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:
Feb. 16, 2021

Filed:

Oct. 19, 2017
Applicant:

Aurora Flight Sciences Corporation, Manassas, VA (US);

Inventors:

Riley Griffin, Cambridge, MA (US);

Edward Scott, Cambridge, MA (US);

Sean Humbert, Cambridge, MA (US);

Assignee:
Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/16 (2006.01); G01C 21/16 (2006.01); G05D 1/02 (2020.01); B64C 3/00 (2006.01); G01B 7/16 (2006.01); G05D 1/08 (2006.01); G01B 11/16 (2006.01); B64C 39/02 (2006.01); G01C 19/5698 (2012.01); G01P 15/18 (2013.01);
U.S. Cl.
CPC ...
B64C 13/16 (2013.01); B64C 3/00 (2013.01); G01B 7/16 (2013.01); G01C 21/16 (2013.01); G05D 1/0204 (2013.01); G05D 1/0816 (2013.01); B64C 39/024 (2013.01); G01B 11/18 (2013.01); G01C 19/5698 (2013.01); G01P 15/18 (2013.01);
Abstract

An aerial vehicle comprising an airframe, an aircraft flight controller to provide an output control signal, and a planar printed circuit board positioned on the airframe. The printed circuit board may include coupled thereto a processor, a rate gyroscope, and at least three accelerometers. The processor is configured to generate an actuation signal based at least in part on a feedback signal received from at least one of said rate gyroscope and the at least three accelerometers. The processor communicates the actuation signal to said aircraft flight controller, which is configured to adjust the output control signal based on said actuation signal.


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