微型卫星ERPSat-1飞行微带天线的设计与原型

C. Hamrouni, B. Neji, A. Alimi, K. Schilling
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引用次数: 11

摘要

用新技术制造的小卫星使得在太空中完成许多任务和实验成为可能。在这方面,突尼斯Sfax工程学院智能机器研究小组实验室的Pico卫星小组为突尼斯第一颗Pico卫星ERPSat-1的使用设计并制作了微带天线的原型。其谐振频率为2.4 GHz。各种损失,如大气、自由空间、电离层和雨的损失被考虑在内。大气和自由空间损失随Pico卫星ERPSat1与地面天线之间的距离而变化。在仿真过程中,需要考虑地面天线的仰角、指向和极化损耗的变化。获得的微带天线将用于微型卫星间及其地面站通信。在本文中,我们介绍了ERPSat-1微带天线的设计,结果和使用模型的限制,以证明其在空间通信中的应用。作为第一步,这些微带天线将用于遥感系统,用于从相机到Sfax大学regm实验室开发的FPGA平台的数据传输。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design and prototype of a flight microstrip antennas for the Pico satellite ERPSat-1
Small satellites, accomplished by new technologies, allowed the achievement of many tasks and experiments in space. In this context, Pico satellites team of Research Group on Intelligent Machines laboratory of the engineering school of Sfax, Tunisia, has designed and prototyped Microstrip antennas for the first Tunisian Pico satellite ERPSat-1 use. Its resonant frequency is 2.4 GHz. The various losses like atmospheric, free space, Ionosphere and rain losses are taken in consideration. Atmospheric and free space losses vary in accordance with the distance between the Pico satellite ERPSat1 and the ground antenna. During simulations, the changes of the earth antenna which are based on elevation angle, pointing and polarization losses should be taken in consideration. The obtained Microstrip antennas will be used for inter Picosatellites and their ground stations communication. In this paper, we present the design of the ERPSat-1 Microstrip antennas, the results and the limits of the used models to prove their use for space communications. As a first step, these Microstrip antennas will be used in remote sensing system for data transmission from camera to the FPGA platform developed in REGIM laboratory of Sfax University.
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