LAboratory of Lightweight Aircrafts COndition Monitoring: integration of multimodal experimental data fusion and digital twin simulations

The project aims to create a physical and virtual laboratory for the monitoring and diagnosis of light aircraft. Heterogeneous measurements are processed through Data Fusion techniques and integrated with simulations of a Digital Twin. Data classification algorithms provide indicators of the aircraft’s health status to promptly identify any faults. The case study is an ultralight helicopter, for which a simplified test bench is created to validate the procedure.

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