开放射流风洞中风湍流条件下四旋翼飞行和电池消耗评估

M. N. Elya, M. Z. Jurij, M. R. Saad, S. Azrad
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摘要

本文介绍了风湍流条件下四旋翼飞行的电池消耗结果。这项研究是在一个开放式射流风洞中进行的。在开式射流风洞的排气部分研制了运动捕捉系统。动作捕捉系统包括安装在风洞排气部分外的6台光学跟踪摄像机,以及地面站的一台PC机。使用两种尺寸的LiPo可充电电池,分别为5200 mAH,放电率为30℃和4200 mAH,放电率为40℃,以评估四旋翼飞行器的电池消耗和飞行性能。结果表明,与5200 mAH电池相比,4200 mAH电池的性能更好(悬停时的稳态误差更小)。为了克服湍流,四旋翼螺旋桨必须快速行动,因此4200毫安时电池的更高放电率提供了更好的性能,因为它使四旋翼盘旋在接近所需的设定点。
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Evaluation of Quadrotor Flight and Battery Consumption under Wind Turbulence conditions in an Open-Jet Wind Tunnel
This paper presents the results of battery consumption for quadrotor flight under wind turbulence conditions. The study was performed in an open-jet wind tunnel. A motion capture system was developed at the exhaust part of the open-jet wind tunnel. The motion capture system comprised 6 optitrack cameras installed outside the exhaust part of the wind tunnel, and a PC at the ground station. A LiPo rechargeable battery was used, with two sizes, namely 5200 mAH with a discharge rate of 30 C and 4200 mAH with a discharge rate of 40 C, to evaluate the quadrotor's battery consumption and flight performance. The results show that the 4200 mAH battery performed better (with a smaller steady-state error during hovering) compared to the 5200 mAH battery. To overcome turbulence, the quadrotor propellers have to act fast, so the higher discharge rate from 4200 mAH battery gave better performance, as it kept the quadrotor hovering in close proximity to the desired setpoint.
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