DocumentCode
3568306
Title
Robust adaptive tracking control of delta wing vortex-coupled roll dynamics subject to delay and SMA actuator dynamics
Author
Pakmehr, Mehrdad ; Gordon, Brandon W. ; Rabbath, C.A.
Author_Institution
Dept. of Mech. Eng., Concordia Univ., Montreal, Que., Canada
Volume
2
fYear
2005
Firstpage
980
Abstract
In this paper, a feedback control strategy for stabilizing vortex-coupled delta wing roll dynamics with state delay and parameter uncertainty in the rolling moment coefficient relying on a robust adaptive tracking neuro-controller, which employs a network of Gaussian radial basis functions (RBF) to adaptively compensate for the rolling moment coefficient, is proposed. The stabilizing controller is shown to render the control system globally practically stable, whereas the robust adaptive tracking neuro-controller provides satisfactory tracking performance. The rolling moment coefficient, as a function of left and right vortex breakdown positions, is estimated online in an adaptive neuro-controller structure using a special feature of RBF networks for the delta wing case. The numerical simulation illustrates the applicability of the developed controller.
Keywords
Gaussian processes; adaptive control; aerospace computing; aircraft control; control engineering computing; delay systems; feedback; intelligent actuators; neurocontrollers; radial basis function networks; robust control; tracking; uncertain systems; vehicle dynamics; Gaussian radial basis functions; SMA actuator dynamics; applied nonlinear control; delta wing vortex-coupled roll dynamics; feedback control; parameter uncertainty; robust adaptive tracking neurocontroller; stabilizing controller; state delay; Actuators; Adaptive control; Control systems; Delay; Electric breakdown; Feedback control; Programmable control; Radial basis function networks; Robust control; Uncertain systems;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation, 2005 IEEE International Conference
Print_ISBN
0-7803-9044-X
Type
conf
DOI
10.1109/ICMA.2005.1626685
Filename
1626685
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