An aircraft includes a brake lever for receiving a pilot braking input as a lever travel of the brake lever, a braking wheel operatively coupled with the brake lever to brake the aircraft based on the lever travel, a brake actuator operatively coupled with the braking wheel to apply a braking force in response to a braking pressure provided to the brake actuator, and a brake pressure circuit. The brake pressure circuit is configured for: estimating a maximum braking pressure above which the braking wheel will skid with respect to a ground surface; scaling a lever gain of the brake lever to command the maximum braking pressure at a full travel of the brake lever such that a remaining brake lever travel indicates the amount of braking capability remaining for the aircraft; and braking the braking wheel based on the lever gain and the lever travel.
VEHICLE BRAKE PEDAL TRAVEL BASED ON BRAKING FORCE AVAILABLE BETWEEN BRAKING WHEELS AND GROUND
FAHRZEUGBREMSPEDALWEG BASIEREND AUF DER VERFÜGBAREN BREMSKRAFT ZWISCHEN BREMSRÄDERN UND BODEN
COURSE DE PÉDALE DE FREIN DE VÉHICULE BASÉE SUR LA FORCE DE FREINAGE DISPONIBLE ENTRE LES ROUES DE FREINAGE ET LE SOL
09.08.2023
Patent
Elektronische Ressource
Englisch
IPC: | B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF |
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