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. 03, 2020

Filed:

Aug. 07, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Douglas Conrad Cameron, Jr., Ladera Ranch, CA (US);

Michael James Duffy, Lansing, NY (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 31/06 (2006.01); B64D 45/00 (2006.01); B64C 39/02 (2006.01); B64C 27/54 (2006.01); G05D 13/62 (2006.01); G05D 17/02 (2006.01); B64C 27/57 (2006.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); B64C 27/57 (2013.01); B64C 39/024 (2013.01); B64D 45/00 (2013.01); G05D 13/62 (2013.01); G05D 17/02 (2013.01); B64C 2201/024 (2013.01); B64C 2201/108 (2013.01); B64D 2045/0085 (2013.01);
Abstract

Embodiments described herein provide active dampening of flexible modes of a UAV during flight operations. During operation of a UAV having a flexible airframe, the thrust and/or torque of the motor(s) coupled to propellers can induce flexing in the airframe that reduces the flight performance of the UAV. Measurements of a linear acceleration and/or an angular rate at a location proximate to the motor are performed, and flexible modes in the airframe of the UAV are identified based on the measurements. An operation of the motor(s) is modified based on the measurements to dampen the flexible mode.


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