Methods of automatically controlling the airplane are reviewed. Equations for the controlled motion including inertia effects of the control are developed and methods of investigating the stability of the resulting fifth and higher order equations are presented. The equations for longitudinal and lateral motion with both ideal and non-ideal controls are developed in dimensionless form in terms of control parameters based on simple dynamic tests of the isolated control unit.


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    Titel :

    Theory of automatic control of airplanes


    Beteiligte:

    Erscheinungsdatum :

    01.04.1939


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



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