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. 14, 2026

Filed:

Jul. 06, 2023
Applicant:

The Johns Hopkins University, Baltimore, MD (US);

Inventors:

Joseph L. Moore, Finksburg, MD (US);

Max R. Basescu, Columbia, MD (US);

Adam C. Polevoy, Columbia, MD (US);

Bryanna Y. Yeh, Hanover, MD (US);

Luca Scheuer, Philadelphia, PA (US);

Kevin C. Wolfe, Lutherville, MD (US);

Assignee:

The Johns Hopkins University, Baltimore, MD (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64U 10/25 (2023.01); B64C 19/02 (2006.01); B64U 50/13 (2023.01); G05D 1/00 (2006.01); B64U 101/30 (2023.01);
U.S. Cl.
CPC ...
B64U 10/25 (2023.01); B64C 19/02 (2013.01); B64U 50/13 (2023.01); G05D 1/0808 (2013.01); B64U 2101/30 (2023.01);
Abstract

A fixed-wing unmanned aerial vehicle (UAV) includes a propeller gimbal operably coupled to the body of the UAV at the forward end and the propeller gimbal is configured to pivot the propeller about a gimbal pivot axis to change a propeller angle. A controller of the UAV may be configured to control an attitude of flight of the UAV by controlling operation of the motor, the propeller gimbal, and the control surface assembly. The controller may be further configured to determine in-flight trajectory modifications that may require high maneuverability via high angle-of-attack attitudes of flight that are implemented via the propeller gimbal and trajectories determined from a dynamics model of the fixed-wing UAV.


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