Improved methods and systems for controlling hydraulically or electrically actuated anti-lock
brake systems (ABS) on air and land vehicles requiring only measurement of wheel angular speed although
brake torque measurements can also be employed if available. A sliding mode observer (SMO) based estimate of net or different wheel torque (road / tire torque minus applied
brake torque) derived from the measured wheel speed is compared to a threshold differential wheel torque derived as a function of a “skid
signal” also based on wheel speed only to generate a braking
control signal. The braking
control signal can be employed to rapidly and fully applying and releasing the brakes in a binary on-off manner and, as an additional option, possibly modulating the maximum available brake
hydraulic pressure or
electrical current when the brakes are in the “on” state in a continuous manner. In the case of the basic on-off component of braking, the brakes are released when the estimate of differential wheel torque is less than the threshold differential wheel torque (i.e. for relatively high values of
brake torque), and the brakes are applied fully when the estimate of differential wheel torque is greater than or equal to the threshold differential wheel torque. For
aircraft landing gear applications, a fore-aft
accelerometer mounted on the
landing gear can be used to suppress nonlinear gear displacement oscillations commonly called gear
walk in the direction of wheel roll.