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. 08, 2018

Filed:

Jun. 07, 2016
Applicant:

Thales, Courbevoie, FR;

Inventors:

Johan Boyer, Toulouse, FR;

Benoît Dacre-Wright, Toulouse, FR;

Assignee:

THALES, Courbevoie, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64F 1/18 (2006.01); B64C 19/00 (2006.01); G05D 1/00 (2006.01); G05D 1/06 (2006.01); G08G 5/00 (2006.01); G08G 5/02 (2006.01);
U.S. Cl.
CPC ...
B64F 1/18 (2013.01); B64C 19/00 (2013.01); G05D 1/0005 (2013.01); G05D 1/0676 (2013.01); G08G 5/0021 (2013.01); G08G 5/025 (2013.01); G08G 5/0034 (2013.01); Y02T 50/84 (2013.01);
Abstract

A method of automatic determination of a descent and approach profile for an aircraft is based on a backward computation of propagation of a state of the aircraft along segments S(i) from a backward computation start point to the start point DECEL of onset of the deceleration of the aircraft. The method of automatic determination comprises for each segment S(i) a step of determining an optimal speed V(i) of the aircraft over the range of speeds of the next aerodynamic configuration C(j+1) to be implemented as a function of a predetermined deceleration strategy and/or of predetermined constraints inherent in the flight procedure or introduced by the pilot in his flight plan.


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