DocumentCode :
1930366
Title :
Controller design via adaptive critic and model reference methods
Author :
Lendaris, George G. ; Santiago, Roberto ; McCarthy, Jay ; Carroll, Michael
Author_Institution :
Dept. of Electr. & Comput. Eng., Portland State Univ., OR, USA
Volume :
4
fYear :
2003
fDate :
20-24 July 2003
Firstpage :
3173
Abstract :
Dynamic programming (DP) is a principled way to design optimal controllers for certain classes of nonlinear systems; unfortunately, DP is computationally very expensive. The reinforcement learning methods known as adaptive critics (AC) provide computationally feasible means for performing approximate dynamic programming (ADP). The term \´adaptive\´ in AC refers to the critic improved estimations of the value function used by DP. To apply DP, the user must craft a Utility function that embodies all the problem-specific design specifications/criteria. Model reference adaptive control methods have been successfully used in the control community to effect on-line redesign of a controller in response to variations in plant parameters, with the idea that the resulting closed loop system dynamics will mimic those of a reference model. The work (1) uses a reference model in ADP as the key information input to the Utility function, and (2) uses ADP off-line to design the desired controller Future work will extend this to on-line application. This method is demonstrated for a hypersonic shaped airplane called LoFLYTE®; its handling characteristics are natively a little "hotter" than a pilot would desire. A control augmentation subsystem is designed using ADP to make the plane "feel like" a better behaved one, as specified by a reference model. The number of inputs to the successfully designed controller are among the largest seen in the literature to date.
Keywords :
aircraft control; control system synthesis; dynamic programming; learning (artificial intelligence); model reference adaptive control systems; nonlinear control systems; optimal control; LoFLYTE; adaptive critics; closed loop system dynamics; control augmentation subsystem; dynamic programming; hypersonic shaped airplane; model reference adaptive control methods; nonlinear systems; on-line redesign; optimal controller design; plant parameters; reinforcement learning; utility function; value function; Adaptive control; Airplanes; Closed loop systems; Control systems; Dynamic programming; Learning; Nonlinear control systems; Nonlinear systems; Optimal control; Programmable control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Neural Networks, 2003. Proceedings of the International Joint Conference on
ISSN :
1098-7576
Print_ISBN :
0-7803-7898-9
Type :
conf
DOI :
10.1109/IJCNN.2003.1224080
Filename :
1224080
Link To Document :
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