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首页> 外文期刊>CEAS Aeronautical Journal >Conceptual design and control of twin-propeller tail-sitter mini-UAV
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Conceptual design and control of twin-propeller tail-sitter mini-UAV

机译：双螺旋桨尾桨小型无人机的概念设计与控制

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This paper describes progress made on the design and analysis of a twin-propeller tail-sitter mini-UAV (named V-TS). 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. However, this configuration also brings new challenges and difficulties, especially in the case of control. Free software which was used in the design process is presented and described. AVIGLE Demonstrator is analyzed in SU2 to verify correct settings of the aerodynamic analysis. Furthermore, 3D model of the V-TS mini-UAV with the Y-tail configuration and its basic geometrical parameters are shown. The results prove that it is aerodynamically efficient for our purpose. In addition, probably all control modes, transitional flight phases, and difficulties which appear in the control of the twin-propeller tail-sitter mini-UAV are defined and solutions are proposed. The transitional flight phases are determined as a combination of the control modes and sub-modes.
机译：本文介绍了双螺旋桨尾桨微型无人机（命名为V-TS）的设计和分析进展。由于V-TS mini-UAV是飞机和直升飞机的组合，因此可以实现前向飞行时的高能效和悬停飞行时的VTOL能力。但是，这种配置也带来了新的挑战和困难，特别是在控制的情况下。介绍并描述了设计过程中使用的免费软件。在SU2中对AVIGLE Demonstrator进行了分析，以验证空气动力学分析的正确设置。此外，还显示了具有Y型尾部配置的V-TS mini-UAV的3D模型及其基本几何参数。结果证明，对于我们的目的，它在空气动力学方面是有效的。此外，可能定义了所有控制模式，过渡飞行阶段以及在双螺旋桨尾桨小型微型无人机的控制中出现的困难，并提出了解决方案。过渡飞行阶段被确定为控制模式和子模式的组合。

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