DocumentCode :
905020
Title :
Robust control for high-performance materials testing
Author :
Bailey, F.N. ; Cockburn, J.C. ; Dee, A.
Author_Institution :
Dept. of Electr. Eng., Minnesota Univ., Minneapolis, MN, USA
Volume :
12
Issue :
2
fYear :
1992
fDate :
4/1/1992 12:00:00 AM
Firstpage :
63
Lastpage :
70
Abstract :
The use of root-locus-based robust design techniques in the design of a digital controller for a high-performance variable-amplitude fatigue test is described. Evaluation of the resulting controller on a prototype laboratory materials testing system, designed to simulate the mechanical stress loads experienced by certain aircraft components, shows that it meets design performance goals of 0.25% specimen load accuracy while providing robustness to specimen compliance over a 10 to 1 range. This performance significantly exceeds that obtained with traditional hand-tuned controllers.<>
Keywords :
aerospace test facilities; automatic testing; computerised instrumentation; digital control; fatigue testing; laboratory apparatus and techniques; materials testing; root loci; stability; aircraft components; digital controller; high-performance materials testing; high-performance variable-amplitude fatigue test; mechanical stress loads; robust control; root-locus-based robust design techniques; specimen compliance robustness; specimen load accuracy; Aerospace control; Aircraft; Digital control; Fatigue; Laboratories; Materials testing; Mechanical variables control; Robust control; Stress control; Virtual prototyping;
fLanguage :
English
Journal_Title :
Control Systems, IEEE
Publisher :
ieee
ISSN :
1066-033X
Type :
jour
DOI :
10.1109/37.126857
Filename :
126857
Link To Document :
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