公开(公告)号：US20140148980A1

公开(公告)日：2014-05-29

申请号：US14089535

申请日：2013-11-25

Applicant: DASSAULT AVIATION

Inventor： Nicolas LE CORRE ,  Sébastien LEPAGE ,  Alain BOUCHER

IPC: G08G5/00

CPC classification number: G08G5/00 ,  G05D1/0083 ,  G05D1/0676 ,  G08G5/025

Abstract: The method according to the invention comprise the following steps, dynamic measurement of the current geographical position of the aircraft, and its current ground speed, calculation of a first length representative of a flight phase of the aircraft, and calculation of a second length representative of a ground phase of the aircraft, calculation of the position of the stop point based on the first length, the second length and the current geographical position. The calculation of the first length comprises a phase for dynamically estimating a distance traveled by the aircraft during at least part of a flare phase of the aircraft.

Abstract translation: 根据本发明的方法包括以下步骤：飞行器当前地理位置的动态测量及其当前地面速度，代表飞行器飞行阶段的第一长度的计算，以及代表飞行器的第二长度的计算 飞机的地面相位，基于第一长度，第二长度和当前地理位置计算停止点的位置。 第一长度的计算包括一个阶段，用于动态地估计飞机在至少部分飞机的火炬阶段期间行驶的距离。