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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Contributors:
    D. M. Watson (author) / G. H. Hardy (author)

    Publication date :

    1983


    Size :

    21 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    CONCEPT OF MEDIUM TWIN-ENGINE STOL TRANSPORT AIRPLANE

    Pavlenko, O. / Petrov, A. / Pigusov, E. | British Library Conference Proceedings | 2018


    Flight Reference Display for Powered-Lift STOL Aircraft

    K. Tanaka / K. Funabiki / M. Nakamura et al. | NTIS | 1994