| [1] Langley R C. The entry plasma sheath and its effects on space vehicle electromagnetic systems volume I[C]//Fourth Plasma Sheath Symposium. Hampton, Virginia: Scientific and Technical Information Office: National Aeronautics and Space Administration, 1971: 137-157.[2] James P R, Churchill R J. Progress in reentry communications[J]. IEEE Transactions on Aerospace and Electronic Systems, 1971, AES-7(5): 879-894.[3] Hartunian R A, Stewart G E, Fergason S D, et al. Causes and mitigation of radio frequency blackout during reentry of reusable launch vehicles ATR-2007(5309)-1[R]. Washington, D. C.: the Aerospace Corporation EI Segundo, 2007.[4] Christopher N D, Peter Y P, Sven G B. Hypersonic or re-entry plasma communication[C]//17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Reston: AIAA, 2011: 1-13.[5] Wu R H, Liu H Y, Liu J Q, et al. Experiment on influence of the communication signals transmission in plasma sheath[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(11): 1437-1442 (in Chinese). 邬润辉, 刘洪艳, 刘佳琪, 等. 等离子体鞘套对C波段通信信号传输影响的试验[J]. 北京航空航天大学学报, 2013, 39(11): 1437-1442.[6] David M, Jeffrey P, Jamey S, et al. Radio frequency (RF) blackout during hypersonic reentry[C]//AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. Reston: AIAA, 2005: 205-243.[7] Ma P, Zeng X J, Shi A H, et al. Experimental investigation on electromagnetic wave transmission characteristic in the plasma high temperature gas[J]. Journal of Experiments in Fluid Mechanics, 2010, 24(5): 51-69 (in Chinese). 马平, 曾学军, 石安华, 等. 电磁波在等离子体高温气体中传输特性实验研究[J]. 实验流体力学, 2010, 24(5): 51-69.[8] Shawn G O, Alranzo B R, Brian E G, et al. RF signal impact study of an SPT[C]//32nd Joint Propulsion Conference and Exhibit. Reston: AIAA, 1996: 1-11.[9] Yang M, Li X P, Xie K, et al. A large volume uniform plasma generator for the experiments of electromagnetic wave propagation in plasma[J]. Physics of Plasmas, 2013, 20(012101): 1-6.[10] Xie K, Li X P, Yang M, et al. Experimental study on attenuation characteristics of L and S band electronmagnetic wave in plasma[J]. Journal of Astronautics, 2013, 34(8): 1166-1171 (in Chinese). 谢楷, 李小平, 杨敏, 等. L、S频段电磁波在等离子体中衰减实验研究[J]. 宇航学报, 2013, 34(8): 1166-1171.[11] Gao P, Li X P, Liu Y M, et al. Plasma sheath phase fluctuation and its effect on GPS navigation[C]//10th International Symposium on Antennas, Propagation & EM Theory (ISAPE). Xi'an: Xidian University, 2012: 579-582.[12] Donald S F, Peter E N, Merlin G M, et al. Re-entry plasma induced pseudorange and attenuation effects in a GPS simulater[C]//SPIE Defense and Security Symposium. Orlando, FL: 2004: 1-11.[13] Gao P, Li X P, Yang M, et.al. Effect of time-varying plasma sheath phase fluctuation on GPS navigation[J]. Journal of Astronautics, 2013, 34(10):1330-1336 (in Chinese). 高平, 李小平, 杨敏, 等. 时变等离子鞘套相位抖动对GPS导航的影响[J]. 宇航学报, 2013, 34(10): 1330-1336.[14] Xie K, Li X P, Liu D L, et al. Reproducing continuous radio blackout using glow discharge plasma[J]. Review of Scientific Instruments, 2013, 84(104701): 1-6.[15] Shi L, Guo B L, Liu Y M, et al. Research on integrated channel model for near-space hypersonic vehicle[J]. Journal of Astronautics, 2011, 32(7): 1557-1563 (in Chinese). 石磊, 郭宝龙, 刘彦明, 等. 临近空间高速飞行器综合信道模型研究[J]. 宇航学报, 2011, 32(7): 1557-1563.[16] Heald C B, Wharton M A. Plasma diagnostics with microwaves[M]. New York: Wiley, 1965: 57-65.[17] Stix T H. Waves in plasma[M]. New York: American Institute of Physics, 1992: 3-33.[18] Gregoire D J, Santoru J, Schumacher R W, et al. Electromagnetic wave propagation in unmagnetized plasmas[R]. Bolling AFB DC: Air Force Office of Scientific Research, 1992.[19] Bai X Y, Zhang Z T, Yang B, et al. Study on the method of non-equiblium plasma sheath by using strong ionization discharge[J]. Acta Aeronoutica et Astronautica Sinica, 2004, 25(1): 51-54 (in Chinese). 白希尧, 张芝涛, 杨波, 等. 用于飞行器的强电离放电非平衡等离子体隐身方法研究[J]. 航空学报, 2004, 25(1): 51-54. |
CJA
