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:
Jul. 11, 2017

Filed:

May. 04, 2016
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Herve Morel, Lamanon, FR;

Nicolas Queiras, Les Pennes Mirabeau, FR;

Assignee:

AIRBUS HELICOPTERS, Marignane, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/08 (2006.01); B64C 13/16 (2006.01); B64C 27/82 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0816 (2013.01); B64C 13/16 (2013.01); B64C 27/82 (2013.01); G05D 1/0858 (2013.01); B64C 2027/8281 (2013.01);
Abstract

A method of controlling a deflection angle of pitching stabilizer means for an aircraft. The method includes a preliminary stage for preparing at least one control relationship delivering a setpoint angle that is to be reached by the deflection angle as a function of at least one flight parameter of the aircraft and of an incidence parameter of the pitching stabilizer means. During an operational stage an operational stage (STP), a 'flight' value is determined for each of the flight parameters, a 'setpoint' value is determined for the incidence parameter, a setpoint angle is determined by inputting the flight values and setpoint value into the control relationship, and at least one actuator is actuated in order to cause the deflection angle of the pitching stabilizer means to reach the setpoint angle.


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