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:
May. 27, 2025

Filed:

Sep. 16, 2022
Applicant:

Airbus Helicopters Deutschland Gmbh, Donauworth, DE;

Inventors:

Oliver Dieterich, Woerthsee, DE;

Christian Fischer, Neuried, DE;

Robin Lantzsch, Augsburg, DE;

Sueleyman Oezkurt, Leinfelden-Echterdingen, DE;

Walter Fichter, Constance, DE;

Tobias Rath, Munich, DE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 13/38 (2006.01); B64C 27/00 (2006.01); B64D 47/00 (2006.01);
U.S. Cl.
CPC ...
B64C 13/38 (2013.01); B64C 27/00 (2013.01); B64D 47/00 (2013.01);
Abstract

A flight control system that is adapted for controlling movements of a rotary wing aircraft while considering passenger discomfort, to a rotary wing aircraft with such a flight control system, and to a method of operating a flight control system. The flight control system includes sensors configured to generate sensor data based on captured motions of the rotary wing aircraft, motion actuators that are adapted for inducing a translational and/or a rotational movement of the rotary wing aircraft about at least one of a yaw axis, a roll axis, or a pitch axis, and a passenger discomfort-aware control unit that is configured to generate, based on the sensor data, passenger discomfort-aware actuator control signals for controlling the motion actuators of the rotary wing aircraft.


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