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DOI:
飞控与探测:2021,(6):1-8
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高超声速飞行器太赫兹测控通信设计与分析
(1.西北工业大学 电子信息学院;2.上海航天控制技术研究所)
Research on Terahertz TT & C Communication Performance of Hypersonic Vehicle
(1.School of Electronics and Information,Northwestern Polytechnical University;2.Shanghai Aerospace Control Technology Institute)
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中文摘要: 针对高超声速飞行器在临近空间通信是面临的黑障问题,提出了一种利用太赫兹波来进行测控通信(TT & C)的方法。在建立时变、非均匀等离子体模型的基础上,采用移位算子时域有限差分(SO-FDTD)方法分析了不同的等离子体参数对电磁波散射特性的影响。在此基础上建立了太赫兹抗黑障测控通信系统模型,并重点研究了太赫兹抗黑障测控通信的系统性能。结合实际的通信系统参数和环境参数,进行了太赫兹抗黑障测控通信系统性能仿真,结果表明,通信距离、等离子体上升时间、温度和压强都会对通信系统的误码率性能产生影响,其中通信距离对系统性能的影响显著。总体来看,提升入射波频率是减轻等离子体影响的有效方法,其次为了保障系统的误码率性能应根据链路预算设计合理的通信距离。
中文关键词: 高超声速  黑障  太赫兹  测控  性能
Abstract:Aiming at the problem of black barrier in near space communication of hypersonic vehicle, a method of tracking, telemetry and command (TT & C) communication using terahertz wave is proposed. Based on the time-varying and inhomogeneous plasma model, the shift operator finite difference time domain (SO-FDTD) method is used to analyze the influence of different plasma parameters on electromagnetic wave scattering characteristics. On this basis, the model of terahertz anti-black barrier TT & C system is established, and the performance of terahertz anti-black barrier TT & C system is mainly studied. Combined with the actual communication system parameters and environmental parameters, the performance simulation of terahertz anti-black barrier TT & C communication system is carried out. The results show that the communication distance, plasma rise time, temperature and pressure all have an impact on the BER performance of the communication system, and the communication distance has a significant impact on the system performance. In general, increasing the frequency of incident wave is an effective way to reduce the influence of plasma. Secondly, in order to ensure the BER performance of the system, a reasonable communication distance should be designed according to the link budget.
文章编号:20210601     中图分类号:TN911.72    文献标志码:A
基金项目:上海航天科技创新基金资助项目(SAST2019-078);大学生创新创业训练计划项目(S202010699400);国家自然科学基金项目( 61701407,61871327)
引用文本:
左晓亚,许东欢,刘佳怡,姚如贵.高超声速飞行器太赫兹测控通信设计与分析[J].飞控与探测,2021,(6):1-8.

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