An antiskid brake control system, comprising: a brake control unit, BCU (150); a wheel/brake assembly (132,134) comprising a wheel (24), a brake stack (26), and an actuator (28) configured to apply a braking force onto the brake stack; and a wheel speed sensor (27) in electronic communication with the BCU, the wheel speed sensor configured to detect a wheel speed corresponding to the wheel; wherein the BCU is configured to: receive an aircraft mass from an avionics unit; calculate an aircraft kinetic energy; generate an antiskid brake command signal based upon the aircraft kinetic energy; and send the antiskid brake command signal to a brake control component for controlling the braking force.


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    Title :

    SYSTEMS AND METHODS FOR AIRCRAFT ANTISKID BRAKING


    Additional title:

    SYSTEME UND VERFAHREN FÜR ANTIRUTSCH-BREMSUNG VON FLUGZEUGEN
    SYSTÈMES ET PROCÉDÉS DE FREINAGE ANTIPATINAGE D'AÉRONEF


    Contributors:

    Publication date :

    2023-06-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF



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    Dynamics of Aircraft Antiskid Braking Systems

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


    Dynamics of aircraft antiskid braking systems

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