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:
Dec. 19, 2023

Filed:

Feb. 27, 2023
Applicant:

Electra Aero, Inc., Manassas, VA (US);

Inventors:

Robert John Hansman, Jr., Cambridge, MA (US);

Christopher B. Courtin, Somerville, MA (US);

Oliver Masefield, Stans, CH;

Assignee:

Electra Aero, Inc., Manassas, VA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/00 (2006.01); G05D 1/08 (2006.01); B64C 13/16 (2006.01); B64D 31/10 (2006.01);
U.S. Cl.
CPC ...
G05D 1/0825 (2013.01); B64C 13/16 (2013.01); B64D 31/10 (2013.01);
Abstract

An aircraft may include a tail having a rudder and a pair of wings. The pair of wings may include at least one flap and at least one roll control device. The aircraft may also include at least two thrust-producing devices. The aircraft may also include a differential thrust control system including a computing device having at least one processor. The at least one processer may be configured to control an attitude of the aircraft by selectively operating the at least two thrust-producing devices, the rudder, and the at least one roll control device based at least in part on a plurality of conditions provided by a plurality of sensors on the aircraft and a selected mode setting of a mode control panel. The computing device may be communicatively coupled to the at least two thrust-producing devices, the rudder, and the at least one roll control device.


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