• DocumentCode
    1792303
  • Title

    Automatic testing equivalent system design of manned spacecraft

  • Author

    Fusheng Zhang ; Zhiyong Xie

  • Author_Institution
    Inst. of Manned Space Syst. Eng., China Acad. of Space Technol., Beijing, China
  • fYear
    2014
  • fDate
    3-6 Aug. 2014
  • Firstpage
    1962
  • Lastpage
    1966
  • Abstract
    Interface test between spacecraft and electrical ground testing system(EGTS) before assembly integration and testing (AIT) is time-consuming and over ties up manpower. An equivalent system has been designed based on PXI instrument and auto-test programming in order to increase the system efficiency and automation. The system could simulate actual spacecraft to send pyrotechnic device state signal, analog signal, and execute the result of ground controlling order, and exchange testing data with EGTS to realize the user-defined automatic test. A typical application result shows that the consuming time of the automatic system falls to 6 minutes from 65 minutes and tied-up manpower declines from 4 to 2 compared with conventional equivalent system, which achieves a big step forward in system efficiency and configuration.
  • Keywords
    aerospace computing; automatic programming; automatic testing; space vehicles; EGTS; PXI instrument; analog signal; assembly integration and testing; automatic testing equivalent system design; autotest programming; electrical ground testing system; interface test; manned spacecraft; pyrotechnic device state signal; user-defined automatic test; Extraterrestrial measurements; Instruments; Power supplies; Signal processing; Software; Space vehicles; Testing; Automatic testing; Equivalent system; Manned spacecraft; PXI;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronics and Automation (ICMA), 2014 IEEE International Conference on
  • Conference_Location
    Tianjin
  • Print_ISBN
    978-1-4799-3978-7
  • Type

    conf

  • DOI
    10.1109/ICMA.2014.6886003
  • Filename
    6886003