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:
Apr. 16, 2019

Filed:

Aug. 08, 2016
Applicant:

Gulfstream Aerospace Corporation, Savannah, GA (US);

Inventors:

Michael Clay Harden, Savannah, GA (US);

Jong-Yeob Shin, Savannah, GA (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/16 (2006.01); B64C 5/02 (2006.01); B64C 5/10 (2006.01);
U.S. Cl.
CPC ...
B64C 13/16 (2013.01); B64C 5/02 (2013.01); B64C 5/10 (2013.01);
Abstract

A control unit for controlling movement of a stabilizer and an elevator on an aircraft, the control unit comprising a processor which is configured to receive a pitch reference command from a flight control input device of the aircraft, determine, based on the pitch reference command, an elevator command configured to command the elevator in the aircraft nose-up or nose-down direction, determine a difference between the elevator command and a desired elevator value corresponding to the pitch reference command, determine a threshold value as a desired maximum elevator deflection at a given pitch reference command, compare the difference with the threshold value and in response thereto generate a command signal configured to retain a current position of the stabilizer when the difference is smaller than or equal to the threshold value, and to command the elevator in the aircraft nose-up or nose-down direction based on the pitch reference command.


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