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This paper describes a methodology used to create a mathematical model for electric vertical takeoff and landing (eVTOL) aircraft using data gathered in flight testing. The methodology is developed with a discussion of unique eVTOL vehicle attributes and practical strategies intended to inform future flight-based model development efforts for eVTOL aircraft.

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This page is a summary of: System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data, Journal of Aircraft, February 2023, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c036896.
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