The attitude director indicator system utilizes cathode-ray tube image generation techniques to provide an attitude-director display with a high degree of flexibility. The display includes roll and pitch attitude, roll, pitch and yaw command, glide slope deviation, crab angle and radar altitude, and indications of failures. (Author)
Attitude Director Indicator System for FAA All-Weather Landing System
1969
30 pages
Report
Keine Angabe
Englisch
METHOD OF DISPLAYING AN "ATTITUDE DIRECTOR INDICATOR" IN A HEAD VIEWING SYSTEM FOR AIRCRAFT
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