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Sbarufatti, Claudio
in Cooperation with on an Cooperation-Score of 37%
Topics
- modeling
- helicopter
- qualification
- fatigue cracking
- structural health monitoring system
- assessment
- estimate
- landing
- chemical element
- behavior
- maintenance
- monitoring
- validation
- altitude
- synthetic
- system safety
- fuselage
- algorithm
- velocity
- neural network
- sensor
- face
- filtration
- strain gage
- bird
- bird strike
- honeycomb structure
- impact test
- aircraft
- health
- structural health monitoring
- cracking
- aluminum
- optimisation
- data
- estimating
- diagnosis
- alarm system
- strain measurement
- show 9 more
Publications
- 2017Analysis of a helicopter main gearbox by means of numerical modelling approach
- 2016Model-Assisted performance qualification of a distributed SHM system for fatigue crack detection on a helicopter tail boom
- 2016Experimental validation of a computational hybrid methodology to estimate fuselage damage due to harsh landingcitations
- 2015Model-based structural integrity assessment of helicopter fuselage during harsh landing
- 2015Low-velocity impact monitoring system for a helicopter frame by means of an artificial neural network
- 2013MEMS for structural health monitoring in aircraftcitations
- 2013Helicopter harsh landing events: A computational hybrid methodology to estimate fuselage damagecitations
- 2013Artificial neural networks for structural health monitoring of helicopter harsh landingscitations
- 2012Diagnostic system validation for damage monitoring of helicopter fuselage
- 2012ANN based Bayesian hierarchical model for crack detection and localization over helicopter fuselage panels
- 2011Sensor network optimization for damage detection on aluminium stiffened helicopter panels
- 2010Probability of detection and false alarms for metallic aerospace panel health monitoring
Places of action
booksection
MEMS for structural health monitoring in aircraft
Topics
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