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:
Aug. 20, 2019

Filed:

Oct. 06, 2017
Applicant:

Airbus Operations Sas, Toulouse, FR;

Inventor:

Stéphane Delannoy, Sainte Marie, FR;

Assignee:

AIRBUS OPERATIONS SAS, Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/10 (2006.01); B64C 13/50 (2006.01); B64C 13/04 (2006.01); G05D 1/08 (2006.01); B64C 13/18 (2006.01);
U.S. Cl.
CPC ...
G05D 1/101 (2013.01); B64C 13/04 (2013.01); B64C 13/0421 (2018.01); B64C 13/18 (2013.01); B64C 13/503 (2013.01); B64C 13/506 (2018.01); G05D 1/0825 (2013.01);
Abstract

A system including a set of computation modules configured to be utilized for computation of gains of at least one piloting law relative to at least one piloting axis of the aircraft and a data capture unit for capturing in at least one computation unit associated with a given piloting axis of the aircraft first values illustrating aerodynamic coefficients of the aircraft and second values defining delay and filter characteristics of the control chain relative to the given piloting axis, the computation unit being configured to compute the gains of the piloting law utilizing at least a part of the set of computation modules and the computation unit computing inputs intended for at least one actuator of a control surface adapted to control the aircraft relative to the given piloting axis in accordance with a corresponding current control value.


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