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If a piloted aircraft design is particularly susceptible to pilot-induced oscillations, it can lead to poor handling qualities and even safety hazards. This work details a machine learning-based control design that can reduce pilot-induced oscillation tendencies due to a variety of factors.

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This page is a summary of: Model Reference Control for Reducing Pilot-Induced Oscillation Tendencies, Journal of Guidance Control and Dynamics, February 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g008400.
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