Minimizing Fatigue Damage in Aircraft Structures
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[1] Ari Visa,et al. Link between Flight Maneuvers and Fatigue , 2011 .
[2] J. A. Tikka. Flight parameter based fatigue analysis approach for a fighter aircraft , 2008 .
[3] Keith Worden,et al. Experimental validation of a structural health monitoring methodology: Part III. Damage location on an aircraft wing , 2003 .
[4] S. Chiba,et al. Dynamic programming algorithm optimization for spoken word recognition , 1978 .
[5] Riccardo Poli,et al. A Field Guide to Genetic Programming , 2008 .
[6] Ari Visa,et al. Reasoning logical rules from multisensor data for lifecycle management of aircraft structures , 2013, 2013 IEEE Congress on Evolutionary Computation.
[7] Keith Worden,et al. Genetic optimisation of a neural damage locator , 2008 .
[8] S. C. Reed,et al. Development of a parametric-based indirect aircraft structural usage monitoring system using artificial neural networks , 2007, The Aeronautical Journal (1968).
[9] M. Bodruzzaman,et al. Decision fusion methodologies in Structural Health Monitoring systems , 2012, 2012 Proceedings of IEEE Southeastcon.
[10] Ari Visa,et al. A Novel Algorithm for Identifying Patterns from Multisensor Time Series , 2009, 2009 WRI World Congress on Computer Science and Information Engineering.
[11] H Azzam. A practical approach for the indirect prediction of structural fatigue from measured flight parameters , 1997 .
[12] J. Ross Quinlan,et al. Induction of Decision Trees , 1986, Machine Learning.
[13] Fu-Kuo Chang,et al. Encyclopedia of structural health monitoring , 2009 .