Reference is made to flight tests of VJ101C VTOL, built by EntwicklungsringSued (EWR) for German Defense Ministry; flight and simulator experience gained from program emphasize need for stability augmentation in at least pitch and roll axes; other features, such as control stick steering and engine failure protection, were also provided; since some of flights were performed on telescopic simulator, range of control parameters could be expanded to permit wider range and better separation of control variables; all three phases of VJ101 program as well as three distinct prototypes are described.


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    Titel :

    Problems unique to VTOL automatic flight control


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Mueller, L.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Automatic flight control for VTOL aircraft

    Mueller, L.J. | Engineering Index Backfile | 1966



    VTOL flight control in 1980

    DENDY, J. / TRIBKEN, E. | AIAA | 1968