悬停鞘翅的稳定性

2018 XIII International Scientific Conference - New Trends in Aviation Development (NTAD) Pub Date : 2018-08-01 DOI:10.1109/NTAD.2018.8551686

S. Fábry, P. Tulipán, P. Gašparovič

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引用次数: 1

摘要

介绍了一种单旋翼垂直起降(VTOL)无人机。为了处理成功的飞行，必须解决与多旋翼无人机相比的几个差异。以保持稳定悬停为目标，研究几何、作用力和力矩。建议使用稳定系统，以使操作员能够将注意力集中在主要飞行任务上。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Stability of a Hovering Coleoptere

Single rotor vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV) is described. Severaldifferences in comparison to multirotor UAV have to be solved to handle succesfull flight. Geometry, acting forces and moments are investigated with goal to keep stable hovering. Stabilization system is recommended for freeing operators attention to the main flight task.

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2018 XIII International Scientific Conference - New Trends in Aviation Development (NTAD)

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