A mathematical model of the Sikorsky SH-3G helicopter based on classical nonlinear, quasi-steady rotor theory was developed. The model was validated statically and dynamically by comparison with Navy flight-test data. The model incorporates ad hoc revisions which address the ideal assumptions of classical rotor theory and improve the static trim characteristics to provide a more realistic simulation, while retaining the simplicity of the classical model.


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    Title :

    Mathematical model of the SH-3G helicopter


    Contributors:

    Publication date :

    1982-12-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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