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:
Sep. 10, 2024

Filed:

Jul. 13, 2021
Applicant:

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

Inventors:

Gregory Mainland Horn, Mountain View, CA (US);

Damon Vander Lind, Alameda, CA (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/18 (2006.01); B64C 13/04 (2006.01); B64C 13/50 (2006.01); B64C 29/00 (2006.01); B64D 31/06 (2024.01); G05D 1/00 (2006.01); G05D 1/08 (2006.01); B64D 45/00 (2006.01);
U.S. Cl.
CPC ...
B64C 13/18 (2013.01); B64C 13/04 (2013.01); B64C 13/503 (2013.01); B64C 29/0033 (2013.01); B64D 31/06 (2013.01); G05D 1/0808 (2013.01); B64D 2045/0085 (2013.01);
Abstract

A geometry-based flight control system is disclosed. In various embodiments, a set of inceptor inputs associated with a requested set of forces and moments to be applied to the aircraft is received. An optimal mix of actuators and associated actuator parameters to achieve to an extent practical the requested forces and moments is computed, including by taking into consideration dynamically varying effectiveness of one or more actuators based on a current dynamic state of the aircraft. An output comprising for each actuator in the optimal mix a corresponding set of one or more control signals associated with the set of actuator parameters computed for that actuator is provided.


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