An aircraft includes a first landing gear assembly, a second landing gear assembly, a braking circuit, a brake control circuit, and a braking capability circuit. The landing gear assemblies each include a first braking wheel and a second braking wheel. The braking circuit may apply brakes independently to each of the braking wheels. The brake control circuit actuates braking of the first braking wheels in response to initial receipt of a braking command in a first braking phase and restrict braking at the second braking wheels during the first braking phase until the first braking wheels reach an anti-skid limit at an end of the first braking phase. The braking capability circuit determines a braking capability of the aircraft based on an amount of braking applied to reach the anti-skid limit at the first braking wheels.


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    Title :

    VEHICLE BRAKING CAPABILITY DETERMINATION BY BRAKING WITH FEWER THAN ALL AVAILABLE BRAKING WHEELS


    Additional title:

    BREMSFÄHIGKEITSBESTIMMUNG EINES FAHRZEUGS DURCH BREMSEN MIT WENIGER ALS ALLEN VERFÜGBAREN BREMSRÄDERN
    DÉTERMINATION DE LA CAPACITÉ DE FREINAGE D'UN VÉHICULE PAR UN FREINAGE AVEC MOINS DE LA TOTALITÉ DES ROUES DE FREINAGE DISPONIBLES


    Contributors:

    Publication date :

    2023-07-05


    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