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
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