Method for computing and displaying piloting information including a “relief factor”

Patent metadata

Field	Value
Publication number	US-10569897-B2
Application number	US-201715846013-A
Country	US
Kind code	B2
Filing date	Dec 18, 2017
Priority date	Dec 29, 2016
Publication date	Feb 25, 2020
Grant date	Feb 25, 2020

Abstract

A method is provided for two-dimensional graphic representation on an aircraft display screen of an image or of a symbol or of a symbology (P E ) whose three-dimensional coordinates in a terrestrial reference frame are known. The graphic representation of the object or of the symbol is stretched in a vertical axis by a constant factor (α) lying between 1.0 and 1.2, the stretching having, for its neutral plane, the local horizontal geographic plane containing the aircraft. Furthermore, when the symbology is a pitch scale consisting of graduations, two successive graduations being separated by a constant angular value, the graphic representations of two successive graduations of the pitch scale are separated by a constant distance on the display screen.

First claim

The invention claimed is:

1. A method for two-dimensional graphic representation on an aircraft display screen (E) of an outside landscape whose three-dimensional coordinates in a terrestrial reference frame are known, wherein the graphic representation of the outside landscape is stretched only in a vertical axis by a constant factor (α), said stretching having, for its neutral plane, the local horizontal geographic plane containing the aircraft, said constant factor (α) being different from 1 and lying between 1.0 and 1.2.

2. The graphic representation method according to claim 1 , wherein a pitch scale (P E ) consisting of graduations is superimposed on the graphic representation of the outside landscape, two successive graduations being separated by a constant angular value, wherein the graphic representations of two successive graduations of the pitch scale are separated by a constant distance on the display screen, the distance being proportional to the product of the constant factor (α) by a second factor (β), the second factor (β) depending on the instantaneous angle of elevation (S) of the aircraft according to the expression:

β
=

1
+

tan
2

⁡

(
S
)

1
+

α
2

⁢

tan
2

⁡

(
S
)

.

3. The graphic representation method according to claim 1 , wherein the graphic representation includes a symbol (A) representative of the trajectory of the aircraft, and wherein the vertical coordinate of the symbol in the terrestrial reference frame is multiplied by the constant factor (α) before passage into a reference frame of the aircraft and projection on the display screen.

4. The graphic representation method according to claim 3 , wherein the symbol relates to a pitch scale.

5. The graphic representation method according to claim 3 , wherein the symbol is a navigation marker.

6. The graphic representation method according to claim 1 , wherein the graphic representation of the outside landscape is derived from an image sensor.

7. The graphic representation method according to claim 1 , wherein the display screen is an opaque or semi-transparent instrument panel screen or a screen of a head-up display device.

Assignees

• Thales Sa

Inventors

• Lux Johanna
• Monvoisin Emmanuel
• Rouzes Siegfried

Classifications

• G01C23/005 Primary

  Flight directors (indicating arrangements specially adapted for rotary gyroscopes G01C19/32) · CPC title

• G09G2340/125

  wherein one of the images is motion video · CPC title

• G09G2340/0414

  Vertical resolution change · 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

• B64D43/00 Primary

  Arrangements or adaptations of instruments · CPC title