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:
Mar. 04, 2014

Filed:

Aug. 17, 2011
Applicants:

David Lemay, Chaville, FR;

David Frank, Paris, FR;

Michel Basset, Heimsbrunn, FR;

Yann Chamaillard, Le Bardon, FR;

Inventors:

David Lemay, Chaville, FR;

David Frank, Paris, FR;

Michel Basset, Heimsbrunn, FR;

Yann Chamaillard, Le Bardon, FR;

Assignee:

Messier-Bugatti-Dowty, Velizy Villacoublay, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G05D 1/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

A method of controlling a yawing movement of an aircraft running along the ground, the aircraft comprising at least one first landing gear with a steerable bottom part bearing wheels. The method comprises the steps of (1) on the basis of a yaw rate setpoint {dot over (φ)}, determining a wheel-steering prepositioning angle θ; and (2) using closed-loop control which as its input has the yaw rate setpoint and which generates a command to steer the bottom part in order to steer it through a steering angle θequal to the sum of this prepositioning angle θand of an angle θwhich is determined taking account of an error between the yaw rate setpoint {dot over (φ)}and the measured yaw rate {dot over (φ)}when the steerable bottom part is steered by the steering angle θ.


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