Title :
A nonlinear dynamic inversion Predictor-Based Model Reference Adaptive Controller for a Generic Transport Model
Author :
Campbell, S.F. ; Kaneshige, J.T.
Author_Institution :
SGT Inc., Greenbelt, MD, USA
fDate :
June 30 2010-July 2 2010
Abstract :
Presented here is a Predictor-Based Model Reference Adaptive Control (PMRAC) architecture for a generic transport aircraft. At its core, this architecture features a three-axis, non-linear, dynamic-inversion controller. Command inputs for this baseline controller are provided by pilot roll-rate, pitch-rate, and sideslip commands. This paper will first thoroughly present the baseline controller followed by a description of the PMRAC adaptive augmentation to this control system. Results are presented via a full-scale, nonlinear simulation of NASA´s Generic Transport Model (GTM).
Keywords :
aircraft; model reference adaptive control systems; nonlinear control systems; predictive control; NASA generic transport model; adaptive augmentation; baseline controller; dynamic-inversion controller; generic transport aircraft; nonlinear controller; pilot roll-rate; pitch-rate; predictor-based model reference adaptive controller; sideslip commands; three-axis controller; Adaptive control; Aerodynamics; Aerospace control; Aircraft; Control system synthesis; Control systems; NASA; Nonlinear dynamical systems; Predictive models; Programmable control;
Conference_Titel :
American Control Conference (ACC), 2010
Conference_Location :
Baltimore, MD
Print_ISBN :
978-1-4244-7426-4
DOI :
10.1109/ACC.2010.5530683
