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
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