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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    Title :

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


    Contributors:

    Publication date :

    1983-10-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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