Rotary Wing UAV Modeling and Control: A Design Application

Erol Duymaz, A. E. Oğuz
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Abstract

Great progress has been made in the use of Unmanned Aerial Vehicles (UAVs) in recent years, and it is now possible to see UAVs not only in military and industrial applications but also in every field, from education to logistics and visual arts. On the other hand, experimental platform problems for control theory applications in electrical-electronics, mechatronics and control engineering departments in engineering faculties are occasionally noticeable from time to time. In this study, a UAV modeling and control approach is proposed for control design application in undergraduate engineering education. UAV modeling was carried out in a simulation environment, and PD (proportional-derivative) control application was carried out on a sample platform along with simulation experiments. After theoretical discussions, it has been seen that it is possible to use the proposed UAV system control as a low-cost control design application tool in both simulation environments and experimental environments.
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旋转翼无人机建模与控制:设计应用
近年来,无人驾驶飞行器(UAV)的应用取得了长足的进步,现在不仅在军事和工业领域,而且在教育、物流和视觉艺术等各个领域都可以看到无人驾驶飞行器的身影。另一方面,工科院校电气电子学、机电一体化和控制工程系的控制理论应用实验平台问题时有发生。本研究提出了一种无人机建模与控制方法,用于本科工程教育中的控制设计应用。无人机建模在仿真环境中进行,PD(比例-派生)控制应用在样本平台上与仿真实验一起进行。经过理论讨论,可以看出在仿真环境和实验环境中都可以将所提出的无人机系统控制作为一种低成本的控制设计应用工具。
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