Details of operation of Flarescan controller used by FAA as part of program to evaluate Flarescan guidance system for all-weather landing; description of throttle control system compatible with Flarescan; simulation studies of basic system parameters such as transmitter location, glide slope angle, scan rate, winds, beam noise, and early and late flare engagements; flight test evaluation of Flarescan and problem areas discovered; changes in coupler design proposed to reduce dispersions due to variations in system parameters.
Airborne all-weather landing system using Flarescan-ILS guidance
SAE -- Paper
SAE Meeting ; 1962 Landing
1962
7 pages
Conference paper
English
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An Airborne All - Weather Landing System Using Flarescan - ILS Guidance
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