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Evaluation of a computer-generated perspective tunnel display for flight path followingThe display was evaluated by monitoring pilot performance in a fixed base simulator with the vehicle dynamics of a CH-47 tandem rotor helicopter. Superposition of the predicted future vehicle position on the tunnel image was also investigated to determine whether, and to what extent, it contributes to better system performance (the best predicted future vehicle position was sought). Three types of simulator experiments were conducted: following a desired trajectory in the presence of disturbances; entering the trajectory from a random position, outside the trajectory; detecting and correcting failures in automatic flight. The tunnel display with superimposed predictor/director symbols was shown to be a very successful combination, which outperformed the other two displays in all three experiments. A prediction time of 4 to 7 sec. was found to optimize trajectory tracking for the given vehicle dynamics and flight condition. Pilot acceptance of the tunnel plus predictor/director display was found to be favorable and the time the pilot needed for familiarization with the display was found to be relatively short.
Document ID
19810005447
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Grunwald, A. J.
(NASA Langley Research Center Hampton, VA, United States)
Robertson, J. B.
(NASA Langley Research Center Hampton, VA, United States)
Hatfield, J. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1980
Subject Category
Aircraft Instrumentation
Report/Patent Number
NASA-TP-1736
L-13253
Report Number: NASA-TP-1736
Report Number: L-13253
Accession Number
81N13958
Funding Number(s)
PROJECT: RTOP 505-34-23-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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