SDR Helix Antenna Deployment Experiment (SHADE) on board BEXUS

Melina Koukou, Vasilis Vellikis, Ioannis Varvaringos, Konstantinos Koutropoulos, Ioannis Myrsinias, D. Argiropoulos, Andronikos Dourmisis, Orestis Rafail Nerantzis, Ioannis Ioannou, Elli Loukaridou Kizili, Spyros Megalou
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Abstract

In the field of space travel, space communications has always presented a slew of obstacles and hurdles that must be overcome in order to complete a successful mission. Space limits inside a satellite or spaceship, vast distances between satellites and ground stations, and a phenomenon known as "Faraday Rotation" in the ionosphere are only a few of the most typical issues. Satellite antennas must be small, compact, efficient, and circularly polarized as a result of the aforementioned issues. The helix antenna is an excellent answer for all of the requirements. In this work we develop a deployment and pointing mechanism of a helix antenna operated with software defined radio algorithms. The features of helix antennas are exceptional, and they are especially suitable for satellite communication. Three coaxial cylinders, two stepper motors, one pulley, and one thread make up a deployment-pointing mechanism. The mechanism deploys the antenna along its longitudinal axis and turns it horizontally towards the ground station. During the flight, the antenna is deployed and retracted. Under different positioning situations, the GPS, an altimeter, and a compass calculate the gondola's position in order to rotate the antenna towards the Ground Station and close the communication link. The antenna's rotation mechanism is triggered by the integrated attitude determination and control system algorithms in order to correct the pointing and orientation towards the Ground Station. The antenna uses software defined radio algorithms to achieve weight and volume reductions while maintaining high efficiency and reconfigurability. The experiment includes a high-definition camera that provides real-time information on the antenna's orientation and condition. SHADE's flight on the BEXUS 28/29 balloon resulted in effective deployment and transmission, as well as the ability to receive and decode transmitted packets. The rotating mechanism met the pointing requirements, and all of the sensor's data was correctly saved to our system. Throughout the trip, there were no signs of thermal risk
机载BEXUS上的SDR螺旋天线展开实验(SHADE)
在太空旅行领域,为了成功完成任务,空间通信一直存在一系列必须克服的障碍和障碍。卫星或宇宙飞船内部的空间限制,卫星和地面站之间的巨大距离,以及电离层中被称为“法拉第旋转”的现象,这些只是最典型的问题中的几个。由于上述问题,卫星天线必须是小、紧凑、高效和圆极化的。螺旋天线是一个很好的回答所有的要求。在这项工作中,我们开发了一种螺旋天线的部署和指向机制,该机制由软件定义的无线电算法操作。螺旋天线具有独特的特点,特别适用于卫星通信。三个同轴气缸、两个步进电机、一个滑轮和一根螺纹组成了一个部署指向机构。该机构沿着其纵轴展开天线,并将其水平转向地面站。在飞行过程中,天线展开和收缩。在不同的定位情况下,GPS、高度计和指南针计算出贡多拉的位置,从而使天线向地面站方向旋转,关闭通信链路。天线的旋转机构由综合姿态确定和控制系统算法触发,以纠正指向地面站的指向和方向。该天线采用软件定义的无线电算法,在保持高效率和可重构性的同时实现重量和体积的减少。该实验包括一个高清摄像机,可以提供天线方向和状况的实时信息。SHADE在BEXUS 28/29气球上的飞行实现了有效的部署和传输,以及接收和解码传输数据包的能力。旋转机构满足指向要求,传感器的所有数据都正确保存到系统中。在整个旅程中,没有任何热风险的迹象
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