• DocumentCode
    2475784
  • Title

    Description and flight test of a rollout and turnoff (ROTO) head-up display (HUD) guidance system

  • Author

    Hueschen, Richard M. ; Hankins, Walter W. ; Barker, L. Keith

  • Author_Institution
    NASA Langley Res. Center, Hampton, VA, USA
  • Volume
    2
  • fYear
    1998
  • fDate
    31 Oct-7 Nov 1998
  • Abstract
    The ROTO system provided guidance that resulted in mean ROT values essentially the same as those for current clear-weather operations and standard deviation ROT values a factor of 1.5 to 2.0 less (depending on exit comparison). Assuming the pilots can follow the guidance in low visibility conditions, these ROT values imply that clear-weather runway capacity could be maintained in low visibility conditions. All the pilots liked the system and found the guidance easy to follow after a couple of training runs. In general, the pilots were able to control the aircraft ground speed along the runway to within 10 knots of commanded ground speed from the ROTO guidance
  • Keywords
    Global Positioning System; aerospace simulation; aircraft control; head-up displays; aircraft ground speed; clear-weather runway capacity; guidance system; head-up display; low visibility conditions; mean ROT values; rollout and turnoff system; standard deviation ROT values; Aircraft navigation; Airports; Automatic control; Displays; Global Positioning System; Multilevel systems; NASA; Satellite navigation systems; Switches; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 1998. Proceedings., 17th DASC. The AIAA/IEEE/SAE
  • Conference_Location
    Bellevue, WA
  • Print_ISBN
    0-7803-5086-3
  • Type

    conf

  • DOI
    10.1109/DASC.1998.739816
  • Filename
    739816