Method for graphically representing a synthetic three-dimensional view of the exterior landscape in an on-board visualisation system for aircraft

US10249267B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10249267-B2
Application numberUS-201615394778-A
CountryUS
Kind codeB2
Filing dateDec 29, 2016
Priority dateDec 29, 2015
Publication dateApr 2, 2019
Grant dateApr 2, 2019

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  1. Title

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  2. Abstract

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  4. Key dates

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  5. First independent claim

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Abstract

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The general field of the invention is that of the graphical representation of a synthetic three-dimensional view of the exterior landscape in an on-board visualization system for aircraft, said graphical representation being displayed on a visualization screen comprising the piloting and navigation information of said aircraft superposed onto said three-dimensional synthetic representation of the exterior landscape, said synthetic representation being computed up to a first determined distance, characterized in that said three-dimensional synthetic representation is tilted at a tilt angle about an axis positioned at the level of the terrain in a substantially horizontal plane, and substantially perpendicularly to an axis between the flight direction and the heading of the aircraft, said axis moving with the aircraft.

First claim

Opening claim text (preview).

What is claimed is: 1. A method for graphically representing a synthetic three-dimensional view of the exterior landscape in an on-board visualisation system for aircraft, said graphical representation being displayed on a visualisation screen comprising the piloting or navigation information of said aircraft superposed onto said three-dimensional synthetic representation of the exterior landscape, said synthetic representation being computed up to a first determined distance, wherein said three-dimensional synthetic representation is tilted at a tilt angle about an axis positioned at the level of the terrain in a substantially horizontal plane, and substantially perpendicularly to an axis between the flight direction and the heading of the aircraft, said axis moving with the aircraft, said tilt angle being computed so that the angle between the horizon line or ZPRL and the limit of the synthetic representation computed up to a first determined distance is limited to three degrees. 2. The graphical representation method according to claim 1 , wherein the axis is positioned substantially vertically with respect to the aircraft. 3. The graphical representation method according to claim 1 , wherein the axis is positioned in front of the aircraft, at a second distance of between a few tens of nautical miles and 40 nautical miles. 4. The graphical representation method according to claim 1 , wherein below a determined difference in altitude between the aircraft and the overflown terrain, the tilt angle is zero. 5. The graphical representation method according to claim 4 , wherein the value of the determined difference in altitude between the aircraft and the overflown terrain is 7500 feet. 6. The graphical representation method according to claim 1 , wherein above a determined difference in altitude between the aircraft and the overflown terrain, the tilt angle increases with altitude. 7. The graphical representation method according to claim 1 , wherein the tilt angle is determined so that the angular difference between the limit of the three-dimensional representation of the exterior landscape computed up to the first determined distance and a line representing the true horizon is less than one degree. 8. The graphical representation method according to claim 1 , wherein the visualisation device comprises a real image of the exterior landscape superposed onto the synthetic view of the exterior landscape. 9. The graphical representation method according to claim 1 , wherein the visualisation device is one of the screens of the instrument panel of the aircraft. 10. The graphical representation method according to claim 1 , wherein the visualisation device is a visualisation device referred to as a “heads-up” visualisation device comprising an optical element superposing the synthetic image or the real image onto the exterior landscape.

Assignees

Inventors

Classifications

  • G09G5/38Primary

    with means for controlling the display position · CPC title

  • Adaptation to parameters characterising the motion of the vehicle · CPC title

  • Avionics applications · CPC title

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

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

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What does patent US10249267B2 cover?
The general field of the invention is that of the graphical representation of a synthetic three-dimensional view of the exterior landscape in an on-board visualization system for aircraft, said graphical representation being displayed on a visualization screen comprising the piloting and navigation information of said aircraft superposed onto said three-dimensional synthetic representation of t…
Who is the assignee on this patent?
Thales Sa
What technology area does this patent fall under?
Primary CPC classification G09G5/38. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Apr 02 2019 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).