• DocumentCode
    3390610
  • Title

    Application of DGPS simulator in HIL simulation of aerocraft

  • Author

    Wang Liang ; Wu Cheng-fu ; Kang Feng-ju

  • Author_Institution
    North West Polytech. Univ. China, Xi´an
  • fYear
    2008
  • fDate
    10-12 Oct. 2008
  • Firstpage
    562
  • Lastpage
    564
  • Abstract
    In order to resolve the problem that DGPS (differential global positioning system) can not be used in the HIL (hardware-in-loop) simulation of aerocraft, but only simulated by math modeling, a method how to use DGPS in HIL simulation was brought forward on the base of GSS7700GPS simulator and NovAtel DGPS receiver. The DGPS simulation system configuration fig of aerocarft was shown.The trial data of single GPS and DGPS was acquired and plotted in the table. Comparing single GPS trial data with DGPS trial data, it improved that DGPS has more positioning accuracy than single GPS. The method realized that the whole DGPS out-of-doors running process could be simulated realistically in static environment of laboratory. The accuracy and reliability of DGPS simulation of aerocraft were improved greatly by using the method.
  • Keywords
    Global Positioning System; aerospace simulation; differential global positioning system simulator; hardware-in-loop aerocraft simulation; math modeling; Acceleration; Aerodynamics; Computational modeling; Computer networks; Computer simulation; Frequency; Global Positioning System; Receiving antennas; Signal generators; Transceivers;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    System Simulation and Scientific Computing, 2008. ICSC 2008. Asia Simulation Conference - 7th International Conference on
  • Conference_Location
    Beijing
  • Print_ISBN
    978-1-4244-1786-5
  • Electronic_ISBN
    978-1-4244-1787-2
  • Type

    conf

  • DOI
    10.1109/ASC-ICSC.2008.4675423
  • Filename
    4675423