Volume 32 Issue 6
Nov.  2012
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Article Navigation >  Chinese Journal of Space Science  > 2012  >  32(6): 834-840
LIU Wei, ZENG Li, SONG Jingxing. Design of Data Acquisition and Processing Unit for Complex Detector in the Ionosphere[J]. Chinese Journal of Space Science, 2012, 32(6): 834-840. doi: 10.11728/cjss2012.06.834
Citation: LIU Wei, ZENG Li, SONG Jingxing. Design of Data Acquisition and Processing Unit for Complex Detector in the Ionosphere[J]. Chinese Journal of Space Science, 2012, 32(6): 834-840. doi: 10.11728/cjss2012.06.834
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Design of Data Acquisition and Processing Unit for Complex Detector in the Ionosphere

doi: 10.11728/cjss2012.06.834 cstr: 32142.14.cjss2012.06.834
  • 1.

    University of Chinese Academy of Sciences, Beijing 100049

  • 2.

    State Key Laboratory of Space Weather, Center for Space Science and Applied Research, Chinese Academy of Sciences, Beijing 100190

  • 3.

    School of Astronautics, Beihang University, Beijing 100191

  • Received Date: 2011-05-25
  • Rev Recd Date: 2012-04-27
  • Publish Date: 2012-11-15
    Abstract
  • Complex Detector in the Ionosphere (CDI), designed for fast responsive spacecraft platform, is a novel conceptual payload instrument for in-situ plasma and partially ionized gases complex measurement in the ionosphere. CDI is an integrated miniature of conventional planar Langmuir probe, retarding potential analyzer and ion trap mass analyzer. In this article, based on USB2.0 and FPGA (Field-Programmable Gate Array techniques using Commercial-Off-The-Shelf (COTS) parts with highly integration level, a multi-channel Data Acquisition and Processing Unit (DPAU for CDI instrument is designed. The DAPU system and hardware design are both introduced. In addition, analysis on logic resource of FPGA and simulation on reading and writing time sequence are also introduced in the article.

     

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    • References(9)
  • [1]
    Li Junbao. Modeling optimal modular bus system design for rapid responsive spacecraft[J]. J. Astron., 2010, 31(4):1219-1223. In Chinese (李君宝. 快响应航天器模块 化总线优化设计的建模[J]. 宇航学报, 2010, 31(4):1219-1223)
    [2]
    Li Haomo. Miniaturization and integration of small satellite payload[J]. Semicond. Inf., 1998, 35(1):9-12. In Chinese (李浩模. 小型卫星有效载荷的小型化 与集成化[J]. 半导体情报, 1998, 35(1):9-12)
    [3]
    Xing Kefei, Yangjun, Wang Yueke, et al. Study on the anti-radiation technique for Xilinx SRAM-based FPGA[J]. J. Astron., 2007, 28(1):123-151. In Chinese (邢克飞, 杨俊, 王跃科, 等. Xilinx SRAM型FPGA 抗辐射设计技术研究[J]. 宇航学报, 2007, 28(1):123-151)
    [4]
    Panqing, Liao Yurong. Concepts and Research of Rapid Response[M]. National Defense Industry Press, 2010. In Chinese (潘清, 廖育荣, 等. 空间概念与研究进展[M]. 北京: 国防工业出版社, 2010)
    [5]
    You Zheng, Tian Hexiang, Libin, it et al. Plug-and-play technology for an integration electronic system in a micro-satellite[J]. J. Tsinghua Univ.: Sci. Tech., 2009, 49(11):8-13. In Chinese (尤政, 田贺祥, 李滨, 等. 微小卫星综合电子系统中的即插即用技 术[J]. 清华大学学报, 2009, 49(11):8-13)
    [6]
    Wang Wenhua, Han Shuangli, Zhang Yu, et al. Research on the reliability of FPGA configurationin space-based systems[J]. Chin. J. Space Sci., 2011, 31(1):106-111. In Chinese (王文华, 韩双丽, 张宇, 等. 航天应用FPGA配置可靠性研 究[J]. 空间科学学报, 2011, 31(1):106-111)
    [7]
    Wang Xuying, Lu Ying-hua, Zhang Likun. Design and implementation of high speed real-time data acquisition system based on FPGA[J]. J. China Univ. Posts Telecommun., 2006, 13(4):61-66
    [8]
    Yang, Shujie, Guo, Zonglian. Development of high-speed data acquisition system based on FPGA[J]. Elec. Power Autom. Equip., 2008, 28(6):93-96
    [9]
    Baronti F, Lazzeri A, Roncella R, et al. FPGA/DSP-based implementation of a high-performance multi-channel counter[J]. J. Syst. Archit., 2009, 55(10):310-316
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