陈萌, 魏兵, 何欣波. 高空核爆电磁脉冲入射情形下航空母舰上鞭状天线耦合特性分析[J]. 中国舰船研究, 2023, 18(4): 20–27. doi: 10.19693/j.issn.1673-3185.03121
引用本文: 陈萌, 魏兵, 何欣波. 高空核爆电磁脉冲入射情形下航空母舰上鞭状天线耦合特性分析[J]. 中国舰船研究, 2023, 18(4): 20–27. doi: 10.19693/j.issn.1673-3185.03121
CHEN M, WEI B, HE X B. Analysis of coupling characteristics of whip antenna on aircraft carrier under incident electromagnetic pulse of high-altitude nuclear electromagnetic pulse[J]. Chinese Journal of Ship Research, 2023, 18(4): 20–27. doi: 10.19693/j.issn.1673-3185.03121
Citation: CHEN M, WEI B, HE X B. Analysis of coupling characteristics of whip antenna on aircraft carrier under incident electromagnetic pulse of high-altitude nuclear electromagnetic pulse[J]. Chinese Journal of Ship Research, 2023, 18(4): 20–27. doi: 10.19693/j.issn.1673-3185.03121

高空核爆电磁脉冲入射情形下航空母舰上鞭状天线耦合特性分析

Analysis of coupling characteristics of whip antenna on aircraft carrier under incident electromagnetic pulse of high-altitude nuclear electromagnetic pulse

  • 摘要:
      目的  在考虑海面影响的情况下,研究大型舰船上鞭状天线在高空核爆电磁脉冲(HEMP)入射下的感应电流与脉冲入射角度和天线位置的关系。
      方法  考虑海面的影响,采用半空间时域有限差分法(FDTD),用细导线算法解决由于精细结构导致的计算网格量巨大、效率低下的问题,用集总元件FDTD算法计算天线后面负载对感应电流的影响,采用基于多点接口(MPI)的并行算法提高计算效率。
      结果  计算结果表明:在HEMP入射的情形下,某航空母舰模型上鞭状天线的感应电流与天线位置和入射角度等有关;典型情形下天线端口处的感应电流峰值为5.6 A。
      结论  进一步分析表明,天线端口处感应电流的大小主要取决于天线位置,与脉冲的入射角关系不大。所做研究为大型舰船脉冲电磁波入射情形下的感应电流计算分析提供了算法基础,为舰船电磁兼容问题分析提供理论支撑。

     

    Abstract:
      Objectives  Under the condition of considering the influence of the sea surface, the relationships between the induced current of a whip antenna on a large ship under the incidence of high-altitude nuclear electromagnetic pulse (HEMP) and the incident angle of the pulse and antenna position are studied.
      Methods   The half-space finite different time domain (FDTD) method is used to consider the influence of the sea surface; the thin wire algorithm is used to solve the problems of huge computational grid and low efficiency caused by the fine structure; the lumped element FDTD method is used to consider the influence of the load behind the antenna on the induced current; and a parallel algorithm based on MPI is used to speed up the calculation.
      Results  The results show that the induced current on the whip antenna of an aircraft carrier model is related to the antenna position and incident angle in the HEMP incident case. The peak value of the induced current at the antenna port is 5.6 A in typical cases.
      Conclusions  The analysis shows that the magnitude of the induced current at the antenna port mainly depends on the antenna position and has little relationship with the incident angle of the pulse. The research provides an algorithm basis for the calculation and analysis of induced current in the case of the incident pulse electromagnetic wave of large ships, and the research results provide a theoretical support for the analysis of ship electromagnetic compatibility problems.

     

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