| 摘要 |
The present invention relates to an unmanned aerial vehicle having delta wings and joined wings. According to the unmanned aerial vehicle of the present invention, a pair of joined wings are connected to a wingtip of a pair of delta wings connected to both sides of a fuselage so as to increase endurance through high-lifting and resistance and high efficiency and to improve very excellent flight performance at various speed zones and short take-off and landing performance. An elevon including a rudder is comprised between a rear part of the fuselage and a lower part of the joined wing. A pairing for both a reconnaissance camera installation space and an airplane throwing handle is comprised at a center of a lower part of the fuselage. |
