SelenIRIS:用于立方体卫星的月地光通信终端

Jorge Rosano Nonay, C. Fuchs, Davide Orsucci, C. Schmidt, D. Giggenbach
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引用次数: 1

摘要

卫星的小型化以及制造和发射成本的下降使月球任务成为许多航天公司和机构关注的焦点。然而,在传统的射频通信系统中,在远距离上实现立方体卫星所需的数据速率越来越具有挑战性。自由空间光学(FSO)通信提供了一种紧凑、轻便、低功耗的替代方案,具有更高的数据吞吐量和更少的限制(例如,更少的政府法规、信道干扰、窃听……)。基于其在激光通信和新空间技术方面的悠久传统,德国航空航天中心(DLR)正在为其OSIRIS计划研究seleniris——一种用于月地光学数据传输的小型终端。本文将分析将技术从飞行验证的低地球轨道终端(如OSIRIS4CubeSat (O4C)[1])转移到月球轨道上的概念任务所需的必要适应。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
SelenIRIS: a Moon-Earth Optical Communication Terminal for CubeSats
Satellite miniaturization and sinking costs of manu-facturing and launches are bringing Moon missions in the focus of many space companies and agencies. However, achieving the desired data rates on CubeSats over long ranges is proving increasingly challenging with traditional radio-frequency communication systems. Free-space optical (FSO) communications offer a compact, light, and low-power alternative with higher data throughput and fewer limitations (e.g., fewer governmental regulations, channel interference, eavesdropping...). Based on its long heritage of laser communications and new-space tech-nology, the German Aerospace Center (DLR) is investigating SelenIRIS-a miniaturized terminal for Moon-Earth optical data transmissions-for its OSIRIS program. This paper will analyze the necessary adaptations that are required to transfer the technology from the flight-proven low Earth orbit terminals like OSIRIS4CubeSat (O4C) [1] to a concept mission in Lunar orbit.
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