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:
Jan. 02, 2018

Filed:

Jun. 03, 2015
Applicant:

Thales, Courbevoie, FR;

Inventors:

Sylvain Lissajoux, Toulouse, FR;

Matthieu Claybrough, Toulouse, FR;

Christophe Garnavault, Meudon la Foret, FR;

Assignee:

THALES, Courbevoie, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 31/06 (2006.01); B64D 33/04 (2006.01); B64C 25/44 (2006.01); G01C 23/00 (2006.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); B64C 25/44 (2013.01); B64D 33/04 (2013.01); G01C 23/00 (2013.01);
Abstract

A method and device for controlling at least one actuator control system of an aircraft, an associated computer program product and aircraft are disclosed. In one aspect, the method includes determining a variation in thrust of the aircraft for controlling a variable relating to the aircraft relative to a set point, calculating a first control command signal to be sent to an engine control system in order to obtain the variation in thrust, and transmitting the first control command signal to the engine control system. The controlled variable can be an acceleration along a direction taken by a speed vector among the air speed vector and the ground speed vector and the set point can be an acceleration set point along the direction.


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