鹦鹉微型无人机螺旋桨尺寸的改进及其对飞控系统的影响研究

E. H. Kadhim, A. Abdulsadda
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引用次数: 1

摘要

无人驾驶飞行器(uav)广泛应用于运输、交付、监视和监视等领域。基于湍流和乱流的稳定、弹性和精确飞行的发展将可能成为开发独特飞行控制系统的关键特征。在本次研究中,我们研究了一种小型Parrot迷你无人机——Mambo无人机的控制系统,使用MATLAB程序进行了设计,同时我们在设计中通过改变原飞机的重量来增加无人机的湍流,其中我们增加了重量,并多次计算了飞机螺旋桨的垂直投影面积,直到我们得到了最好的空间,让螺旋桨能够承载更多的额外重量。我们增加了无人机的重量,因为飞机在飞行过程中遇到了恶劣的条件,比如下雪或灰尘落在它身上。为了使飞机能够承受这些天气条件而不坠落和碰撞,我们计算了飞机机翼面积的适当增加,并将其实际应用于MATLAB-R2021a Simulink程序中,并在实验室内进行了仿真和实时应用,得到了良好的结果,仿真程序中加入了湍流。螺旋桨的新设计证明了飞机携带大约三分之一飞机重量的额外有效载荷的能力,如道路章节所示。在未来的工作中,我们建议将这种设计应用于带有固定螺旋桨的大型飞机上,并研究其他天气条件对无人机的影响,例如温度、湿度等的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Improving the Size of the Propellers of the Parrot Mini-Drone and an Impact Study on its Flight Controller System
Unmanned Aerial Vehicles (UAVs) are widely used in transportation, delivery, surveillance and surveillance applications. The development of stable, resilient, and accurate flight based on turbulence and turbulence will likely become a key feature in the development of unique flight control systems. In this research, we studied the control system of a small Parrot mini drone, the Mambo drone, which was designed using the MATLAB program, while we added turbulence to the drone by changing the weight of the original plane in the design, where we increased the weight and calculated the vertical projection area of the propellers of the plane several times until we got the best space for the propellers able to carry more extra weight. We imposed an increase in the drone's weight due to bad conditions that the plane experienced during its flight, such as snow or dust falling on it. In order to make the aircraft bear these weather conditions without falling and colliding, we calculated an appropriate increase in the area of the aircraft wing, and we actually applied it in the MATLAB-R2021a Simulink program, and we got good results using simulation as well as in real-time inside the laboratory, turbulence was added in the simulation program. The new design of the propellers demonstrated the aircraft's ability to carry an additional payload of approximately one-third of the aircraft's weight, as shown in the roads chapter. In future work, we propose to use this design on larger aircraft with fixed propellers and to study the effects of other weather conditions on UAVs, such as the effect of temperature, humidity, and others.
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