• DocumentCode
    2655591
  • Title

    Airborne shock response spectra analyzer based on FPGA

  • Author

    Chen De-Rong ; Xiang-bin, Li

  • Author_Institution
    Dept. of Electron. Eng., Tsinghua Univ., Beijing, China
  • fYear
    2003
  • fDate
    25-29 Aug. 2003
  • Firstpage
    224
  • Lastpage
    227
  • Abstract
    How to get enough shock environment information with limited system capacity is a key problem in space vehicle telemetry. In this paper, an airborne shock response spectra analyzer is developed based on FPGA which can real time calculate peak response spectra on board and then sending it to the ground station instead of the signal form three-axis accelerometer during the flight test. Flight test shows the analyzer can effectively compress the shock data and get enough shock environment information with limited system capacity. Moreover, the compression ratio of shock data can be flexibly adjusted according to the telemetry system capacity and real-time requirement of measurement, and some design parameters can be changed on-line. Therefore the analyzer has good applicability.
  • Keywords
    aerospace testing; field programmable gate arrays; shock waves; space telemetry; spectral analysers; FPGA; airborne shock response spectra analyzer; field programmable gate arrays; flight test; limited system capacity; on board spectra; shock data; shock environment information; space vehicle telemetry; three axis accelerometer; Accelerometers; Electric shock; Field programmable gate arrays; Information analysis; Real time systems; Satellite ground stations; Signal analysis; Space vehicles; System testing; Telemetry;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on
  • Print_ISBN
    0-7803-8149-1
  • Type

    conf

  • DOI
    10.1109/ICIASF.2003.1274871
  • Filename
    1274871