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
Link To Document :
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