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总体方案阶段星载天线电磁兼容的仿真 被引量:2

Simulation Analysis of EMC between Spaceborne Antennas in Scheme Phase of Satellite System Design
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摘要 为适应卫星总体方案阶段对星载天线电磁兼容的快速预测需求,提出了Antenna Magus和FEKO软件相结合的快速仿真方法。首先利用Antenna Magus建立天线的初级模型,再无缝导入FEKO软件并优化得到分析所需天线模型,最后进行天线对之间的隔离度仿真。并对某型号卫星总体方案阶段论证中增加S中继终端分系统带来的天线电磁兼容问题进行了仿真,仿真结果与实际测量结果一致,表明仿真方法可有效应用于卫星工程实践。 In this paper, Antenna Magus combined with FEKO is proposed to meet the demand of rapid analysis of EMC problem be- tween spaceborne antennas in satellite's scheme phase. Antennas' primary models are to build up in Antenna Magus firstly, and will be secondly seamless imported to FEKO to get the needed models after some appropriate optimizations. Endly, isolation between antennas will be simulated. As an example, EMC problem between antennas in a satellite's scheme phase brought by a new subsystem called S-band relay terminal is simulated. The simulation results agreed well with the measurements, which means that the simulation method could be effective used to satellite engineering.
出处 《安全与电磁兼容》 2012年第3期58-60,共3页 Safety & EMC
关键词 总体方案阶段 星载天线 电磁兼容 ANTENNA Magus FEKO scheme phase of satellite system design spaceborne antenna EMC Antenna Magus FEKO
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  • 1Liang Changhong, Liu ziliang, Zhang Yu. New theory of isola- tion between antennas[C]//Proceedings of IEEE International Symposium on Microwave, Antenna, Propagation and EMC Technologies for Wireless Communications. Beijing:IEEE, 2005:585-589.
  • 2David M Pozar著,张肇仪,等译.微波工程(第三版)[M].北京:电子工业出版社,2006,62-65;206-209.
  • 3中国航天工业总公司一院第704所.GJB3590-1999.航天系统电磁兼容性要求[S].北京:[出版地不祥],1999.

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