• DocumentCode
    1992921
  • Title

    Flight Simulator Fidelity Evaluation Automated Test System Analysis

  • Author

    Wang, Chunguang ; Han, Junwei ; Li, Guixian ; Jiang, Hongzhou

  • Author_Institution
    Harbin Inst. of Technol., Harbin
  • Volume
    2
  • fYear
    2008
  • fDate
    21-22 Dec. 2008
  • Firstpage
    726
  • Lastpage
    728
  • Abstract
    An automated test system for evaluating flight simulator fidelity has been implemented. The system is designed to automatically test statically and dynamically the performance of flight simulator. The testing item file is designed, the file parser supporting for batch command file formats is presented, trim function and the flying part of the test are completed, evaluation way is presented. The ability to act on virtual pilot is the most important contributor to the test efficiencies of the automated test system.
  • Keywords
    aerospace simulation; aircraft testing; program compilers; program diagnostics; program testing; automated test system analysis; batch command file format; file parser; flight simulator fidelity evaluation; trim function; Aerospace engineering; Aerospace simulation; Aerospace testing; Aircraft propulsion; Analytical models; Automatic testing; Computational modeling; Delay effects; Educational technology; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Education Technology and Training, 2008. and 2008 International Workshop on Geoscience and Remote Sensing. ETT and GRS 2008. International Workshop on
  • Conference_Location
    Shanghai
  • Print_ISBN
    978-0-7695-3563-0
  • Type

    conf

  • DOI
    10.1109/ETTandGRS.2008.352
  • Filename
    5070465