Method for three-dimensional graphic representation of a landing runway on an aircraft display device

Patent metadata

Field	Value
Publication number	US-10232952-B2
Application number	US-201615394774-A
Country	US
Kind code	B2
Filing date	Dec 29, 2016
Priority date	Dec 29, 2015
Publication date	Mar 19, 2019
Grant date	Mar 19, 2019

Abstract

The general field of the invention is that of the methods for three-dimensional graphic representation of at least one landing runway on a display device of an onboard display system for aircraft, said graphic representation being displayed in a synthetic of an outside landscape, said runway comprising a coloured rectangular form, an outline surrounding said form and markings the position of the aircraft in relation to said runway being known in a horizontal plane with a first accuracy and in a vertical axis with a second accuracy. When the first accuracy is above a first threshold and/or when the second accuracy is above a second threshold, the appearance of the rectangular form or of the outline or of at least one marking is modified.

First claim

What is claimed is:

1. A method for three-dimensional graphic representation of at least one landing runway on a display device of an onboard display system for aircraft, said graphic representation being displayed in a synthetic view of an outside landscape, said runway comprising a coloured rectangular form, an outline surrounding said form and markings, the position of the aircraft in relation to said runway being known in a horizontal plane with a first accuracy and in a vertical axis with a second accuracy, wherein, when the first accuracy is above a first threshold and/or when the second accuracy is above a second threshold, the appearance of the rectangular form or of the outline or of at least one marking is modified without disappearance of both the rectangular form and the outline surrounding said form and markings.

2. The graphic representation method according to claim 1 , wherein the appearance modification is an enlargement of the rectangular form, this enlargement consisting in blurring the perimeter of the rectangular form over a width that is a function of the first and/or of the second accuracy.

3. The graphic representation method according to claim 2 , wherein the blurring is a continuous transparency gradient, the transparency increasing with the distance to the centre of the runway, the transparency law being a Gaussian or linear or radial function.

4. The graphic representation method according to claim 2 , wherein the blurring is obtained by a set of interleaved rectangles, each rectangle having a transparency value increasing with the distance to the centre of the runway.

5. The graphic representation method according to claim 1 , wherein the appearance modification consists in changing the outline to dotted lines and enlarging it, the enlargement being an increasing function of the first and/or of the second accuracy.

6. The graphic representation method according to claim 1 , wherein, when the display comprises several runways belonging to one and the same airport, all or part of the graphic representation of the runways simultaneously undergoes the same appearance modifications.

7. The graphic representation method according to claim 1 , wherein the appearance modifications are made progressively.

8. The graphic representation method according to claim 1 , wherein the method comprises at least two different appearance modifications, the first appearance modification depending on the first accuracy threshold and on the second accuracy threshold, the second appearance modification depending on a seventh accuracy threshold and on an eighth accuracy threshold, the second appearance modification succeeding or being added to the first modification.

9. The graphic representation method according to claim 1 , wherein the appearance modifications are effective only when the aircraft is below a predetermined distance to the runway.

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 and/or the real image on the outside landscape.

Assignees

• Thales Sa

Inventors

• Monvoisin Emmanuel
• Mariani Pierre
• Dumas Pierre-Yves
• Lux Johanna

Classifications

• 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

• G06T15/00

  Three-dimensional [3D] image rendering · CPC title

• B64D43/00 Primary

  Arrangements or adaptations of instruments · CPC title

• G06T2219/2016

  Rotation, translation, scaling · CPC title

• G06T17/05

  Geographic models · CPC title