Daily Thermo-Elastic Distortion Characterisation during Antenna In-orbit Test for Geostationary Satellites

A. Iacono, B. Pinsard
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Abstract

Before bringing a new satellite into service after launch, in-orbit testing (IOT) is essential to compare in-flight performance with on-ground references. Antenna IOT is essential to remove any mechanical depoint in order to optimize the alignment of the antenna and therefore RF performance. Depending on the frequency band of operation, thermo-elastic distortion (TED) evaluations could play an important role into the determination of the correct amount of mechanical correction to apply to the antenna. It is in fact essential to discriminate between a fixed contribution derived from an authentic geometry misalignment and an expected TED behavior. The aim of this paper is to describe the methodology to show the correlation between the antenna thermal behaviour, as-measured in-orbit, and its predictions over a period of 24 hours for the Inmarsat-6 F1 Ka-band commercial payload.
地球静止卫星天线在轨试验日热弹性畸变特性
在发射后将新卫星投入使用之前,在轨测试(IOT)对于将飞行性能与地面参考进行比较至关重要。天线物联网对于消除任何机械点至关重要,以便优化天线的对准,从而优化射频性能。根据工作频带的不同,热弹性变形(TED)评估可以在确定应用于天线的正确机械校正量方面发挥重要作用。事实上,区分来自真实几何偏差的固定贡献和预期的TED行为是至关重要的。本文的目的是描述显示Inmarsat-6 F1 ka波段商业有效载荷在24小时内在轨测量的天线热行为与其预测之间相关性的方法。
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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