基于科安德效应的无人机设计与控制

Jaehyeok Jeon, Hyoju Lee, Seonhye Han, HyunYong Lee, Choon-Joo Lee, Y. Kim, Hyoukryeol Choi
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引用次数: 2

摘要

本文提出了一种称为VTOL的无人机(UAV)。我们设计了无人机的整体形状。我们确定了飞行器的最佳表面形状和飞碟的宽高比。最后,我们建立了无人机和控制其飞行使用抗扭矩和襟翼链接。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design and control of an unmanned aerial vehicle (UAV) based on the Coandă effect
In this paper, we present an unmanned aerial vehicle (UAV) called VTOL. we designed the overall shape of the UAV. we determined the optimal surface shape of the vehicle and the ratio of width to height of the saucer. Finally, we built the UAV and controlled its flight using anti-torque and flap links.
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