Several advances have been made in the recent years in the integration of Structural Health Monitoring (SHM) systems within Structural Integrity (SI) management. The current state-of-the-art Airbus Defence and Space (ADS) SHM System relies on both an analytical elastic wave propagation model and a Dynamic Distributed Fibre Optics Sensing (DFOS) Environmental and Operational Conditions (EOC) measurement and compensation model. This hybrid SHM system is able to properly diagnose mechanical impacts (events) and resulting damages that may occur during aircraft operation, while accounting for punctual alterations in the structure due to changes in ambient temperature or pressure. In this paper, a demonstrative application of this system is presented for the diagnosis of a Bird Strike Test Event. The test has been carried out in controlled conditions for a hybrid metal-composite fuselage cockpit structure, within the scope of CS2 PASSARO EU program. The results show the reliability of the ADS SHM system for supervised conditions.
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