DocumentCode :
488985
Title :
A System Identification Model for Adaptive Nonlinear Control
Author :
Linse, Dennis J. ; Stengel, Robert F.
Author_Institution :
Graduate Research Assistant, Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ 08544
fYear :
1991
fDate :
26-28 June 1991
Firstpage :
1752
Lastpage :
1757
Abstract :
A system identification model that combines generalized-spline function approximation with a nonlinear control system is described. The complete control system contains three main elements: a nonlinear-inverse-dynamic control law that depends on a comprehensive model of the plant, a state estimator whose outputs drive the control law, and a function approximation scheme that models the system dynamics. The system-identification task, which combines an extended Kalman filter with a function approximator modeled here as an artificial neural network, is considered in detail. The state estimator provides the necessary data so that continuous training of the neural network is possible during normal operation. The results of an application of the identification techniques to a nonlinear transport aircraft model are presented.
Keywords :
Adaptive control; Aircraft; Artificial neural networks; Control system synthesis; Function approximation; Nonlinear control systems; Nonlinear dynamical systems; Programmable control; State estimation; System identification;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1991
Conference_Location :
Boston, MA, USA
Print_ISBN :
0-87942-565-2
Type :
conf
Filename :
4791685
Link To Document :
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