Development of a Novel Water Landing UAV with Deflatable Floater

Yiyun Bai, Ju-Hyeon Hong, A. Zolotas
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引用次数: 2

Abstract

A novel design of amphibious UAV with a swimming-ring shaped floater that can inflate before landing and deflate after taking off is presented. An air pump system is developed to control the floater and is integrated in the whole flight control system. The mechanism of such system is discussed, while simulations in MATLAB and Simulink carried out for a UAV with simple missions and trajectories are shown. Results illustrate the feasibility of using the proposed design within the remit of water landing UAVs.
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一种新型可充气浮筒水上降落无人机的研制
提出了一种新型水陆两栖无人机的设计方案,该方案采用了一种可在着陆前充气、起飞后放气的浮圈式飞行器。开发了一种气泵系统来控制浮子,并将其集成到整个飞行控制系统中。讨论了该系统的工作机理,并在MATLAB和Simulink中对具有简单任务和轨迹的无人机进行了仿真。结果表明,在水上着陆无人机的范围内使用所提出的设计是可行的。
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