DocumentCode :
2848910
Title :
Adaptive control of piecewise linear systems with applications to NASA GTM
Author :
Qian Sang ; Gang Tao
Author_Institution :
Dept. of Electr. & Comput. Eng., Univ. of Virginia, Charlottesville, VA, USA
fYear :
2011
fDate :
June 29 2011-July 1 2011
Firstpage :
1157
Lastpage :
1162
Abstract :
Nonlinear plants with their operating range covering multiple trim points are modeled as piecewise linear systems, where variations in operating points are modeled as switches between constituent linearized system dynamics. The adaptive state feedback for state tracking control problem for such systems is studied, for which piecewise linear reference model systems are used to generate desired state trajectories. Adaptive control schemes are developed, and it is proved that asymptotic tracking performance can be achieved if the reference input is sufficiently rich and the switches are sufficiently slow. Stability and tracking performance of the proposed adaptive control schemes are analyzed and evaluated on the high-fidelity Simulink model of the Generic Transport Model (GTM) developed at NASA Langley.
Keywords :
aerospace control; asymptotic stability; control system synthesis; model reference adaptive control systems; nonlinear control systems; piecewise linear techniques; state feedback; tracking; NASA GTM; adaptive control; adaptive state feedback; asymptotic tracking performance; generic transport model; high-fidelity Simulink model; linear system dynamics; nonlinear plants; piecewise linear reference model system; piecewise linear system; stability; state tracking control problem; trim points; Adaptation models; Adaptive control; Atmospheric modeling; Bismuth; Linear systems; Stability analysis; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2011
Conference_Location :
San Francisco, CA
ISSN :
0743-1619
Print_ISBN :
978-1-4577-0080-4
Type :
conf
DOI :
10.1109/ACC.2011.5990918
Filename :
5990918
Link To Document :
بازگشت