Degree Type

Thesis

Date of Award

2010

Degree Name

Master of Science

Department

Electrical and Computer Engineering

First Advisor

Umesh Vaidya

Abstract

With rising fuel costs there is an initiative to conserve fuel during fight. Several methods have been proposed to calculate an optimum speed to y during cruise flight to maximize the range of a particular aircraft. This paper compares 11 of these methods using the same aircraft model and discusses how to implement these techniques in an autothrottle. Alternative implementations also include adding the algorithm to the Flight Management System to use during flight planning, or to including it in the databases to use during dispatch calculations. The results show that the speeds calculated by these methods are more fuel efficient than the usual cruise operating speed.

Since flying at the optimum speed is not always practical, this research also looked at the design of the industry autothrottle. Improvements to the industry autothrottle speed control law were implemented to see if improvements to fuel consumption could be achieved at any speed. The results show that the improvements proposed did not improve the fuel consumption during the conditions simulated.

Copyright Owner

Rebecca Marie Johnson

Language

en

Date Available

2012-04-30

File Format

application/pdf

File Size

110 pages

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