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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Dynamics of Aircraft Antiskid Braking Systems


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

    Erscheinungsdatum :

    1982


    Format / Umfang :

    100 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Dynamics of aircraft antiskid braking systems

    Tanner, J. A. / Stubbs, S. M. / Dreher, R. C. et al. | NTRS | 1982


    Intelligent Aircraft Antiskid Braking Systems – A Review

    Sudheendra, P. / Bhat, Vinayambika S. | Springer Verlag | 2024


    SYSTEMS AND METHODS FOR AIRCRAFT ANTISKID BRAKING

    GEORGIN MARC | Europäisches Patentamt | 2023

    Freier Zugriff

    Systems and methods for aircraft antiskid braking

    GEORGIN MARC | Europäisches Patentamt | 2024

    Freier Zugriff

    SYSTEMS AND METHODS FOR AIRCRAFT ANTISKID BRAKING

    GEORGIN MARC | Europäisches Patentamt | 2021

    Freier Zugriff