• DocumentCode
    1236293
  • Title

    The STOL maneuver technology demonstrator manned simulation test program

  • Author

    Feeser, Kenneth A. ; Zeh, James M. ; Leggett, David B.

  • Author_Institution
    Wright-Patterson AFB, OH, USA
  • Volume
    4
  • Issue
    9
  • fYear
    1989
  • Firstpage
    3
  • Lastpage
    12
  • Abstract
    The STOL maneuver technology demonstrator (S/MTD) simulation is a high-fidelity, pilot-in-the-loop motion base simulation. The simulation was used to evaluate takeoff, landing, and air-to-air tasks before the first flight of the S/MTD aircraft to improve aircraft flying qualities, conduct engineering research, and ensure safety of flight. 208 hours of pilot-in-the-loop evaluations were conducted. A description is given of the simulation hardware, modeling, test methods and results for the pilot-vehicle interface (PVI), flying qualities, and aircraft failure evaluations in the STOL landing (SLAND) flight control system mode. The SLAND evaluation was part of a complete validation of the operational flight program control laws.<>
  • Keywords
    aerospace computing; aerospace simulation; aircraft control; safety; STOL landing; STOL maneuver technology demonstrator; aerospace simulation; aircraft failure; flight control; operational flight program control laws; pilot-in-the-loop motion base simulation; pilot-vehicle interface; safety; simulation test program; takeoff; Aerospace control; Aerospace electronics; Aerospace simulation; Aircraft navigation; Aircraft propulsion; Computational modeling; Displays; Gears; Synthetic aperture radar; Testing;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0885-8985
  • Type

    jour

  • DOI
    10.1109/62.35663
  • Filename
    35663