航天器天线射频耦合模型

G. Galgani, G. Scozza, E. Scione, A. Sabatini, G. Spera, Scorzafava Edmondo, G. Varacalli
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引用次数: 1

摘要

由于卫星的高度一体化和客户任务所需的多波段操作,卫星天线场在天线容纳要求方面变得非常关键。最佳的有效载荷性能驱动了射频滤波器和天线放置的早期设计。一旦卫星一体化进入后期阶段,更换天线的成本就会增加,而且会影响卫星的时序。有时,两个天线之间要求的解耦水平是具有挑战性的,必须通过非常准确和可靠的建模工具[3]-[9]进行预测和验证,目的是由于可访问性问题和进度限制而最小化和优化卫星级别的测试。本文的范围是展示一种有效的方法来预测天线耦合因素,应用电磁仿真工具在一个真实的工业案例中,研究了一个非常大的SAR阵列和x波段的数据下行链路天线之间可能的EMI风险。GALILEO-EMT[1]套件在本次活动中得到了应用,最后在泰利斯阿莱尼亚意大利空间团队设计的具有代表性的低轨道地球观测卫星模型上进行了耦合测试(即cosmos - skymed,由意大利航天局(ASI)管理,由ASI和意大利国防部长共同资助的项目)。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Model for RF Coupling on Spacecraft Antennas
Satellites antenna farms are becoming very critical in terms of antenna accommodation requirements, due to the high level of integration of the satellite and due to multi band operations required from customer missions. The optimal payload performances drive an early design of RF filters and antenna placement. Once the satellite integration goes in advanced phase, the antenna replacement becomes costly and impacts timing. Sometimes the decoupling level requested between two antennas is challenging and has to be predicted and verified by very accurate and reliable modeling tools [3]–[9] with the aim to minimize and optimize the testing at satellite level due to accessibility issues and to schedule constraints. Scope of this paper is to show an effective approach to predict antenna coupling factors applying EM simulation tools on a real industrial case where a possible EMI risk between a very large SAR array and Data Downlink antenna in X-band was studied. The GALILEO-EMT [1] suite was applied in this activity that ended with a coupling test on a representative satellite Mockup designed by Thales Alenia Space Italia team in the frame of a Low Orbit Earth Observation Satellite qualification (i.e. COSMO-SkyMed, a program managed by the Italian Space Agency (ASI) and co-funded by ASI and the Italian Minister of Defence).
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