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. 26, 2017

Filed:

Jul. 18, 2016
Applicant:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Inventors:

Sung K. Kim, Bedford, TX (US);

Christopher M. Bothwell, Grapevine, TX (US);

Robert Lee Fortenbaugh, Pantego, TX (US);

Assignee:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/00 (2006.01); B64G 1/24 (2006.01); B64C 13/50 (2006.01); B64C 13/04 (2006.01); B64D 43/00 (2006.01); B64C 13/12 (2006.01);
U.S. Cl.
CPC ...
B64C 13/503 (2013.01); B64C 13/04 (2013.01); B64C 13/12 (2013.01); B64D 43/00 (2013.01);
Abstract

According to one embodiment, a flight control system includes a pilot control assembly and a flight control computer. The pilot control assembly can receive commands from a pilot. The flight control computer can receive, from the pilot control assembly, a pilot command to change a first flight characteristic, wherein changing the first flight characteristic would result in an expected change to a second flight characteristic. The flight control computer can instruct, in response to the received pilot command, the flight control system to change a first operating condition of the flight control system based on an inherently-coupled relationship between the first flight characteristic and the second flight characteristic. The flight control computer can instruct, in response to the expected change to the second flight characteristic, the flight control system to change a second operating condition of the flight control system.


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