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A computer model was developed for a coaxial rotorcraft by combining the physics-based system knowledge with flight data. The resulting model accurately reflects the rotorcraft’s behavior during flight.

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This page is a summary of: Higher-Order System Identification and Control Design for a Coaxial Rotorcraft, Journal of Aircraft, April 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c038157.
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