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. 08, 2025

Filed:

Feb. 26, 2023
Applicant:

Joby Aero, Inc., Santa Cruz, CA (US);

Inventors:

Gregor Veble Mikic, Santa Cruz, CA (US);

Jason Ryan, Santa Cruz, CA (US);

JoeBen Bevirt, Santa Cruz, CA (US);

Assignee:

Joby Aero, Inc., Santa Cruz, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 43/02 (2006.01); G01P 5/00 (2006.01); G01P 5/02 (2006.01); G01P 21/02 (2006.01); G06V 20/64 (2022.01); G06V 40/10 (2022.01); G06V 40/20 (2022.01);
U.S. Cl.
CPC ...
B64D 43/02 (2013.01); G01P 5/00 (2013.01); G01P 5/02 (2013.01); G01P 21/025 (2013.01); G06V 20/64 (2022.01); G06V 40/103 (2022.01); G06V 40/23 (2022.01);
Abstract

A method for determining airspeed of an aircraft that includes determining a rotor model relating a power coefficient of a propeller of the aircraft to an axial inflow velocity through the propeller as a function of a set of rotor operating parameters; determining the set of rotor operating parameters by sampling an electronic control signal associated with an electric motor actuating the propeller; computing the axial inflow velocity through the propeller based on the set of rotor operating parameters using the rotor model; and determining the airspeed based on the axial inflow velocity.


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