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:
Mar. 05, 2024

Filed:

May. 24, 2021
Applicants:

Airbus (S.a.s.), Blagnac, FR;

Airbus Operations (S.a.s.), Toulouse, FR;

Inventors:

Philippe Foucault, Blagnac, FR;

Maxime Lefort, Toulouse, FR;

Quentin Demoulin, Toulouse, FR;

Assignees:

Airbus (S.A.S.), Blagnac, FR;

Airbus Operations (S.A.S.), Toulouse, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G06T 7/73 (2017.01); B64D 47/08 (2006.01); G06T 7/12 (2017.01); G06T 7/149 (2017.01); G06T 17/00 (2006.01); G06V 20/64 (2022.01);
U.S. Cl.
CPC ...
G06T 7/75 (2017.01); G06T 7/12 (2017.01); G06T 7/149 (2017.01); G06T 17/00 (2013.01); G06V 20/64 (2022.01); B64D 47/08 (2013.01); G06T 2207/10028 (2013.01); G06T 2207/10032 (2013.01); G06T 2207/30241 (2013.01);
Abstract

The method includes a step of acquisition of an image of the leading aircraft, a step of extraction of the outline, an adjustment step including implementing an outline registration algorithm, to determine an optimized profile from a comparison of the outline of the leading aircraft with a profile of the leading aircraft determined from a three-dimensional model of the leading aircraft and from an initial position of the following aircraft with respect to the leading aircraft, and a step of determination of the positioning according to six degrees of freedom of the following aircraft with respect to the leading aircraft, from the optimized profile and from the three-dimensional model of the leading aircraft. The method thus makes it possible to rapidly and accurately determine the positioning of the following aircraft with respect to the leading aircraft, this positioning being used to implement a formation flight.


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