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This research article describes the development of a compact tilt-rotor unmanned aerial vehicle (UAV) that can perform vertical take-off and landing as well as high-speed cruise flight. The UAV uses a tricopter configuration with three coaxial rotors that can tilt to transition between rotor-mode and fixed-wing flight. Due to the multi-mode capability, controlling the UAV is challenging as it behaves as a nonlinear, multi-input/multi-output system. The researchers designed a control allocation method and au

Author

Arshia Moftakharihajimirzaei

Language

EN