Estimating Fields in Spacecraft Cavities: Experimental Validation and Optimization of Finite-Difference Time-Domain and Power Balance Computational Tools

IF 1.8 Q3 ENGINEERING, ELECTRICAL & ELECTRONIC
Javier Jair Pazos;Matthew C. Miller;Jeff Phillips;Eric Miller;Tim McDonald;Jennifer Kitaygorsky
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引用次数: 0

Abstract

Electromagnetic fields in representative spacecraft cavities were successfully predicted using finite-difference time-domain and power balance computational tools. Results were validated with measurements of two test articles, showing excellent correlation in shielding effectiveness from 300 MHz to 18 GHz. The validated tools were then extended to predict fields inside representative, to-scale payload fairings including common systems and components like satellite payloads, antennas, acoustic blankets, and a cable harness. Various computational techniques were used to compare their speed and accuracy. Ultimately, we conclude that a multi-fidelity approach – combining full-wave, statistical, and hybrid solutions – is beneficial and necessary for complex and large cavity problems. The tools and techniques presented here can serve as part of a toolkit to rapidly estimate shielding effectiveness, the impact of payloads, and overall fields in spacecraft cavities.
航天器空腔场估计:时域有限差分和功率平衡计算工具的实验验证与优化
利用时域有限差分和功率平衡计算工具,成功地预测了具有代表性的航天器空腔中的电磁场。通过对两种供试品的测量验证了结果,显示出在300MHz至18GHz的屏蔽有效性方面的良好相关性。然后,经过验证的工具被扩展到预测具有代表性的内部场,以缩放有效载荷整流罩,包括卫星有效载荷、天线、声学毯和电缆束等常见系统和组件。使用了各种计算技术来比较它们的速度和准确性。最终,我们得出结论,高保真度方法——结合全波、统计和混合解决方案——对于复杂和大型空腔问题是有益和必要的。这里介绍的工具和技术可以作为工具包的一部分,快速估计屏蔽效果、有效载荷的影响和航天器空腔中的整体场。
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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来源期刊
CiteScore
4.30
自引率
0.00%
发文量
27
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