定位姿态四轴飞行器数据采集系统设计

A. Triwiyatno, Sumardi, H. Afrisal, Dhamastya Adhi Putra, Taufik Rahmadani
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引用次数: 0

摘要

四轴飞行器在飞行时需要监控以确定物体的位置和姿态。姿态包括滚转、俯仰角和偏航角。在四轴飞行器中,当目标飞离并超出操作员的观察范围时,监控是困难的。监控需要一个监控系统来进一步监控对象。一种可以用来确定四轴飞行器的位置和运动的方法是结合GPS技术和惯性传感器。本文讨论了利用GPS和惯性传感器相结合的方法,对四轴飞行器中硫气体传感器的位置、姿态和读数进行数据采集监测。通信模块采用的是433mhz射频,采用STM32F103,主单片机采用STM32F4DISCOVERY。然后通过Visual c#实时显示被接受对象的数据。纬度和经度的测试是通过跟踪物体的路径来完成的,而横滚、俯仰角和偏航角的测试是通过将物体放置在参考角度来完成的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design of Data Acquisition System for Position and Attitude Quadcopter
Quadcopter requires monitoring to determine the position and attitude of the object when flying. Attitude consists of roll, pitch, and yaw angles. In quadcopter monitoring is difficult when the object is flying away and outside the operator's viewing range. Monitoring requires a monitoring system to monitor objects further. One way that can be used to determine the position and motion of a quadcopter is by combining GPS technology and Inertial Sensor. This study discusses data acquisition to monitor the position, attitude, and value of reading the sulfur gas sensor in the quadcopter by combining GPS and Inertial Sensor. The communication module used is 433 MHz radio frequency with STM32F103 and the main microcontroller using STM32F4DISCOVERY. Data about accepted objects is then displayed through Visual C # in real time. Testing of latitude and longitude is done by tracking the path of the object, while testing roll, pitch, and yaw angles is done by placing the object in accordance with the reference angle.
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