AIRCRAFT BRAKE CONTROL ARCHITECTURE HAVING IMPROVED ANTISKID REDUNDANCY

摘要

According to the present invention, an electromechanical braking system (10) is provided. The braking system (10) includes at least one brake system control unit (BSCU (20)) for converting an input brake command signal into a brake clamp force command signal. In addition, the braking system (10) includes a first electromechanical actuator controller (EMAC (26)) and a second electromechanical actuator controller (EMAC) configured to receive the brake clamp force command signal from the at least one BSCU (20) and. to convert the brake clamp force command signal to at least one electromechanical actuator drive control signal. Further, the braking system (10) includes at least one electromechanical actuator (18) configured to receive the at least one drive control signal and to apply a brake clamp force to at least one wheel (12-15) to be braked in response to the at least one drive control signal. Moreover, the first EMAC (24) and the second EMAC (26) are configured to perform antiskid control in relation to the at least one wheel (12-15) to be braked.