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. 29, 2008

Filed:

Mar. 14, 2005
Applicants:

Guner Firuz, Seattle, WA (US);

Michael H. Jaeger, Seattle, WA (US);

Robert M. Agate, Seattle, WA (US);

William M. Bresley, Seattle, WA (US);

Inventors:

Guner Firuz, Seattle, WA (US);

Michael H. Jaeger, Seattle, WA (US);

Robert M. Agate, Seattle, WA (US);

William M. Bresley, Seattle, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G05D 1/08 (2006.01); G05D 3/00 (2006.01); B64C 13/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

Methods and systems for automatically controlling aircraft takeoff rolls. A method in accordance with one embodiment of the invention includes receiving an indication of a target takeoff roll path for an aircraft, and automatically controlling a direction of an aircraft, while the aircraft is on a takeoff roll, to at least approximately follow the target takeoff roll path. The method can further include providing an input to a rudder of the aircraft and, upon receiving an indication of an engine failure, can transfer the input from the rudder to a rudder trim element. In still further embodiments, the method can include commanding a ground track angle when an airspeed of the aircraft reaches a threshold value, and maintaining the ground track angle as the airspeed of the aircraft exceeds the threshold value.


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