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
Link To Document :
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