DocumentCode :
3521567
Title :
Robust nonlinear aircraft tracking control using synthetic jet actuators
Author :
MacKunis, W. ; Subramanian, Sivaraman ; Mehta, Sharad ; Ton, C. ; Curtis, J.W. ; Reyhanoglu, M.
Author_Institution :
Dept. of Phys. Sci., Embry-Riddle Aeronaut. Univ., Daytona Beach, FL, USA
fYear :
2013
fDate :
10-13 Dec. 2013
Firstpage :
220
Lastpage :
225
Abstract :
A robust, nonlinear tracking control strategy is presented for an aircraft equipped with synthetic jet actuators (SJA). The control law is designed to be easily implementable, requiring no observers, function approximators, or adaptive laws. By exploiting minimal knowledge of the structure of the nonlinear SJA dynamic model, a matrix decomposition technique is exploited to compensate for the input-multiplicative parametric uncertainty inherent in the SJA dynamics. The control law is shown to yield global asymptotic trajectory tracking in the presence of parametric uncertainty, actuator nonlinearity, and unknown, nonlinear external disturbances. A rigorous Lyapunov-based stability analysis is utilized to prove the theoretical result, and numerical simulation results are provided to demonstrate the performance of the proposed control law.
Keywords :
Lyapunov methods; actuators; aircraft control; compensation; control system synthesis; matrix decomposition; nonlinear control systems; position control; robust control; Lyapunov-based stability analysis; actuator nonlinearity; compensation; control law design; global asymptotic trajectory tracking; input-multiplicative parametric uncertainty; matrix decomposition technique; nonlinear SJA dynamic model; nonlinear external disturbances; numerical simulation; robust nonlinear aircraft tracking control; synthetic jet actuators; Aerospace control; Aircraft; Robustness; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control (CDC), 2013 IEEE 52nd Annual Conference on
Conference_Location :
Firenze
ISSN :
0743-1546
Print_ISBN :
978-1-4673-5714-2
Type :
conf
DOI :
10.1109/CDC.2013.6759885
Filename :
6759885
Link To Document :
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