The nonlinear set of equations which represent helicopter motion is linearized about a prescribed nominal state. Once the linearized system is obtained it is validated by comparing the output of the nonlinear system to that of its linearized counterpart. Having obtained a linear model, linear system theory may then be applied in order to investigate the stability and control characteristics of the aircraft.


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    Titel :

    Helicopter Motion: Equation Linearization


    Beteiligte:
    Fermelia, A. (Autor:in) / Gyorog, D. A. (Autor:in) / Flanigan, V. J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1976-11-01


    Format / Umfang :

    2031333 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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