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Influence of space charged particles on satellite optical communication system

Wybrane pełne teksty z tego czasopisma
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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Although research of satellite optical communication system has been carried out for many years, there is scarce literature to comprehensively analyze the influence of space environment on satellite optical communication system. Different kinds of particles and fields exist in the space environment, including high energy charged particles, solar radiation, plasma environment, space fragment, etc. The Influence of space charged particles on satellite optical communication system was investigated in detail, which mainly related to single event upset (SEU), total dose effect and plasma environment. For SEU analysis the relation between single proton upset rate and satellite orbit was analyzed in detail. The reliability index of equipment based on SEU was proposed, the numerical calculation results have proved that the SEU effect was relatively less and corresponded to higher reliability of SRAM/MOS equipment under lower orbit altitude and inclination. For plasma environment analysis there is no obvious influence of plasma on laser signal transmission. But charging and discharging processes on satellite surface would lead to the malfunction of satellite communication system. The influence of charged particles and its related plasma on satellite optical communication system was investigated, which would be helpful for the design and the improvement of performance of satellite optical communication system.
Czasopismo
Rocznik
Strony
251--265
Opis fizyczny
bibliogr. 14 poz.,
Twórcy
autor
autor
autor
autor
autor
autor
autor
autor
  • Telecommunication Engineering Institute, Air Force Engineering University, Xi'an 710077, China
Bibliografia
  • [1] ZHAO SHANG-HONG, Optical communication system, Xi Dian University Publishing Company, 2005 (in Chinese).
  • [2] HOU RUI, ZHAO SHANG-HONG, LI YONG-JUN, et al., Analysis of space environment effects on satellite optical communication system, Optical Communication Technique 32(4), 2008, pp. 61–63.
  • [3] YU QINGKUI, ZHAO DAPENG, SEU rate prediction induced by space particles, Chinese Space Scientific Technology 53(6), 1998, pp. 56–61.
  • [4] XUE YUXIONG, CAO ZHOU, SEU rate calculation induced by high energy proton on satellite based electronic system, Space Craft Environmental Engineering 22(8), 2005, pp. 192–195.
  • [5] PETERSEN E.L., The SEU figure of merit and proton upset rate calculations, IEEE Transactions on Nuclear Science 45(6), 1998, pp. 2550–2562.
  • [6] PETERSEN E.L., Predictions and observations of SEU rates in space, IEEE Transactions on Nuclear Science 44(6), 1997, pp. 2174–2187.
  • [7] BARAK J., REED R.A., LABEL K.A., On the figure of merit model for SEU rate calculations, IEEE Transactions on Nuclear Science 46(6), 1999, pp. 1504–1510.
  • [8] GARRETT H.B., WHITTLESEY A.C., Spacecraft charging: An update, IEEE Transaction on Plasma Science 28(6), 2000, pp. 2017–2028.
  • [9] GREGDIRE D.J., Electromagnetic Wave Propagation in Unmagnetized Plasma, ADA250710, 1992.
  • [10] SUN AIPING, LI LIQIONG, QIU XIAOMING, Interaction of the electromagnetic waves and non--magnetized plasmas, Nuclear Fusion and Plasma Physics 22(3), 2002, pp. 135–137.
  • [11] MENGU CHO, HOSODA S., OKUMURA T., et al., Intermediate report on development of high voltage solar array in LEO plasma environment, Radio Science Conference 2004, pp. 612–613.
  • [12] YANG JUAN, SU WEIYI, MAO GENWANG, On calculating effectiveness of Plasma defense against low orbit spy satellite, Journal of Northwestern Polytechnical University 23(1), 2005, pp. 93–96.
  • [13] GU SHIFEN, SHI LIQIN, ZANG ZHENQUN, Arc discharges for high voltage solar array in the space plasma, Chinese Journal of Space Science 15(2), 1995, pp. 131–135.
  • [14] LI JIAWEI, LI ZHONGYUAN, Charging process of space dust and its dependence on plasma parameters, Chinese Journal of Space Science 24(5), 2004, pp. 321–323.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BPW7-0011-0023
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