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Three methods of presenting flight vector information in a head-up display during simulated STOL approachesA simulator study was conducted to determine the usefulness of adding flight path vector symbology to a head-up display designed to improve glide-slope tracking performance during steep 7.5 deg visual approaches in STOL aircraft. All displays included a fixed attitude symbol, a pitch- and roll-stabilized horizon bar, and a glide-slope reference bar parallel to and 7.5 deg below the horizon bar. The displays differed with respect to the flight-path marker (FPM) symbol: display 1 had no FPM symbol; display 2 had an air-referenced FPM, and display 3 had a ground-referenced FPM. No differences between displays 1 and 2 were found on any of the performance measures. Display 3 was found to decrease height error in the early part of the approach and to reduce descent rate variation over the entire approach. Two measures of workload did not indicate any differences between the displays.
Document ID
19750018924
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dwyer, J. H., III
(NASA Ames Research Center Moffett Field, CA, United States)
Palmer, E. A., III
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
A-5992
NASA-TM-X-3273
Report Number: A-5992
Report Number: NASA-TM-X-3273
Accession Number
75N26996
Funding Number(s)
PROJECT: RTOP 504-09-33
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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