Abstract
Pilot’s perception of variables presented on the Electronic Flight Instrument System, EFIS, has been investigated. A stimulus response technique has been used to determine the accuracy and speed of the perception process. By varying the exposure time of the stimuli, it has been shown that the perception of the variable magnitude is faster and more accurate than the perception of the first derivative or rate of that variable. Results of experiments on roll and pitch attitude perception, the influence of scale division, and the perception of the indicated airspeed are shown.
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