Method for graphic representation of the relative position of the sky and the earth in an onboard display system for aircraft

Patent metadata

Field	Value
Publication number	US-10464688-B2
Application number	US-201615394777-A
Country	US
Kind code	B2
Filing date	Dec 29, 2016
Priority date	Dec 29, 2015
Publication date	Nov 5, 2019
Grant date	Nov 5, 2019

Abstract

The general field of the invention is that of the methods for graphic representation of the relative position of the sky and of the earth in an onboard display system for aircraft, said graphic representation being displayed on a display screen comprising piloting and navigation information superimposed on a three-dimensional synthetic representation of the outside landscape. Said graphic representation is displayed only when the attitude of the aircraft is unusual, an unusual attitude corresponding to a roll value or to a pitch value located outside of a first range of nominal values. It comprises two disc segments of identical form, that are opaque and of different colour, situated symmetrically on a circle concentric to that bearing the roll scale, the straight-line segments of the two disc segments being parallel to the line representing the zero longitudinal trim indicator, the rotation of the two disc segments being slaved to the rotation of said zero longitudinal trim indicator.

First claim

What is claimed is:

1. A method comprising:
displaying a graphic representation on a display screen of an onboard display system for an aircraft, wherein:
in an aircraft attitude that is not unusual, the graphic representation consists of piloting and navigation information superimposed on a three-dimensional synthetic representation of the outside landscape or on a real image of the outside landscape; and
in an unusual aircraft attitude, the graphic representation consists of:
piloting and navigation information superimposed on a three-dimensional synthetic representation of the outside landscape or on a real image of the outside landscape, and
symbols showing the relative positions of sky and earth, the symbols comprising two elongate forms, one representing the sky and the other representing the earth, the rotation of the two elongate forms being slaved to the rotation of a line representing the zero longitudinal trim indicator;

wherein an unusual aircraft attitude corresponds to a roll value or to a pitch value located outside a first range of nominal values.

2. The graphic representation method according to claim 1 , wherein the graphic representation in an unusual aircraft attitude comprises at least two different representation modes, a first representation mode corresponding to roll or pitch values located outside of a first range of nominal values, and a second representation mode corresponding to roll or pitch values located outside of a second range of values, higher than the first range of nominal values.

3. The graphic representation method according to claim 2 , wherein the first representation mode comprises two identical elongate forms, that are opaque and of different colour, situated symmetrically on a circle concentric with the circle bearing the roll scale.

4. The graphic representation method according to claim 3 , wherein in the first representation mode the two elongate forms comprise two disc segments of identical form, that are opaque and of different colour, each disc segment being limited by a circular arc and a straight-line segment joining the ends of said circular arc, the two disc segments being situated symmetrically on a circle concentric with the circle bearing the roll scale, the straight-line segments of the two disc segments being parallel to the line representing the zero longitudinal trim indicator.

5. The graphic representation method according to claim 4 , wherein the width of the disc segment lies between 15% and 25% of the length of the straight-line segment.

6. The graphic representation method according to claim 4 , wherein the second representation mode comprises the two preceding disc segments and two areas of identical form that are semi-transparent and of different colours, the two areas being situated symmetrically relative to the line representing the zero longitudinal trim indicator on a circle concentric to that bearing the roll scale, the first area extending between the straight-line segment of the first disc segment and the line representing the zero longitudinal trim indicator, without ever leaving the area defined by the straight-line segments of the first and of the second disc segments, the second area extending between the straight-line segment of the second disc segment and the line representing the zero longitudinal trim indicator, without ever leaving the area defined by the straight-line segments of the first and of the second disc segments.

7. The graphic representation method according to claim 1 , wherein, when the roll value is located outside of a third range of values, lower than the first range of nominal values, the roll scale is widened, continually or discretely, so as to increase with the roll value.

8. The graphic representation method according to claim 2 , wherein the first range of roll values lies between −45 degrees and +45 degrees, the second range of roll values lies between −50 degrees and +50 degrees, the first range of pitch values lies between −12.5 degrees and +15 degrees, the second range of pitch values lies between −25 degrees and +25 degrees.

9. The graphic representation method according to claim 2 , wherein the display device comprises a function to avoid untimely changes from the first representation mode to the second representation mode and vice versa.

10. The graphic representation method according to claim 1 , wherein the display device comprises a real image of the outside landscape superimposed on the synthetic view of the outside landscape.

11. The graphic representation method according to claim 1 , wherein the display device is one of the aircraft instrument panel screens.

12. The graphic representation method according to claim 1 , wherein the display device is a so-called “head up” display device comprising an optical element superimposing the synthetic image, the real image, or both the synthetic image and the real image, on the outside landscape.

Assignees

• Thales Sa

Inventors

• Monvoisin Emmanuel
• Mariani Pierre
• Frestel Norbert
• Lux Johanna

Classifications

• G06T19/006

  Mixed reality (object pose determination, tracking or camera calibration for mixed reality G06T7/00) · CPC title

• B64D43/00 Primary

  Arrangements or adaptations of instruments · CPC title

• G01C23/00 Primary

  Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration · CPC title

• G06T2200/04

  involving 3D image data · CPC title

• G06T2215/16

  Using real world measurements to influence rendering · CPC title