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A new type of hybrid aircraft—the lifting-wing quadcopter, characterized by mechanical simplicity, robust wind resistance, low cruise speed, and reliable transition flight, is proposed. We designed a controller and verified its reliable transition flight, precise trajectory tracking, and energy-saving features through real flight experiments.

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This page is a summary of: Lifting-Wing Quadcopter Modeling and Unified Control, Journal of Guidance Control and Dynamics, March 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g008134.
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