公开(公告)号：US09073644B2

公开(公告)日：2015-07-07

申请号：US14279956

申请日：2014-05-16

Applicant: AIRBUS OPERATIONS (S.A.S.)

Inventor： Virginie Le Gall ,  Alexandre Buisson ,  Pierre-Xavier Catinat ,  Valentin Vincent

IPC: G05D1/06 ,  B64D45/04

CPC classification number: B64D45/04 ,  G05D1/06 ,  G05D1/0676

Abstract: Method and device for automatically determining an optimized approach profile for an aircraft. The device provides for a flexible configuration change speed which is not limited to the standard single predetermined configuration change speed in order to prevent segments which are not authorized, in particular segments which are too steep, the following configuration (Ci+1) being able to be maintained during a configuration change in an upstream direction until the corresponding speed profile reaches a maximum speed.

Abstract translation: 用于自动确定飞行器优化的进场曲线的方法和装置。 该装置提供了灵活的配置改变速度，其不限于标准的单个预定配置改变速度，以便防止未授权的段，特别是太陡峭的段，以下配置（Ci + 1）能够 在上游方向的配置更改期间维持，直到相应的速度曲线达到最大速度。

公开(公告)号：US09378645B2

公开(公告)日：2016-06-28

申请号：US14549745

申请日：2014-11-21

Applicant: Airbus Operations S.A.S.

Inventor： Jaouad Berrajaa ,  Virginie Le Gall ,  Alexandre Buisson

IPC: G05G5/02 ,  G08G5/02 ,  G05D1/00 ,  G05D1/06 ,  G08G5/00 ,  G01C23/00

CPC classification number: G08G5/02 ,  G01C23/00 ,  G05D1/00 ,  G05D1/0005 ,  G05D1/0676 ,  G08G5/0034 ,  G08G5/025

Abstract: This relates to a method and device for constructing a vertical profile for an aircraft descent and/or approach. The construction device comprises a data-capture unit configured to provide, for at least one of a plurality of parameters, a value relating to a user strategy. A construction unit is configured to automatically construct a vertical profile for an aircraft descent and/or approach, using the value thus provided.

Abstract translation: 这涉及一种用于构建飞行器下降和/或方法的垂直剖面的方法和装置。 施工设备包括数据捕获单元，其被配置为针对多个参数中的至少一个提供与用户策略相关的值。 构造单元被配置为使用由此提供的值来自动构造用于飞机下降和/或接近的垂直轮廓。

公开(公告)号：US09142135B2

公开(公告)日：2015-09-22

申请号：US14279418

申请日：2014-05-16

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Virginie Le Gall ,  Alexandre Buisson ,  Pierre-Xavier Catinat ,  Valentin Vincent

IPC: G08G5/02 ,  B64C19/00 ,  G05D1/06

CPC classification number: G08G5/02 ,  B64C19/00 ,  G05D1/0676

Abstract: A method and device for automatically determining an optimized approach and/or descent profile for an aircraft are provided. The device comprises means for optimizing an approach and/or descent profile of an aircraft avoiding long and steep geometric segments, the device to this end inserting an idle segment, if it satisfies the restrictions, in the profile relating to the descent phase and/or to the approach phase, wherein said idle segment can be followed by a geometric segment.

Abstract translation: 提供一种用于自动确定飞行器的优化进近和/或下降轮廓的方法和装置。 该装置包括用于优化飞行器的接近和/或下降轮廓以避免长而陡峭的几何段的装置，该装置为此在与下降相和/或下降相关的轮廓中满足限制时插入空闲段 到接近阶段，其中所述空闲段可以跟随几何段。