The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 05, 2018

Filed:

Jan. 15, 2014
Applicant:

Airbus Defence and Space Gmbh, Ottobrunn, DE;

Inventors:

Christoph Vernaleken, Eiterfeld, DE;

Marco Opitz, Rohrbach, DE;

Harald Neujahr, Markt Schwaben, DE;

Eugenio Ferreira, Paris, FR;

Lutz Broszio, Ingolstadt, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/00 (2006.01); G05D 1/08 (2006.01); G05D 3/00 (2006.01); G06F 7/00 (2006.01); G06F 17/00 (2006.01); G01C 21/00 (2006.01); G01C 23/00 (2006.01); B64D 45/00 (2006.01); G08B 21/00 (2006.01);
U.S. Cl.
CPC ...
G01C 23/005 (2013.01); B64D 45/00 (2013.01); G01C 21/00 (2013.01); G01C 23/00 (2013.01);
Abstract

A method for displaying an attitude of an aircraft includes receiving a roll angle, a pitch angle and a yaw angle of the aircraft, generating a display image indicating the roll angle, the pitch angle and the yaw angle, and displaying the display image on a display device. The display image includes a spherical shell with a track angle scale projected onto the spherical shell along a latitude line of the spherical shell and with a pitch angle scale projected onto the spherical shell along a longitude line of the spherical shell. Furthermore, the display image includes a graphical aircraft attitude indicator inside the spherical shell rotated with respect to the spherical shell such that the graphical aircraft attitude indicator indicates the roll angle, the pitch angle and the yaw angle of the aircraft with respect to the spherical shell.


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