基于卫星导航的坐标确定系统硬件

II All-Russian scientific conference with international participation "Achievements of science and technology" Pub Date : 1900-01-01 DOI:10.47813/dnit-ii.2023.7.490-494

D. I. Kovalev, T. P. Cherkasova, A.A. Yablokova, V. Podoplelova

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引用次数: 0

摘要

本文讨论了基于卫星导航的坐标确定系统的硬件构成。给出了该装置的结构框图，并对主要功能模块进行了说明。介绍了一种通过卫星通信系统铱星进行通信的实验装置。根据实验结果发现，在以巡航速度飞行时，可以通过GSM和铱星两种方式将飞行器所在位置的坐标传递给控制站。计划在较大巡航速度的飞机上对实验模型进行测试。

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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Hardware of the system for determining coordinates based on satellite navigation

The article discusses the hardware of the system for determining coordinates based on satellite navigation. The structural diagram of the device is given and a description of the main functional blocks is given. An experimental installation is presented, which provides communication through a satellite communication system Iridium. According to the results of the experiment, it was found that when flying at cruising speed, you can transfer the coordinates of the location of the aircraft to the control station through both GSM and Iridium. The tests of an experimental model on a aircraft with a larger cruising speed are planned.

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II All-Russian scientific conference with international participation "Achievements of science and technology"

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