IP Library Granted Patent US 8,823,555
Granted Patent B2
US 8,823,555 · App. 13/701,287 · Granted Sep 2, 2014

Apparatus for displaying terrain on a display apparatus of an airborne vehicle

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Quick Facts
Patent No.
US 8,823,555
App. No.
13/701,287
Granted
Sep 2, 2014
Kind
B2
Abstract

An apparatus for displaying terrain on a display apparatus of an airborne vehicle is provided. The apparatus includes a synthetic vision system having a terrain and obstruction database, an enhanced vision system with sensors for recording terrain data, a height and position sensor for determining the flight state data, a display apparatus, a processor for fusion of the data from the synthetic vision system and from the enhanced vision system. The height information that is produced by the synthetic vision system and the enhanced vision system is stored as pixels in a two-dimensional grid network. The fusion processor uses an error function for insertion of a pixel into the two-dimensional grid network. The error function provides an estimate of the size of the respective cell in which the pixel is stored, from the distance between the pixel and the sensor position.

Claims (16)

1. A device for displaying terrain on a display device of an aircraft, comprising

a synthetic vision system having a terrain and obstacle database;

an enhanced vision system having sensors configured to acquire terrain data;

a height and position sensor configured to determine flight status data;

a display device;

a fusion processor coupled to the synthetic and enhanced vision systems, wherein the fusion processor is configured to fuse the data from the synthetic and enhanced vision systems to generate terrain data, wherein height information generated by the synthetic and enhanced vision systems is stored as pixels in a two-dimensional grid network; and

a graphics processor configured to send the terrain data generated by the fusion processor to the display device while taking into account the flight status data determined by the height and position sensor,

wherein the fusion processor is configured to use an error function when inserting a pixel into the two-dimensional grid network, the error function providing an estimate of the size of the respective cell, in which the pixel is stored, from the distance of the pixel from the sensor position.

2. The device as claimed in claim 1 , wherein the two-dimensional grid network represents a parameterization of a tangential surface of a terrestrial sphere with a hierarchical non-regular structure and a predeterminable maximum number of cells, and wherein a center of the two-dimensional grid network imaging the position of the sensor of the enhanced vision system.

3. A method for displaying terrain on a display device of an aircraft, comprising

determining, by a height and position sensor, flight status data;

acquiring, by an enhanced vision system having sensors, terrain data;

fusing, by a fusion processor, data from a synthetic vision system and the enhanced vision system to generate terrain data, wherein height information generated by the synthetic and enhanced vision systems is stored as pixels in a two-dimensional grid network;

outputting, by a graphics processor, the terrain data generated by the fusion processor to a display device while taking into account the flight status data determined by the height and position sensor,

wherein the fusion processor uses an error function when inserting a pixel into the two-dimensional grid network, the error function providing an estimate of the size of the respective cell, in which the pixel is stored, from the distance of the pixel from the sensor position.

4. The method as claimed in claim 3 , wherein the two-dimensional grid network represents a parameterization of a tangential surface of a terrestrial sphere with a hierarchical non-regular structure and a predeterminable maximum number of cells, and wherein a center of the two-dimensional grid network imaging the position of the sensor of the enhanced vision system.

Assignments (6)
CORRECTIVE ASSIGNMENT TO CORRECT THE PATENT NUMBER FROM 9476976 TO 9476967 PREVIOUSLY RECORDED AT REEL: 48284 FRAME: 766. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Apr 15, 2020
From: AIRBUS DS ELECTRONICS AND BORDER SECURITY GMBH
To: HENSOLDT SENSORS GMBH
Reel/Frame 052534/0259 →
CORRECTIVE ASSIGNMENT TO CORRECT THE PATENT NUMBER PAT. NO.9476976 PREVIOUSLY RECORDED ON REEL 047691 FRAME 0890. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT OF ASSIGNORS INTEREST. Recorded Jun 18, 2019
From: AIRBUS DEFENCE AND SPACE GMBH
To: AIRBUS DS ELECTRONICS AND BORDER SECURITY GMBH
Reel/Frame 049499/0724 →
CHANGE OF NAME Recorded Feb 7, 2019
From: AIRBUS DS ELECTRONICS AND BORDER SECURITY GMBH
To: HENSOLDT SENSORS GMBH
Reel/Frame 048284/0766 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 6, 2018
From: AIRBUS DEFENCE AND SPACE GMBH
To: AIRBUS DS ELECTRONICS AND BORDER SECURITY GMBH
Reel/Frame 047691/0890 →
CHANGE OF NAME Recorded Oct 19, 2016
From: EADS DEUTSCHLAND GMBH
To: AIRBUS DEFENCE AND SPACE GMBH
Reel/Frame 040418/0890 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 18, 2013
From: SCHAFHITZEL, TOBIAS
To: EADS DEUTSCHLAND GMBH
Reel/Frame 029656/0259 →