改进光学轨道确定方法的基于led的立方体卫星

2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace) Pub Date : 2018-06-01 DOI:10.1109/METROAEROSPACE.2018.8453518

G. Cialone, Paolo Marzioli, S. Masillo, Andrea Gianfermo, Lorenzo Frezza, Alice Pellegrino, F. Piergentili, F. Santoni

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引用次数: 11

摘要

LEDSAT(基于led的小卫星)是一颗单单元立方体卫星，将在其六个面安装发光二极管(led)，以验证、验证和改进当前的光学轨道确定方法。从国际空间站部署后，led还将支持立方体卫星的识别。这颗卫星由罗马大学Sapienza的S5Lab研究小组制造，并已被欧洲航天局接受为“放飞你的卫星!”计划。目前，机载led已经进行了紫外线和伽马射线辐射测试，证明了它们在太空环境中的生存能力。本文介绍了LEDSAT的目标、设计、基于led的有效载荷和预期结果。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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LEDSAT: a LED-Based CubeSat for Optical Orbit Determination Methodologies Improvement

LEDSAT (LED-based small SATellite) is a 1-Unit CubeSat that will mount Light Emitting Diodes (LEDs) on its six faces, in order to validate, verify and improve the current methodologies for optical orbit determination. The LEDs will also support the CubeSat identification after deployment from the ISS. The satellite is being produced by the S5Lab research group at Sapienza – University of Rome, and it has been accepted for the European Space Agency Fly Your Satellite! Programme. Currently, the on-board LEDs have been tested for the UV and gamma-ray radiations, proving their survivability in the space environment. This paper describes the aims, the design, the LED-based payload and the expected results of LEDSAT.

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2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)

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