Hardware of the system for determining coordinates based on satellite navigation

Abstract

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.