二重推進式VTOLドローンの急上昇飛行に関する考察

抄録

In this paper, we examine the rapid ascent capability of a dual propulsion VTOL (Vertical Take-Off and Landing) drone based on its dynamic model. Through numerical optimization, we find the rapid ascent motion that maximizes altitude change within a specified flight duration. The optimization results show that employing both the rotors for rotary-wing mode and the rotor for fixed-wing mode allows for a greater ascent compared to conventional fixed-wing mode flight.