calculating a missed approach surface height at a projected intersection of a missed approach surface with a descending vertical error budget surface and a corresponding Distance to Height of Missed Approach Surface from the runway (DHMAS). For obstacles in the final approach segment and having obstacle range values less than the datum range, a missed approach surface height and a corresponding DHMAS are calculated using ascending climb gradient requirements. All DHMAS values are compared, and a controlling obstacle is determined as the obstacle having a greatest DHMAS. A decision altitude for the controlling obstacle is calculated, and the runway approach procedure is updated with the decision altitude. Relativistic metadata other obstacles can also be calculated and stored.
机译:一种用于在选定的跑道上为飞机建立跑道进场程序的方法,该方法包括:对于飞行路径的最终进场段中的障碍物,并且其障碍物范围值大于基准范围,计算在投影交点处错过的进场表面高度。具有下降的垂直误差预算面的错飞进场曲面和距跑道的相应错失进近曲面高度(DHMAS)。对于最终进近航段中的障碍物,且其障碍物范围值小于基准范围,则使用上升爬升坡度要求来计算错过的进近表面高度和相应的DHMAS。比较所有DHMAS值,并将控制障碍物确定为具有最大DHMAS的障碍物。计算出控制障碍物的决策高度,并用决策高度更新跑道进场程序。相对论元数据中的其他障碍也可以计算和存储。

著录项

  • 公开/公告号US10217370B2

    专利类型

  • 公开/公告日2019-02-26

    原文格式PDF

  • 申请/专利权人 ALASKA AIRLINES INC.;

    申请/专利号US201615346674

  • 发明设计人 MATTHEW B. KING;

    申请日2016-11-08

  • 分类号G08G5/02;G08G5/04;

  • 国家 US

  • 入库时间 2022-08-21 12:10:51

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