A simulator study was undertaken to compare and evaluate the design features of the electronic displays for possible use in V/STOL aircraft: a combined transition display (Display A), a perspective display (Display B), and a hover display (Display C). Display B presents height information via integrated elements; Displays A and C present information similarly except that Display C presents vertical and lateral guidance via conventional cross pointers. High pilot work load was attained by evaluating the displays only as situational guidance displays in a simulated vehicle without stability augmentation. Glide slopes of 6 and 15 deg were used, and steady-state and no-wind conditions were randomly presented. Six pilots participated, and fifty-five objective performance measures were taken along with pilot opinions
Simulator evaluation of three situation and guidance displays for V/STOL aircraft zero-zero landing approaches
01.07.1978
Sonstige
Keine Angabe
Englisch
Displays for approach and landing of V/STOL aircraft
TIBKAT | 1972
V/STOL displays for approach and landing
TIBKAT | 1972
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