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:
Aug. 05, 2025

Filed:

Jun. 21, 2024
Applicant:

Archer Aviation Inc., San Jose, CA (US);

Inventors:

Jeffrey Mark Bosworth, Argyle, TX (US);

Abhishek Vaidya, San Jose, CA (US);

Maicon Secchi, Sao Jose dos Campos, BR;

Marcelo Santos, San Jose, CA (US);

Assignee:

Archer Aviation Inc., San Jose, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G06F 17/00 (2019.01); B64D 31/16 (2024.01); B64D 45/00 (2006.01); B64C 29/00 (2006.01);
U.S. Cl.
CPC ...
B64D 31/16 (2024.01); B64D 45/00 (2013.01); B64C 29/0008 (2013.01); B64D 2045/0085 (2013.01);
Abstract

The present disclosure relates generally to flight control of electric aircraft and other powered aerial vehicles. In one embodiment, an electrical system for an aircraft is disclosed, comprising: at least one processor configured to: receive pilot input indicating a commanded aircraft state, determine an aircraft thrust for achieving the commanded aircraft state, retrieve at least one propeller parameter associated with propeller speeds, wherein the propeller parameter is determined to reduce a structural vibratory response in the aircraft. The at least one processor is further configured to determine a respective command for each propeller of the aircraft to achieve the determined aircraft thrust based on the at least one propeller parameter and control each propeller of the aircraft based on the corresponding respective command.


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