(continued from number 2 page 323-343) This paper concerns the second phase of an experimental validation Programme for a structural health monitoring methodology based on novelty detection. This phase seeks to apply one of the methods considered in the first stage of the work on a more realistic structure, namely the wing of a Gnat aircraft, as opposed to the previously investigated laboratory structure. The novelty detection algorithm used is that of outlier analysis and damage is introduced by making several copies of an inspection panel, each with a different controlled fault. All of these faults were detectable, a single feature was highlighted which proved capable of separating all the fault conditions from the unfaulted. (to be continued)
Experimental validation of a structural health monitoring methodology: Part 2. Novelty detection on a gnat aircraft
Experimentelle Überprüfung einer Methode zur Strukturstabilitäts-Überwachung: Teil 2. Neuartige Detektionsmethode, angewandt an einem Millitärflugzeug
Journal of Sound and Vibration ; 259 , 2 ; 345-363
2003
19 Seiten, 15 Bilder, 4 Tabellen, 6 Quellen
Aufsatz (Zeitschrift)
Englisch
Engineering Index Backfile | 1958