Flight Director System utilized on C-141A "StarLifter" was developed as part of all weather landing system (AWLS) which is FAA certified for Category II weather minimums; AWLS system has successfully demonstrated manual operation to touchdown and is now operational in Air Force Military Airlift Command; flight director system incorporates some new internal computation techniques, includes increased number of operating modes over predecessor systems, and extends use through flare maneuver. (32398)


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    Titel :

    C-141A flight director system


    Weitere Titelangaben:

    ASME -- Aviation Space -- Progress Prospects


    Beteiligte:
    Person, S.D. (Autor:in)

    Kongress:

    ASME Annual Aviation and Space Conference ; 1968 ; United States , Beverly Hills, CA Control equipment



    Erscheinungsdatum :

    1968


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    An Analysis of Flight Test Data on the C-141A Aircraft

    Paterson, J. H. / Blackerby, W. T. / Schwanebeck, J. C. et al. | NTRS | 1970


    C-141A development test program

    SHOCKLEY, E. | AIAA | 1967


    C-141A Pitot-Static System Calibration Tests

    R. K. Pomeroy / H. Klein / J. A. Guthrie et al. | NTIS | 1976