In this paper, the ground maneuver of aircraft anti-skid braking is studied using co-simulation method, which joints the software MSC.ADAMS/Aircraft with MATLAB/Simulink. A virtual prototype of aircraft is established in the multibody system dynamics software MSC.ADAMS/Aircraft. The anti-skid braking control model, which adopts the multi-threshold PID control method with a slip-velocity-controlled, pressure-bias-modulated(PBM) system, is established in MATLAB/Simulink. The ADAMS model is then connected to block diagrams of the anti-skid braking control model in MATLAB/Simulink, so that the ground maneuver of aircraft anti-skid braking is simulated. Results are presented to investigate the performance of anti-skid braking system and responses of aircraft induced by braking. The brake system has good control effect on braking the aircraft, but its performance gets down in low speed stage, which brings on serious skid.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Research on modelling and simulation for aircraft anti-skid braking


    Beteiligte:
    Zhang Ming, (Autor:in) / Nie Hong, (Autor:in) / Wei Xiao-hui, (Autor:in) / Zhou Enzhi, (Autor:in)


    Erscheinungsdatum :

    2008-12-01


    Format / Umfang :

    702230 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






    Landing response of aircraft with optimal anti-skid braking

    Yadav, D. / Singh, C.V.K. | Tema Archiv | 1995


    Aircraft Anti-skid Braking Control Based on Reinforcement Learning

    Jiao, Zongxia / Bai, Ning / Sun, Dong et al. | IEEE | 2023