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 :

    A flight-test evaluation of a go-around control system for a twin engine powered-lift STOL airplane


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

    Erscheinungsdatum :

    01.10.1983


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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