Title :
Adaptive control of uncertain systems with gain scheduled reference models and constrained control inputs
Author :
Pakmehr, Mehrdad ; Yucelen, Tansel
Author_Institution :
Sch. of Aerosp. Eng., Georgia Inst. of Technol., Atlanta, GA, USA
Abstract :
This paper develops a new state feedback model reference adaptive control approach for uncertain systems with gain scheduled reference models in a multi-input multi-output (MIMO) setting with constrained control inputs. A single Lyapunov matrix is computed for multiple linearizations of the nonlinear closed-loop gain scheduled reference system, using convex optimization tools. This approach guarantees stability of the closed-loop gain scheduled reference model. Adaptive state feedback control architecture is then developed, and its stability is proven for the case with constrained control inputs. The resulting closed-loop system is shown to have bounded solutions with bounded tracking error, with the proposed stable gain scheduled reference model. Sufficient conditions for ultimate boundedness of the closed-loop system are derived. A semi-global stability result is proved with respect to the level of saturation for open-loop unstable plants while the stability result is shown to be global for open-loop stable plants. Simulation results show that the developed adaptive controller can be used effectively to control a degraded turboshaft engine for large thrust commands, with guaranteed stability and proper tracking performance.
Keywords :
MIMO systems; aerospace engines; closed loop systems; control system synthesis; convex programming; linearisation techniques; model reference adaptive control systems; nonlinear control systems; open loop systems; stability; state feedback; uncertain systems; Lyapunov matrix; MIMO setting; constrained control inputs; convex optimization tools; degraded turboshaft engine; linearizations; multi-input multi-output setting; nonlinear closed-loop gain scheduled reference system; open-loop stable plants; semi-global stability; state feedback model reference adaptive control approach; sufficient conditions; thrust commands; uncertain systems; Adaptation models; Adaptive control; Closed loop systems; Engines; Mathematical model; Stability analysis; Vectors; Aerospace; Constrained control; Control applications;
Conference_Titel :
American Control Conference (ACC), 2014
Conference_Location :
Portland, OR
Print_ISBN :
978-1-4799-3272-6
DOI :
10.1109/ACC.2014.6859326