Title :
Pattern recognition for nondestructive evaluation
Author :
Amirfathi, M.M. ; Morris, S. ; O´Rorke, P. ; Bond, W.E. ; St.Clair, D.C.
Author_Institution :
Douglas Aircraft Co., Long Beach, CA, USA
Abstract :
The issues involved in automating nondestructive evaluation (NDE) techniques are outlined. Attention is given to research focused on the application of machine learning techniques to the construction and maintenance of knowledge-based systems which are capable of evaluating the readings from nondestructive tests that have been performed on aircraft components. Preliminary results obtained from this research are described. In particular, the authors discuss the application of a symbolic machine learning algorithm, ID3, to the NDE problem. ID3 has been used by Douglas Aircraft to classify defects in sets of standard NDE reference blocks. Based on the preliminary results, a need for an improved method of distinguishing features in the test waveforms is identified. The authors also outline a feature extraction approach from pattern recognition, called scale-space filtering, which can be used to preprocess data for input into a classification algorithm such as ID3.<>
Keywords :
automatic testing; computerised pattern recognition; knowledge based systems; learning systems; mechanical engineering computing; nondestructive testing; A-scan; Douglas Aircraft; NDT; aircraft components; artificial intelligence; classification algorithm; composite materials; data preprocessing; feature extraction; knowledge-based systems; nondestructive evaluation; nondestructive tests; pattern recognition; scale-space filtering; symbolic machine learning algorithm; test waveforms; Aircraft manufacture; Feature extraction; Filtering; Knowledge based systems; Machine learning; Machine learning algorithms; Nondestructive testing; Pattern recognition; Performance evaluation; System testing;
Conference_Titel :
Aerospace Applications Conference, 1991. Digest., 1991 IEEE
Conference_Location :
Crested Butte, CO, USA
Print_ISBN :
0-87942-686-1
DOI :
10.1109/AERO.1991.154534