DocumentCode :
1368952
Title :
Adaptive Output Feedback Design Using Asymptotic Properties of LQG/LTR Controllers
Author :
Lavretsky, Eugene
Author_Institution :
Boeing Co., Huntington Beach, CA, USA
Volume :
57
Issue :
6
fYear :
2012
fDate :
6/1/2012 12:00:00 AM
Firstpage :
1587
Lastpage :
1591
Abstract :
This technical note introduces an observer-based adaptive output feedback tracking control design for multi-input-multi-output dynamical systems with matched uncertainties. The reported methodology exploits asymptotic behavior of LQG/LTR regulators. Sufficient conditions for closed-loop stability and uniform ultimate boundedness of the corresponding tracking error dynamics are formulated. This method is valid for systems whose nominal linearized dynamics are controllable and observable. We assume that the number of the system measured outputs (sensors) is greater than the number of the control inputs (actuators) and that the system output-to-input matrix product has full column rank. In this case, the system can be “squared-up” (i.e., augmented) using pseudo-control signals to yield relative degree one minimum-phase dynamics. Since it is known that the “squaring-up” problem is solvable for any controllable observable triplet (A, B, C), the proposed design is applicable to systems whose regulated output dynamics may be non-minimum phase or have a high relative degree. A simulation example is presented to demonstrate key design features.
Keywords :
MIMO systems; adaptive control; aerospace control; asymptotic stability; closed loop systems; control system synthesis; feedback; linear quadratic Gaussian control; linearisation techniques; matrix multiplication; observers; uncertain systems; LQG/LTR controllers; LQG/LTR regulators; MIMO system; asymptotic properties; closed loop stability; controllable observable triplet; full column rank; linearized dynamics; matched uncertainties; minimum-phase dynamics; multiple-input multiple-output dynamical systems; nonminimum phase; observer-based adaptive output feedback tracking control design; pseudocontrol signals; squaring-up problem; sufficient conditions; system output-to-input matrix product; tracking error dynamics; uniform ultimate boundedness; Aerodynamics; Control design; Observers; Output feedback; Uncertainty; Vehicle dynamics; Vehicles; Flight control; optimal and adaptive control; output feedback;
fLanguage :
English
Journal_Title :
Automatic Control, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9286
Type :
jour
DOI :
10.1109/TAC.2011.2174692
Filename :
6069834
Link To Document :
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