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    • 1. 发明授权
    • Method and a device for assisting the piloting of an aircraft during an approach phase
    • 方法和用于在接近阶段协助飞机驾驶的装置
    • US07522977B2
    • 2009-04-21
    • US11394200
    • 2006-03-31
    • Vincent FoucartEric AlbertPatrice Gonzalez
    • Vincent FoucartEric AlbertPatrice Gonzalez
    • G05D1/10G05D1/02
    • G01C23/005
    • A method for landing an aircraft includes determining the aircraft's deviation from its approach path so as to define a first point of the aircraft's heading. A first straight line passing through the first point and through a second point defining the ground orientation of the approach path is displayed, by a head-up display, on a horizon line with a heading scale. The first straight line represents a ground plot of the approach path. A first assistance gate is displayed such that the first straight line passes through the first assistance gate when the aircraft is aligned on the approach path. A second straight line, parallel with the horizon line and passing through the first point, is displayed and represents a plot on the ground of the origin of the approach path. A second assistance gate is displayed under the horizon line and represents the slope of the approach path.
    • 用于着陆飞行器的方法包括确定飞行器与其进近路径的偏差,以便确定飞机的航向的第一点。 通过第一点并且通过限定接近路径的接地方向的第二点的第一直线通过平视显示器在具有标题的水平线上显示。 第一条直线表示接近路径的地面图。 显示第一辅助闸门,使得当飞行器在接近路径上对准时,第一直线穿过第一辅助闸门。 显示与水平线平行并穿过第一点的第二条直线,并表示接近路径原点的基础上的曲线。 第二辅助门显示在地平线下方,表示进场路径的斜率。
    • 2. 发明申请
    • Method and a device for assisting the piloting of an aircraft during an approach phase
    • 方法和用于在接近阶段协助飞机驾驶的装置
    • US20060224281A1
    • 2006-10-05
    • US11394200
    • 2006-03-31
    • Vincent FoucartEric AlbertPatrice Gonzalez
    • Vincent FoucartEric AlbertPatrice Gonzalez
    • G01C23/00G06F17/00
    • G01C23/005
    • A method and a device for assisting the piloting of an aircraft during an approach phase. The piloting aid device comprises a head up display device for displaying, on a display screen (12), a first straight line (13) representing in a true manner the plot on the ground of a first approach path, a first assistance point (25) such that the first straight line (13) passes through this first assistance point (25) when the aircraft is aligned on the first approach path, a second straight line (21) parallel with the horizon (14) and representing in a true manner the plot on the ground of the ending of a second approach path, a second assistance point (23) placed under the horizon line (14) and representing the slop of the second approach path, and a synthetic runway (22) representing in a true manner the plot on the ground of the sides of a landing runway where said first and second approach paths end.
    • 一种在接近阶段协助飞机驾驶的方法和装置。 引导辅助装置包括头部显示装置,用于在显示屏幕(12)上显示第一直线(13),该第一直线(13)以真实方式表示在第一接近路径的基础上的绘图,第一辅助点(25) ),使得当飞机在第一接近路径上对准时,第一直线(13)穿过该第一辅助点(25),平行于地平线(14)的第二直线(21)并且以真实的方式表示 基于第二进场路径的结束的地块,放置在地平线(14)下方并表示第二进场路径的坡道的第二辅助点(23)以及表示为真实的合成跑道(22) 方式是在所述第一和第二进场路径结束的着陆跑道的侧面的地面上。