关于无人机系统推进的实际问题

D. Lipcinski, M. Popa, C. Ilie, N. Tănase, D. Ovezea, Romulus Marian Mihai
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引用次数: 0

摘要

本文介绍了用于国家安全应用的无人驾驶飞行器(uav)的推进技术。本文介绍了推进系统的现状,重点介绍了无人机系统的电机领域,强调了对这些系统的贡献,并提出了双励磁发电机的技术解决方案。最后,对自备多旋翼飞机(HOVER)配电系统的热特性进行了实验研究。我们的研究结果在选择无人机系统的电源线和电源类型方面证明是有用的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Practical Aspects Regarding the Propulsion of UAV Systems
This paper presents certain technological aspects regarding the propulsion of unmanned aerial vehicles (UAVs), which are dedicated to national security applications. The paper presents the current state of propulsion systems, focused on the field of electric machines for UAV systems, highlighting the contribution to these systems as well as presenting a technological solution of a dual excitation generator. In the last part of the paper, an experimental study is presented regarding the thermal behavior of the power distribution system of a captive multicopter (HOVER). Our results prove useful in choosing the type of power cables and power sources for UAV systems.
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