• DocumentCode
    2834064
  • Title

    The STOL Maneuver Technology Demonstrator manned simulation test program

  • Author

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

  • Author_Institution
    Wright Res. Dev. Center, Wright-Patterson AFB, OH, USA
  • fYear
    1989
  • fDate
    22-26 May 1989
  • Firstpage
    398
  • Abstract
    A description is given of the STOL (short takeoff and landing) Maneuver Technology Demonstrator (S/MTD) simulation, a high-fidelity pilot-in-the-loop motion base simulation. The simulation was used to evaluate takeoff, landing, and air-to-air tasks before first flight of the S/MTD aircraft to improve aircraft flying qualities, conduct engineering research, and insure safety of flight. 208 hours of pilot-in-the-loop evaluations were conducted. The authors describe the simulation hardware, test approach/results of the pilot vehicle interface (PVI), and flying qualities and aircraft failure evaluations in the STOL landing (SLAND) flight control system mode
  • Keywords
    aerospace computing; aerospace simulation; aircraft control; S/MTD aircraft; STOL Maneuver Technology Demonstrator; aerospace computing; aerospace simulation; air-to-air tasks; aircraft failure; flight control; landing; pilot vehicle interface; pilot-in-the-loop motion base simulation; safety; short takeoff and landing; takeoff; Aerospace control; Aerospace engineering; Aerospace safety; Aerospace simulation; Air safety; Aircraft propulsion; Automotive engineering; Hardware; System testing; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace and Electronics Conference, 1989. NAECON 1989., Proceedings of the IEEE 1989 National
  • Conference_Location
    Dayton, OH
  • Type

    conf

  • DOI
    10.1109/NAECON.1989.40240
  • Filename
    40240