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The paper proposes aeroelastic system identification with multi-output autoregressive models that concurrently account for multiple measured data (as strains measured in optical fibers or accelerations). The proposed modeling approaches are tested with wind-tunnel data. They provide smooth identification of the aeroelastic frequencies and damping values, which lead to accurate flutter onset identification.

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This page is a summary of: Aeroelastic System Identification for Flutter Prediction via Multi-Output Autoregressive Modeling, Journal of Aircraft, December 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c037477.
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