Aircraft brake control system

An aircraft brake control system for controlling anti-skid braking of at least first and second wheels in a wheel set of an aircraft, the system comprising a control assembly having:

• wheel speed inputs including:
• an input of an indication of the wheel speed of one or more wheels, and
• determining a threshold value at which the one or more wheels is unlikely to skid, and
• an anti-skid output for maintaining the one or more wheels within the threshold value, wherein the control assembly also has one or more inputs providing an indication of whether or not a wheel of the wheel set has skidded, and wherein the output is a selective output configured to indicate:
• a wheel speed other than the lowest wheel speed, if a wheel skid is not indicated, and
• the lowest wheel speed, if a wheel skid is indicated.