To evaluate advanced research concepts relating to navigation, guidance, and control of a helicopter, a mathematical model is required. In this paper we describe a technique for determining the trims and quasistatic derivatives of a tandem rotor helicopter using a linear perturbation model with a simplified rotor system mathematical model. The results of this model show an acceptable agreement with referenced values.


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    Titel :

    Trim Calculation of Tandem Rotor Helicopter Using Simplified Rotor System Mathematical Model


    Beteiligte:
    M. Hwang (Autor:in) / K. Lee (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    5 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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