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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    Titel :

    Airborne all-weather landing system using Flarescan-ILS guidance


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Moses, K. (Autor:in) / Doniger, J. (Autor:in)

    Kongress:

    SAE Meeting ; 1962 Landing



    Erscheinungsdatum :

    1962


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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

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




    Advanced Scanning Beam Guidance System for All Weather Landing

    L. N. Spinner / V. L. Bencivenga | NTIS | 1968


    Airborne Monocular Vision Guidance Method for Autonomous Landing

    Wang, Qiufu / Bi, Daoming / Huang, Hui et al. | Springer Verlag | 2023