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Method and system of controlling a flight of an aircraft subjected to a required time of arrival constraint

机译:控制受到所需到达时间限制的飞机飞行的方法和系统

摘要

Example systems and methods for controlling a flight of an aircraft subjected to a required time of arrival constraint at a target waypoint and to an additional flight criterion are disclosed herein. An example method includes calculating combinations of cruise speed and descent speed for estimated times of arrival (ETAs) at the target waypoint and determining a subset of the combinations that introduce substantially a same amount of time change in the ETA when changing the corresponding cruise speed to a cruise speed limit as when changing the corresponding descent speed to a descent speed limit. The example method also includes selecting a combination of the subset of the combinations having an ETA substantially equal to the RTA and modifying at least one of a cruise speed or a descent speed of the aircraft based on the selected combination.
机译:本文公开了用于控制飞机的飞行的示例性系统和方法,该飞机在目标航路点受到所需的到达时间限制并受到附加的飞行标准的约束。一种示例方法包括:计算到达目标航路点的估计到达时间(ETA)的巡航速度和下降速度的组合,并确定组合的子集,当将相应的巡航速度更改为ETA时,在ETA中引入基本上相同的时间变化量巡航速度限制,例如将相应的下降速度更改为下降速度限制时。该示例方法还包括:选择具有基本上等于RTA的ETA的组合子集的组合,并基于所选择的组合来修改飞机的巡航速度或下降速度中的至少一个。

著录项

  • 公开/公告号US10049585B2

    专利类型

  • 公开/公告日2018-08-14

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US201615192238

  • 发明设计人 DAVID GARRIDO LÓPEZ;

    申请日2016-06-24

  • 分类号G08G5;G05D1/10;G05D1/06;G06F19;

  • 国家 US

  • 入库时间 2022-08-21 13:05:20

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