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. 13, 2021

Filed:

Nov. 17, 2017
Applicant:

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

Inventors:

Riley Griffin, Manassas, VA (US);

Jeffery Saunders, Manassas, VA (US);

Assignee:
Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G05B 6/02 (2006.01); F16M 11/20 (2006.01); B64D 47/08 (2006.01); F16M 11/18 (2006.01); F16M 13/02 (2006.01); B64C 39/02 (2006.01);
U.S. Cl.
CPC ...
F16M 13/02 (2013.01); B64C 39/024 (2013.01); B64D 47/08 (2013.01); F16M 11/18 (2013.01); F16M 11/2007 (2013.01); G05B 6/02 (2013.01); B64C 2201/123 (2013.01); B64C 2201/127 (2013.01); F16M 2200/04 (2013.01);
Abstract

A gimbal stabilizing system for an aircraft having an airframe is disclosed. The gimbal stabilizing system may comprise a gimbal apparatus having at least one gimbal actuator to adjust a position of the gimbal apparatus about an axis, wherein the gimbal apparatus is positioned on the airframe, an angular acceleration apparatus positioned on the airframe to generate an angular acceleration signal reflecting an angular acceleration of the airframe, and a gimbal controller operatively coupled to each of said angular acceleration apparatus and said gimbal apparatus. The gimbal controller may be configured to generate a gimbal control signal to compensate for the angular acceleration of the airframe based at least in part on a feedback control loop and a feedforward control loop, the feedforward control loop having the angular acceleration signal as an input thereto. The gimbal controller may be further configured to output the gimbal control signal to said gimbal apparatus to adjust a position of the gimbal apparatus.


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