A computer study was performed to assess the accuracy of three brake pressure-torque mathematical models. The investigation utilized one main gear wheel, brake, and tire assembly of a McDonnell Douglas DC-9 series 10 airplane. The investigation indicates that the performance of aircraft antiskid braking systems is strongly influenced by tire characteristics, dynamic response of the antiskid control valve, and pressure-torque response of the brake. The computer study employed an average torque error criterion to assess the accuracy of the models. The results indicate that a variable nonlinear spring with hysteresis memory function models the pressure-torque response of the brake more accurately than currently used models.


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    Titel :

    Dynamics of aircraft antiskid braking systems


    Beteiligte:
    Tanner, J. A. (Autor:in) / Stubbs, S. M. (Autor:in) / Dreher, R. C. (Autor:in) / Smith, E. G. (Autor:in)

    Erscheinungsdatum :

    01.02.1982


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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