The results prove that it is aerodynamically efficient for our purpose. Furthermore, 3D model of the V-TS mini-UAV with the Y-tail configuration and its basic geometrical parameters are shown. AVIGLE Demonstrator is analyzed in SU 2 to verify correct settings of the aerodynamic analysis. Free software which was used in the design process is presented and described. However, this configuration also brings new challenges and difficulties, especially in the case of control. Since the V-TS mini-UAV is a combination of airplanes and copters, high energy efficiency during the forward flight and VTOL capability in the hover flight are achieved. This paper describes progress made on the design and analysis of a twin-propeller tail-sitter mini-UAV (named V-TS).
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