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Hybrid unmanned air vehicles, which combine vertical takeoff and landing capability with a wing for efficient forward flight, can offer benefits over traditional drones in terms of speed and range. We propose a control strategy that can cope with these vehicles' complicated aerodynamics, with very limited modeling.

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This page is a summary of: Incremental Control and Guidance of Hybrid Aircraft Applied to a Tailsitter Unmanned Air Vehicle, Journal of Guidance Control and Dynamics, February 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g004520.
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