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不同入射角度下等离子鞘套中C波段电磁波传输特性

凌云飞 陈长兴 蒋金

凌云飞, 陈长兴, 蒋金. 不同入射角度下等离子鞘套中C波段电磁波传输特性[J]. 空间科学学报, 2016, 36(6): 904-908. doi: 10.11728/cjss2016.06.904
引用本文: 凌云飞, 陈长兴, 蒋金. 不同入射角度下等离子鞘套中C波段电磁波传输特性[J]. 空间科学学报, 2016, 36(6): 904-908. doi: 10.11728/cjss2016.06.904
LING Yunfei, CHEN Changxing, JIANG Jin. Properties of C-Band Wave Propagation in Plasma Sheath with Different Incidence Angle[J]. Journal of Space Science, 2016, 36(6): 904-908. doi: 10.11728/cjss2016.06.904
Citation: LING Yunfei, CHEN Changxing, JIANG Jin. Properties of C-Band Wave Propagation in Plasma Sheath with Different Incidence Angle[J]. Journal of Space Science, 2016, 36(6): 904-908. doi: 10.11728/cjss2016.06.904

不同入射角度下等离子鞘套中C波段电磁波传输特性

doi: 10.11728/cjss2016.06.904
基金项目: 

陕西省自然科学计划项目资助(2014JM8344)

详细信息
    通讯作者:

    凌云飞,E-mail:lingyunf0421@hotmail.com

  • 中图分类号: TN011;V271

Properties of C-Band Wave Propagation in Plasma Sheath with Different Incidence Angle

  • 摘要: 为解决临近空间通信黑障问题,研究了不同入射角对等离子体鞘套中C波段(4~8GHz)电磁波传输特性的影响,分别采用均匀等离子体模型与高斯分布非均匀等离子体模型,根据电磁波在分层介质面的反射和透射传播原理,对不同角度下C波段通信电磁波的传输性能进行计算和对比分析.结果表明,入射波频率的增加以及入射角的减小有利于降低C波段的衰减值,提高透射率,使通信电磁波更有效地穿透等离子体鞘套,为解决临近空间通信黑障问题提供了理论依据.

     

  • [1] SHI Lei, GUO Baolong, LIU Yanming, et al. Research on integrated channel model for near-space hypersonic vehicle[J]. J. Astron., 2011, 23(7):1557-1563
    [2] TIAN Bailing, FAN Wenru, SU Rui, et al. Real-time trajectory and attitude coordination control for reusable launch vehicle in reentry phase[J]. IEEE Trans. Indust. Electron., 2015, 62(3):1639-1649
    [3] CHATTERJEE K, John R R, SINGH S. A new Green's function Monte Carlo algorithm for the solution of the two-dimensional nonlinear Poisson-Boltzmann equation: application to the modeling of the communication breakdown problem in space vehicles during re-entry[J]. J. Comput. Phys., 2014, 276(7):479-485
    [4] SHARIFIAN M, SADEGHI Y. FDTD study of the effects of the doubly ionized ions on the plasma immersion ion implantation process[J]. Plasma Phys., 2014, 80(2):215
    [5] LI Jin, PI Yiming, YANG Xiaobo. A conception on the terahertz communication system for plasma sheath penetration[J]. Wireless Comm. Mobile Comput., 2014, 14:1252-1258
    [6] LI Jiangting, GUO Lixin, JIN Shasha, et al. EM wave propagation characteristic in plasma sheath[J]. Chin. J. Radio Sci., 2011, 26(3):494-500
    [7] SUN Xin, LIU Yanan, LIU Yimin, et al. Study on the transmission properties of plasma sheath based on transfer matrix method[J]. Chin. J. Space Sci., 2014, 34(2):194
    [8] KIM M, KEIDAR M, IAIN D B. Electrostatic manipulation of a hypersonic plasma layer: images of the two-dimensional sheath[J]. IEEE Trans. Plasma Sci., 2008, 36(4):1198-1199
    [9] KEIDAR M, KIM M, BOYD I D. Electromagnetic reduction of plasma density during atmospheric reentry and hypersonic flight[J]. Spacer. Rockets, 2008, 45(3):445-453
    [10] CHEN Yuxun, ZHAO Qing, BO Yong, et al. Numerical simulation and experimental verification of electromagnetic transmission characteristics of plasma sheath[J]. High Power Laser Particle Beams, 2015, 27(3):032-041
    [11] GAO Xiaotian, JIANG Binhao. A matching approach to communicate through the plasma sheath surrounding a hypersonic vehicle[J]. J. Appl. Phys., 2015, 117(23):1-25
    [12] CHALISE R, KHANAL R. The study of kinetic energy of ion and sheath thickness in magnetized plasma sheath[J]. J. Mater. Sci. Eng., 2015, A5(1/2):41-46
    [13] CHEN Changxing, JIANG Jin, LING Yunfei, et al. Aperture coupled antenna design for near space communication in Ka/V dual-band[J]. J. Astron., 2015, 36(8):940-944
    [14] LING Yunfei, CHEN Changxing, JIANG Jin. Analysis of terahertz wave propagation in near space plasma sheath[J]. J. Air Force Eng. Univ.: Nat. Sci., 2016, 17(2):50-56
    [15] CUI Junxia, SHI Huli, TIAN Bingli. Rainfall effects on CAPS micro mobile satellite terminal communication system[J]. Commun. Technol., 2009, 42(6):8-10
    [16] SHI Lei. On Nearspace Vehicle Channel Characteristic[D]. Xi'an: Xi'an Electronic and Engineering University[D], 2012
    [17] ZHENG Ling. Study of Electromagnetic Wave Propagation in Spacecraft Plasma Sheath[D]. Xi'an: Xi'an Electronic and Engineering University, 2013
    [18] National Aeronautics and Space Administration. The Entry Plasma Sheath and its Effects on Space Vehicle Electromagnetic Systems[R]. Washington DC: NASA, 1970
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出版历程
  • 收稿日期:  2015-09-10
  • 修回日期:  2016-03-02
  • 刊出日期:  2016-11-15

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