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:
Nov. 17, 2015

Filed:

Oct. 23, 2014
Applicant:

Thales, Neuilly-sur-Seine, FR;

Inventors:

Jerome Sacle, Valence, FR;

Johan Boyer, Valence, FR;

Francois Coulmeau, Valence, FR;

Assignee:

THALES, Courbevoie, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G05D 1/00 (2006.01); G05D 1/04 (2006.01); G08G 5/00 (2006.01); G01C 21/20 (2006.01); G05D 1/06 (2006.01); G06Q 10/04 (2012.01); G08G 5/02 (2006.01);
U.S. Cl.
CPC ...
G05D 1/00 (2013.01); G01C 21/20 (2013.01); G05D 1/0005 (2013.01); G05D 1/042 (2013.01); G05D 1/0676 (2013.01); G06Q 10/047 (2013.01); G08G 5/003 (2013.01); G08G 5/006 (2013.01); G08G 5/0095 (2013.01); G08G 5/025 (2013.01);
Abstract

A method for aiding navigation for an aircraft between a descent start point and a computation end point, comprises the computation steps of: collecting a flight plan consisting of a succession of waypoints and of the associated vertical constraints; determining a corridor consisting of a floor trajectory and of a ceiling trajectory defining the minimum and maximum altitudes permitted to the aircraft; splitting the corridor into several cells defined between two waypoints furthest apart and between which the ceiling trajectory is distinct from the floor trajectory; determining for at least one cell a vertical trajectory complying with the altitude constraints and comprising the longest possible IDLE segment; and a step consisting in determining and displaying maneuvering points of the aircraft making it possible to follow the target vertical trajectory.


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