Patent ID: 11932222
Assignee: GOODRICH CORPORATION
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 6:
7. A method for brake control, comprising:
receiving, by a brake control unit, an axle acceleration signal indicative of at least one of an axle acceleration or an axle deceleration from the accelerometer;
determining whether an aircraft speed is less than a threshold speed value;
monitoring acceleration oscillations by determining whether the axle acceleration is greater than a threshold acceleration value, in response to the aircraft speed being less than the threshold speed value, and determining whether the axle deceleration is greater than the threshold acceleration value, in response to the aircraft speed being less than the threshold speed value; and
decreasing, by the brake control unit, a braking command pressure in response to the axle acceleration and the axle deceleration being greater than the threshold acceleration value, wherein a braking force applied to a wheel is reduced in response to the brake control unit decreasing the braking command pressure.