NASA NTRS · 19920046624
A system identification model for adaptive nonlinear control
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 as an artificial neural network, is considered. The results of an application of the identification techniques to a nonlinear transport aircraft model are presented.
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Linse, Dennis J., Stengel, Robert F.. 1991-01-01. A system identification model for adaptive nonlinear control. https://ntrs.nasa.gov/citations/19920046624
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