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Head-up displays for STOL visual approachesA simulation study was conducted to determine the effectiveness of a simple head-up display in improving glide-slope tracking performance during steep visual approaches in a STOL aircraft. The head-up display featured an attitude-stabilized horizon bar and glide-slope reference bar parallel to and 7.5 deg below the horizon bar. On some approaches a flight-path marker symbol showing the projected ground impact point was also displayed. Half of the approaches were flown in a conventional mode in which the pilot changed pitch attitude to correct for height errors. The remaining approaches were flown in a direct-lift mode in which the pilot modulated thrust to change the flight-path angle without pitching the aircraft.
Document ID
19730024219
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Palmer, E. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Cronn, F. W.
(San Jose State Univ.)
Date Acquired
August 7, 2013
Publication Date
January 1, 1972
Publication Information
Publication: STOL Technol.
Subject Category
Instrumentation And Photography
Accession Number
73N32952
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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