DocumentCode :
3025373
Title :
Towards faster, smoother, and more compact fuzzy approximation, with an application to non-destructive evaluation of space shuttle´s structural integrity
Author :
Yam, Yeung ; Osegueda, Roberto ; Kreinovich, Vladik
Author_Institution :
Dept. of Mech. & Autom. Eng., Chinese Univ. of Hong Kong, Shatin, Hong Kong
fYear :
1999
fDate :
36342
Firstpage :
243
Lastpage :
247
Abstract :
It is known that fuzzy systems are universal approximators, i.e., any input-output system can be approximated, within any given accuracy, by a system described by fuzzy rules. Fuzzy rules work well in many practical applications. However, in some applications, the existing fuzzy rule approximation techniques are not sufficient. First, in many practical problems (e.g., in many control applications), derivatives of the approximated function are very important, and so, we want not only the approximating function to be close to the approximated one, but we also want their derivatives do be close; however, standard fuzzy approximation techniques do not guarantee the accuracy of approximating a derivative. Second, to get the desired approximation accuracy, we sometimes need unrealistically many rules. We show how both problems can be solved
Keywords :
aerospace computing; extrapolation; function approximation; fuzzy logic; fuzzy systems; space vehicles; structural engineering computing; extrapolation; function approximation; fuzzy approximation; fuzzy rule approximation techniques; fuzzy systems; nondestructive evaluation; space shuttle structural integrity; universal approximators; Aerospace engineering; Automatic control; Extrapolation; Fuzzy control; Fuzzy systems; Image reconstruction; Nondestructive testing; Space shuttles; Space technology; Stress;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Fuzzy Information Processing Society, 1999. NAFIPS. 18th International Conference of the North American
Conference_Location :
New York, NY
Print_ISBN :
0-7803-5211-4
Type :
conf
DOI :
10.1109/NAFIPS.1999.781691
Filename :
781691
Link To Document :
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