An automatic go-around control system was evaluated on the Augmentor Wing Jet Short Takeoff and Landing (STOL) Research Airplane (AWJSRA) as part of a study of an automatic landing system for a powered-lift STOL airplane. The results of the evaluation indicate that the go-around control system can successfully transition the airplane to a climb configuration from any initiation point during the glide-slope track or the flare maneuver prior to touchdown.


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    Titel :

    Flight-Test Evaluation of a Go-around Control System for a Twin Engine Powered-Lift STOL Airplane


    Beteiligte:
    D. M. Watson (Autor:in) / G. H. Hardy (Autor:in)

    Erscheinungsdatum :

    1983


    Format / Umfang :

    21 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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