AIRCRAFT BRAKING SYSTEM HAVING HIGH LEVEL OF AVAILABILITY

An aircraft braking system comprising: a first group (Ga) of actuators and a second group (Gb) of actuators. A first control module (105a) is adapted, in a nominal mode, to control the first group, and in a reconfigured mode, to control the first group and the second group. A second control module (105b) is adapted, in a nominal mode, to control the second group, and in a reconfigured mode, to control the first group and the second group. A monitoring unit adapted is adapted to monitor the first control module and the second control module, and to put the first control module into the reconfigured mode of operation when the monitoring unit detects a failure of the second control module, and to put the second control module into the reconfigured mode when the monitoring unit detects a failure of the first control module. 种飞行器制动系统，包括：第组(Ga)致动器和第二组(Gb)致动器；第控制模块(105a)和第二控制模块(105b)，所述第控制模块(105a)被适配成：在标称模式下，控制所述第组，并且在重配置模式下，控制所述第组和所述第二组，所述第二控制模块(105b)被适配成：在标称模式下，控制所述第二组，并且在重配置模式下，控制所述第组和所述第二组；监视单元，所述监视单元被适配成：监视所述第控