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Initial flight and simulator evaluation of a head up display for standard and noise abatement visual approachesA preliminary assessment was made of the adequacy of a simple head up display (HUD) for providing vertical guidance for flying noise abatement and standard visual approaches in a jet transport. The HUD featured gyro-stabilized approach angle scales which display the angle of declination to any point on the ground and a horizontal flight path bar which aids the pilot in his control of the aircraft flight path angle. Thirty-three standard and noise abatement approaches were flown in a Boeing 747 aircraft equipped with a head up display. The HUD was also simulated in a research simulator. The simulator was used to familiarize the pilots with the display and to determine the most suitable way to use the HUD for making high capture noise abatement approaches. Preliminary flight and simulator data are presented and problem areas that require further investigation are identified.
Document ID
19730009294
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bourquin, K.
(NASA Ames Research Center Moffett Field, CA, United States)
Palmer, E. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Cooper, G.
(NASA Ames Research Center Moffett Field, CA, United States)
Gerdes, R. M.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1973
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-62187
Report Number: NASA-TM-X-62187
Accession Number
73N18021
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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