Root locus method for examining influence of structural coupling on stability of uncontrolled aircraft is presented; graphical technique permits rapid but accurate quantitative evaluation of effects of changes in aeroelastic and aerodynamic characteristics on aircraft stability; problems involved in integrating flexible vehicle into automatic flight control system; similarity of problem as it exists in manned aircraft and multistage missiles; examples illustrate linear control design approach; promising new approach utilizing adaptive (nonlinear control) techniques.


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    Titel :

    Influence of structural elasticity on stability of airplanes and multi-stage missiles


    Weitere Titelangaben:

    AGARD -- Report


    Beteiligte:
    Prince, L.T. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Format / Umfang :

    50 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :