Application of technique described as model-controlled method (termed adaptive or semi-adaptive when applied to autopilots) for providing aircraft with variable stability and control characteristics is shown; development of variable stability helicopter using method is treated to illustrate significant design parameters and to demonstrate advantages of method over more customary approach.


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    Titel :

    Model-controlled method for development of variable-stability aircraft


    Weitere Titelangaben:

    AGARD -- Report


    Beteiligte:
    Gould, D.G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    32 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Variable Stability Aircraft

    G. Klopfstein | NTIS | 1966


    Variable stability aircraft

    Klopfstein, G. | NTRS | 1968



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