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This paper applies an adaptive flight-control system on a 6DOF F-16 aircraft model, which demonstrates that a model-free approach to flight-control system design for rapid design and implementation can be used in niche applications.

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This page is a summary of: Adaptive Flight Control of an F-16 Without Prior Modeling, Journal of Guidance Control and Dynamics, July 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g009136.
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