2026
Design and Control of a Coaxial Dual-Rotor Reconfigurable Tailsitter UAV Based on Swashplateless Mechanism
RA-L 2026
The tailsitter vertical takeoff and landing (VTOL) UAV is widely used due to its lower dead weight, which eliminates the actuators and mechanisms for tilting. However, the tailsitter UAV is susceptible to wind disturbances in multi-rotor mode, as it exposes a large frontal fuselage area. To address