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:
Feb. 07, 2017

Filed:

Sep. 03, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Reza Ghaemi, Niskayuna, NY (US);

Eric Richard Westervelt, Niskayuna, NY (US);

Mark Darnell, Grand Rapids, MI (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G06F 7/70 (2006.01); G06F 19/00 (2011.01); G08G 5/00 (2006.01); G05D 1/04 (2006.01); G06F 17/50 (2006.01); G06F 17/10 (2006.01);
U.S. Cl.
CPC ...
G08G 5/0095 (2013.01); G05D 1/042 (2013.01); G06F 17/10 (2013.01); G06F 17/5009 (2013.01); G08G 5/003 (2013.01);
Abstract

A method, medium, and system to receive a mathematical model representation of performance characteristics for an aircraft and an engine combination; perform a projection based model order reduction on the mathematical model representation; eliminate, based on the projected model, fast dynamics components of the mathematical model representation; determine a reduced order model, as a differential algebraic equation, wherein algebraic equations replace the fast dynamics; set a flight path angle and a throttle level angle as a control to minimize fuel consumption for the modeled aircraft and engine combination; discretize equations of motion for the modeled aircraft and engine combination and formulate optimization equations as a nonlinear programming problem; and determine an optimal open loop control that minimizes fuel consumption for the modeled aircraft and engine combination to climb to a prescribed cruise altitude and airspeed.


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