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:
May. 20, 2025

Filed:

Jan. 24, 2024
Applicant:

Kitty Hawk Corporation, Palo Alto, CA (US);

Inventors:

Alexander David Selwa, San Francisco, CA (US);

Todd Reichert, Mountain View, CA (US);

Mark Johnson Cutler, Sunnyvale, CA (US);

Assignee:

Kitty Hawk Corporation, Palo Alto, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/04 (2006.01); B64C 27/08 (2023.01); B64C 27/20 (2023.01); G05D 1/00 (2006.01); G05D 1/495 (2024.01); G05D 1/652 (2024.01); G05D 1/654 (2024.01); G05G 9/047 (2006.01);
U.S. Cl.
CPC ...
B64C 13/0421 (2018.01); B64C 27/08 (2013.01); B64C 27/20 (2013.01); G05D 1/0816 (2013.01); G05D 1/0858 (2013.01); G05D 1/102 (2013.01); G05D 1/495 (2024.01); G05D 1/652 (2024.01); G05D 1/654 (2024.01); G05G 9/047 (2013.01);
Abstract

A forward velocity associated with an aircraft is received. The aircraft includes a multicopter with a plurality of rotors which rotate in a substantially horizontal plane. A pitch offset is determined based at least in part on the forward velocity, where the pitch offset changes monotonically with the forward velocity. A desired pitch is determined based at least in part on the pitch offset and a pitch angle specified via a hand control. A plurality of control signals for the plurality of rotors is determined based at least in part on the desired pitch.


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