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. 07, 2016

Filed:

Jun. 23, 2015
Applicant:

Thales, Courbevoie, FR;

Inventors:

Manuel Gutierrez-Castaneda, Toulouse, FR;

Bertrand Caudron De Coquereaumont, Tournefeuille, FR;

Xavier Jeanjean, Toulouse, FR;

Assignee:

Thales, Courbevoie, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G05D 1/00 (2006.01); G05D 1/06 (2006.01); B64C 13/18 (2006.01); B64C 13/22 (2006.01); G05D 1/04 (2006.01); G08G 5/00 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0061 (2013.01); B64C 13/18 (2013.01); B64C 13/22 (2013.01); G05D 1/042 (2013.01); G05D 1/0607 (2013.01); G08G 5/0047 (2013.01); G08G 5/003 (2013.01);
Abstract

A method for determining a switch-over vertical point from which an aircraft, having a current position, and flying a current vertical trajectory according to a manual piloting mode having an altitude setpoint, denoted target altitude, loaded by the pilot, switches to a piloting mode guided by a flight management system, in order to rejoin a predefined flight plan having a set of initial altitude constraints, comprising: calculating a first predicted vertical trajectory, determining a first point of intersection between the first predicted trajectory and the target altitude, determining a second predicted trajectory, determining the switch-over vertical point belonging to the first predicted vertical trajectory, based on any incompatible constraints, and as the intersection between the first predicted vertical trajectory and a predicted vertical trajectory calculated by integration of the dynamic flight equations by applying calculation hypotheses for a piloting mode guided by a flight management system.


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