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Neural Network Model of Unsteady, Nonlinear Aerodynamics

Date Issued
May 1, 2002
Author(s)
Henderson, Amy Pearsall
Advisor(s)
Frank G. Collins
Additional Advisor(s)
Kenneth K. Kimble, Bruce Whitehead
Abstract

Many flight control systems are developed from aerodynamic measurements obtained from static wind tunnel testing. These control systems frequently inadequately handle unsteady, nonlinear flight conditions. Dynamic roll angle measurements made in a wind tunnel have been obtained. This aerodynamic data presents a nonlinear, unsteady dynamical system. The roll angle trajectories have been successfully approximated with multilayer feedforward backpropagation neural networks.

Disciplines
Aerospace Engineering
Degree
Master of Science
Major
Aerospace Engineering
Embargo Date
May 1, 2002
File(s)
Thumbnail Image
Name

HendersonAmy.pdf

Size

12.9 MB

Format

Adobe PDF

Checksum (MD5)

a3b2fd7fd291d0184db013265ba6a196

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