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.


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    Title :

    Airborne all-weather landing system using Flarescan-ILS guidance


    Additional title:

    SAE -- Paper


    Contributors:
    Moses, K. (author) / Doniger, J. (author)

    Conference:

    SAE Meeting ; 1962 Landing



    Publication date :

    1962


    Size :

    7 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    An Airborne All - Weather Landing System Using Flarescan - ILS Guidance

    Doniger, J. / Moses, K. | SAE Technical Papers | 1962




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