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:
May. 21, 2019

Filed:

Dec. 07, 2016
Applicants:

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

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

Inventors:

Erwan Le-Bouedec, Toulouse, FR;

Rémi Morin, Plaisance du Touch, FR;

Jérémie Briere, Toulouse, FR;

Mathieu Reguerre, Toulouse, FR;

Nicolas Daniel, Toulouse, FR;

Assignees:

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

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B60T 8/17 (2006.01); G08G 5/00 (2006.01); G08G 5/02 (2006.01); B64C 25/42 (2006.01); G01C 23/00 (2006.01);
U.S. Cl.
CPC ...
B64C 25/426 (2013.01); B60T 8/1703 (2013.01); G01C 23/00 (2013.01); G08G 5/0013 (2013.01); G08G 5/0021 (2013.01); G08G 5/0091 (2013.01); G08G 5/025 (2013.01); G01W 2203/00 (2013.01); G08G 5/0008 (2013.01);
Abstract

The runway state determined on the ground by an aircraft and provided to the aircraft on approach does not make it possible to account for possible degradation of the runway occurring since the previous determination of that runway state. Updating of this runway state on the basis of a simple comparison between a desired deceleration and an observed deceleration resulting from a degraded runway is not satisfactory either. The disclosure herein thus provides for obtaining a local stopping distance according to a local runway state characterizing a runway zone on which the aircraft is in movement at the time of the landing, this local stopping distance being estimated based on local measurements made in the aircraft; obtaining a reference stopping distance according to a reference runway state; then comparing these two distances with each other to determine whether the local runway state is more degraded than the reference runway state.


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