A Concept for Application of Hall Sensors in Measurement of Magnetic Field over Magnetic Catapult Tracks

Sławomir Czubaj, A. Sibilska-Mroziewicz, E. Ładyżyńska-Kozdraś
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Abstract

The growing demand for commercial unmanned aerial vehicles (UAV) requires that innovative technical solutions for the critical aspects of UAV servicing, must be researched. The magnetic catapult discussed in this work is an interesting alternative to the existing UAV deployment or launch platforms. This paper presents the research designed to facilitate the measurement and analysis of the position of a launch truck applied in a UAV magnetic catapult with tracks. The measurement system discussed herein comprised a transducer connected to Hall sensors which were spaced evenly at the base of a superconductor pod. A displacement of the superconductor pod relative to the magnetic field resulted in the variation of the voltage output from individual Hall sensors. A proprietary algorithm was developed and controlled stepper motors which displaced the assembly of the superconductor pod with the Hall sensors along the test track of the UAV magnetic catapult. At the same time as the displacement was sensed by the Hall sensors, they were reading the real-time magnetic strength; it was therefore critical for the microcontroller, which executed the control algorithm, to operate at a sufficient processing frequency (speed). The proprietary control algorithm was executed by an ATMEL ATmega2560 RISC processor. The processor system read the status of every Hall sensor in the assembly and compared it to the reference voltage outputs stored in the microcontroller’s memory. The difference between the voltage output reading and the reference voltage outputs and the superconductor pod’s geometry was used to determine the superconductor pod’s position along the magnetic tracks of the UAV magnetic catapult.
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霍尔传感器在磁弹射器轨道磁场测量中的应用概念
对商用无人机日益增长的需求要求必须研究针对无人机服务关键方面的创新技术解决方案。磁弹射器在这项工作中讨论是一个有趣的替代现有的无人机部署或发射平台。本文介绍了用于无人机带履带磁弹射器的发射车位置测量与分析的研究。本文讨论的测量系统包括一个与霍尔传感器相连的传感器,霍尔传感器均匀地分布在超导吊舱的底部。超导体吊舱相对于磁场的位移导致了各个霍尔传感器输出电压的变化。开发了一种专有算法,并控制步进电机沿无人机磁弹射器测试轨迹移动带有霍尔传感器的超导吊舱组件。霍尔传感器在感知位移的同时,实时读取磁场强度;因此,对于执行控制算法的微控制器来说,以足够的处理频率(速度)操作是至关重要的。该专有控制算法由ATMEL ATmega2560 RISC处理器执行。处理器系统读取组件中每个霍尔传感器的状态,并将其与存储在微控制器存储器中的参考电压输出进行比较。利用电压输出读数与参考电压输出之间的差值以及超导吊舱的几何形状来确定超导吊舱沿无人机磁弹射器磁轨迹的位置。
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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发文量
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审稿时长
53 weeks
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