DocumentCode
3357596
Title
Application of adaptive control with closed-loop reference models to a model aircraft with actuator dynamics and input uncertainty
Author
Zollitsch, Alexander W. ; Holzapfel, Florian ; Annaswamy, Anuradha M.
Author_Institution
Inst. of Flight Syst. Dynamics, Tech. Univ. Munchen, Garching, Germany
fYear
2015
fDate
1-3 July 2015
Firstpage
3848
Lastpage
3853
Abstract
This paper presents an adaptively augmented LQR controller for the FSD ExtremeStar, a high agility model airplane. Uncertainties in the control effectiveness are compensated by a direct model reference adaptive controller (MRAC), which uses closed-loop reference models (CRMs). Simulation results on a nonlinear plant with actuator dynamics and sensor models indicate that the CRM adaptive controller provides additional robustness to plant uncertainties and unmodeled dynamics compared to the classical MRAC architecture, where an open-loop reference model is employed.
Keywords
actuators; aircraft control; closed loop systems; control system synthesis; linear quadratic control; model reference adaptive control systems; nonlinear control systems; robust control; uncertain systems; CRM adaptive controller; FSD ExtremeStar; MRAC; actuator dynamics; adaptively augmented LQR controller; aircraft model; closed-loop reference models; control effectiveness uncertainty compensation; controller design; direct model reference adaptive controller; high agility model airplane; input uncertainty; nonlinear plant; plant uncertainty; robustness; sensor model; unmodeled dynamics; Actuators; Adaptation models; Adaptive systems; Aircraft; Atmospheric modeling; Customer relationship management; Mathematical model;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference (ACC), 2015
Conference_Location
Chicago, IL
Print_ISBN
978-1-4799-8685-9
Type
conf
DOI
10.1109/ACC.2015.7171930
Filename
7171930
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