Constructive Non-Linear Control Design With Applications to Quad-Rotor and Fixed-Wing Aircraft
Author
Abstract

This paper recalls a non-linear constructive
method, based on controlling cascades of conic-systems as it
applies to the control of quad-rotor aircraft. Such a method
relied on the physical model of the system to construct high performance,
modest sampling period (Ts = .02 s) and low complexity
digital-controllers. The control of fixed-wing aircraft,
however is not nearly a straight forward task in extending
results related to the control of quad-rotor aircraft. Although
fixed-wing aircraft and quad-rotor aircraft ultimately share

Year of Publication
2010
Series Title
Technical Report
Date Published
01/2010
Institution
Institute for Software Integrated Systems, Vanderbilt University
City
Nashville, TN
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