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:
Mar. 30, 2021

Filed:

Sep. 11, 2018
Applicant:

Textron Aviation Inc., Wichita, KS (US);

Inventors:

Steven G. Hagerott, Wichita, KS (US);

Philippe A. Ciholas, Sedgwick, KS (US);

Assignee:

Textron Innovation Inc., Providence, RI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/18 (2006.01); G05D 1/08 (2006.01); B64C 9/10 (2006.01); B64C 13/04 (2006.01);
U.S. Cl.
CPC ...
B64C 13/18 (2013.01); B64C 9/10 (2013.01); B64C 13/044 (2018.01); G05D 1/0816 (2013.01);
Abstract

An automatic yaw enhancement method for an aircraft having at least one propeller includes providing to a flight controller a pilot command from a pilot interface and avionic data for an airspeed, an angle of attack, and a thrust. A P-factor compensation is determined based on one or more of the airspeed, the angle of attack, and the thrust. A command to a trim device is determined based on a P-factor compensation. When a rudder bias persists, the command to the trim device is repeatedly updated until a rudder force input is nullified. The methods provide automatic pilot assistance for controlling yaw during asymmetric flight conditions and automatic turn coordination while allowing intentional side-slip for facilitating crosswind landings.


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