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. 31, 2022

Filed:

Aug. 05, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Bryan E. Kashawlic, Chester Heights, PA (US);

Brandon R. Brown, Media, PA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G05D 1/10 (2006.01); B64C 39/02 (2006.01); G05D 1/08 (2006.01); B64D 31/12 (2006.01);
U.S. Cl.
CPC ...
G05D 1/101 (2013.01); B64C 39/024 (2013.01); B64D 31/12 (2013.01); G05D 1/0816 (2013.01); B64C 2201/027 (2013.01); B64C 2201/042 (2013.01); B64C 2201/108 (2013.01); B64C 2201/141 (2013.01);
Abstract

Methods, apparatus, systems, and articles of manufacture are disclosed for flight control prioritization. An example apparatus includes a thrust state determiner to determine a first thrust margin between a first limit of first available power for first rotors of a rotorcraft and a first thrust state associated with the first rotors, determine a second thrust margin between a second limit of second available power for second rotors of the rotorcraft and a second thrust state associated with the second rotors, and identify the first thrust margin or the second thrust margin as a selected thrust margin based on a vertical control profile of the rotorcraft, and a command generator to determine a first vertical control command based on the selected thrust margin and a second vertical control command, the second vertical control command being executed by the rotorcraft, and control the rotorcraft based on the first vertical control command.


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