基于LoRa sv611的通信系统利用惯性测量单元传感器监测火箭行为

M. Misbahuddin, Muhamat Taufik, I. M. B. Suksmadana
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引用次数: 0

摘要

有效载荷是由火箭携带的一种材料,它起到遥测的作用,监测环境条件并将其传输到地面接收站。本研究的目标是设计、建造和测试一个火箭有效载荷监测系统,该系统将跟踪火箭的位置、行为和轨迹。火箭有效载荷和地面控制站是分开设计和制造的。有效载荷由各种组件组成,包括Arduino Uno, MPU-6050传感器,GPS Neo-7M和LoRa SV611发射器。GCS由树莓派、LoRa SV611接收器、USB TTL和python idle组成。俯仰、横摇、偏航、经度、纬度和高度是火箭有效载荷监测系统可以跟踪的六个特征之一。试验结果表明,该有效载荷监测系统能够以较高的精度实时跟踪6个参数和弹道。所有有效载荷测量参数都以图表的形式清晰地显示在GCS界面上,每1000毫秒更新一次。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
LoRa SV611-Based Communication System To Monitor Behaviour of Rocket Using Inertial Measurement Unit Sensor
A payload is a material carried by a rocket that acts as telemetry, monitoring environmental conditions and transmitting them to earth-based receiving stations. The goal of this study is to design, build, and test a rocket payload monitoring system that will track the rocket's position, behaviour, and trajectory. The rocket payload and the Ground Control Station are designed and manufactured separately (GCS). The payload is made up of a variety of components, including an Arduino Uno, an MPU-6050 sensor, a GPS Neo-7M, and a LoRa SV611 transmitter. The GCS is made up of a raspberry Pi, a LoRa SV611 receiver, USB TTL, and python idle. Pitch, roll,  yaw, longitude, latitude, and altitude are among the six characteristics that the rocket payload monitoring system can track. The results of the tests show the rocket payload monitoring system can track six parameters and trajectory in real time with a high degree of accuracy. All payload measurement parameters are clearly displayed in the GCS interface as graphs that are updated every 1000 milliseconds.
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