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Simulator study of pilot-aircraft-display system response obtained with a three-dimensional-box pictorial displayThe effect of varying the two important display parameters of a pictorial display on pilot opinion performance, and pilot aircraft display system servomechanism response is examined. The display presents a picture of a three dimensional box that moves along the desired path ahead of the aircraft. The two display parameters examined are the field of view of the picture (from + or - 5 deg to + or - 45 deg) and the distance to the box (from 92 m (300 ft) to 6100 m (20 000 ft)). The results show that the pilots prefer a distance to the box of 915 m (3000 ft) and a field of view of + or - 30 deg. The best performance, both in the sense of quickness of error correction and lowest standard deviation, is obtained with a distance to the box of 92 m (300 ft) and a field of view of + or - 15 deg. A pilot model analysis is used to determine the gains used by the pilots and the servomechanism response characteristics of the pilot aircraft display system.
Document ID
19840005114
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Adams, J. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1983
Subject Category
Aircraft Instrumentation
Report/Patent Number
NAS 1.60:2122
L-15632
NASA-TP-2122
Report Number: NAS 1.60:2122
Report Number: L-15632
Report Number: NASA-TP-2122
Accession Number
84N13182
Funding Number(s)
PROJECT: RTOP 505-35-23-30
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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