Spincopter Wing Design and Flight Control (CROSBI ID 185958)
Prilog u časopisu | izvorni znanstveni rad | međunarodna recenzija
Podaci o odgovornosti
Orsag, Matko ; Ćesić, Josip ; Haus, Tomislav ; Bogdan, Stjepan
engleski
Spincopter Wing Design and Flight Control
This paper presents dynamical properties of an unmanned aerial vehicle (UAV), called spincopter. The vehicle structure is based on two wings that are forced in rotation (spinning) by propulsion system formed of two propellers. Based on devised dynamical model, that reveals inherent stability of the vehicle, composition of control algorithms for vertical and horizontal movement is proposed. Due to the specific configuration of the propulsion system, movement in horizontal direction is produced by pulsations in rotational speed of propulsion motors. An analysis of influence that such a configuration has on the vehicle dynamics is given. Finally, design recommendations for rotational wings are elaborated, based on extensive simulations of spincopter by using X-Plane® software package.
UAV; rotorcraft; control; aerodynamics
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Podaci o izdanju
70 (1/4)
2013.
165-179
objavljeno
0921-0296
10.1007/s10846-012-9725-2