系统工程与电子技术

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机载卫星通信波束受机身固定遮挡建模及仿真

王燕敏, 李博骁, 叶海军   

  1. 中国电子科技集团公司电子科学研究院, 北京 100041
  • 出版日期:2016-06-24 发布日期:2010-01-03

Modeling and simulation for fixed blockage of airborne satellite communication beam by fuselage

WANG Yan-min, LI Bo-xiao, YE Hai-jun   

  1. Academy of Electronics and Information Technology, China Electronics Technology Group Corporation, Beijing 100041, China
  • Online:2016-06-24 Published:2010-01-03

摘要:

作为超视距通信的主要手段之一,卫星通信是特种飞机执行远程飞行任务的重要保障。由于特种飞机机身的特殊结构,卫星通信波束可能会在飞机处于某些飞行区域或以特定姿态飞行时受到机身固定突出构造的遮挡,造成卫星通信链路性能恶化,甚至通信中断。针对特种飞机机身的固定遮挡难题,利用电磁传播的菲涅尔区理论建立了遮挡模型,并基于投影理论提出了基于双坐标系变换的遮挡分析方法。所提的遮挡模型和分析方法能够准确刻画固定遮挡造成的电磁波传播损耗,为卫星通信天线位置的优化设计提供参照。此外,所提出的分析方法实现复杂度低,适于工程实践。

Abstract:

As a main measure of beyond line-of-sight communication, satellite communication is crucial for the special aircraft with long distance tasks. Due to the specific structure of special aircraft, the satellite communication beam may suffer from fixed blockage by protuberances on top of the fuselage when the aircraft flies in certain airspace or in some specific attitude, causing continuous degradation of the link or even outage of communications. To solve this problem, based on the Fresnel zone theory of electromagnetic propagation, a blockage model and further a blockage analysis approach based on the projection theory and doublecoordinate system transformation are proposed. The proposed model and the analysis approach can accurately characterize the electromagnetic propagation loss, thus reference for the installation position selection of the satellite communication antenna arrays can be provided. In addition, the implementation complexity of the proposed approach is low, which makes it suitable for practical applications.