Preprint Communication Version 1 Preserved in Portico This version is not peer-reviewed

Downlink Analysis of a Low-Earth Orbit Satellite Considering an Airborne Interference Source Moving on Various Trajectory

Version 1 : Received: 18 November 2023 / Approved: 20 November 2023 / Online: 20 November 2023 (15:26:58 CET)

A peer-reviewed article of this Preprint also exists.

Kang, E.; Park, Y.; Kim, J.; Choo, H. Downlink Analysis of a Low-Earth Orbit Satellite Considering an Airborne Interference Source Moving on Various Trajectory. Remote Sens. 2024, 16, 321. Kang, E.; Park, Y.; Kim, J.; Choo, H. Downlink Analysis of a Low-Earth Orbit Satellite Considering an Airborne Interference Source Moving on Various Trajectory. Remote Sens. 2024, 16, 321.

Abstract

This paper analyzes low-Earth orbit (LEO) satellite downlinks when an airborne interference source moves parallel to the satellite trajectory by considering the relative angle differences be-tween the satellites and the interference sources. To make the experimental interference situations more like actual environments, the LEO trajectories are obtained from two-line element set (TLE) data. Airborne interference sources with various altitudes move parallel to the LEO trajectories, and the jamming to signal (J/S) ratio is calculated based on the relative angle differences between the ground station, the LEO satellite, and the interference source. In order to calculate the relative angle difference psi, the coordinates of the satellite and the interference source are converted from the World Geodetic System 1984 (WGS84) to the ground station-centered east-north-up (ENU) system. By applying the relative angle difference psi, we can obtain the sidelobe gain of the ground station antenna in the direction from which the interference comes. The results of the study confirm that, from a J/S ratio perspective, the distances between the ground station, LEO satellite, and airborne interference source are important, and in particular, the relative angle difference psi between the interference source and the satellite is more critical factor.

Keywords

LEO satellite; link budget; antenna radiation patterns; interference situation; relative angle; coordinate system conversion; J/S ratio

Subject

Engineering, Aerospace Engineering

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