DocumentCode :
2201846
Title :
Comparison of contemporary adaptive control design techniques
Author :
Sorrells, J.
fYear :
1989
fDate :
26-28 Mar 1989
Firstpage :
636
Lastpage :
640
Abstract :
A benchmark design problem is formulated and used as a common test bed for the evaluation of specific adaptive controller design techniques. The baseline problem is a common system that is frequently encountered in aerospace applications. A classical proportional-integral-derivative controller is designed and used as a metric for judging the adaptive controllers. The controllers are compared in terms of performance capabilities, operating robustness, and design complexity
Keywords :
adaptive control; control system synthesis; performance index; stability; PID controller; adaptive control design techniques; aerospace applications; benchmark design problem; classical proportional-integral-derivative controller; design complexity; operating robustness; performance capabilities; Adaptive control; Aerodynamics; Control systems; Missiles; Performance analysis; Poles and zeros; Programmable control; Tail; Transfer functions; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
System Theory, 1989. Proceedings., Twenty-First Southeastern Symposium on
Conference_Location :
Tallahassee, FL
ISSN :
0094-2898
Print_ISBN :
0-8186-1933-3
Type :
conf
DOI :
10.1109/SSST.1989.72545
Filename :
72545
Link To Document :
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