论文标题
固定在多轨无人机上的起重机翼，用于长飞行范围
A Lifting Wing Fixed on Multirotor UAVs for Long Flight Ranges
论文作者
论文摘要
本文提出了一个驾驶翼多旋翼无人机，可允许远程飞行。无人机以特殊的安装角度具有起重机翼，与传统的多旋风无人机相比，飞行时可以与转子一起使用，以供应升降机，从而降低能源消耗和飞行范围的改善。它的动态模型是根据经典的多轨道理论和固定翼理论构建的，因为其多个螺旋桨的空气动力学和起重机翼的空气动力学几乎被脱钩。它的设计考虑了空气动力学，机身配置和安装角度。通过实验验证了无人机的性能，这表明当无人机以巡航速度（15m/s）飞行时，举重翼可节省50.14％的功率。
This paper presents a lifting-wing multirotor UAV that allows long-range flight. The UAV features a lifting wing in a special mounting angle that works together with rotors to supply lift when it flies forward, achieving a reduction in energy consumption and improvement of flight range compared to traditional multirotor UAVs. Its dynamic model is built according to the classical multirotor theory and the fixed-wing theory, as the aerodynamics of its multiple propellers and that of its lifting wing are almost decoupled. Its design takes into consideration aerodynamics, airframe configuration and the mounting angle. The performance of the UAV is verified by experiments, which show that the lifting wing saves 50.14% of the power when the UAV flies at the cruise speed (15m/s).
