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. 05, 2016

Filed:

Feb. 06, 2015
Applicant:

Airbus Helicopters, Marignange Cedex, FR;

Inventor:

Bernard Certain, Aix En Provence, FR;

Assignee:

Airbus Helicopters, Marignane, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/56 (2006.01); G05D 1/08 (2006.01); B64C 13/18 (2006.01); B64C 27/57 (2006.01); B64C 27/78 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0808 (2013.01); B64C 13/18 (2013.01); B64C 27/57 (2013.01); G05D 1/0858 (2013.01);
Abstract

A method of enabling an autopilot () to cause a rotorcraft () to follow a path. At least one guide mode (G) relative to at least one progression axis (P, R, V, Y) of the rotorcraft () is selected by the rotorcraft pilot. Said selection causes the selected guide mode (G) to be inhibited () and causes a path setpoint (C) to be acquired () from the pilot of the rotorcraft () operating a manual control member () for controlling the progression of the rotorcraft (). The path setpoints (C) relating to other guide modes (G) of the rotorcraft () that continue to be engaged are conserved in their initial states and the autopilot () adapts the commands relating to the progression axes (P, R, V, Y) relating to these other guide modes (G).


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