Patent ID: 9577850
Date: 2017-02-21
CPC Classifications: B60T,B64C,H04L

Claim:
1. A method of control actuation smoothing comprising: receiving, by an aircraft brake and steering controller (“ABSC”) comprising a processor and a non-transitory memory, target performance data; receiving, by the ABSC, a force command comprising a braking instruction; comparing, by the ABSC, the force command to an expected brake behavior; determining, by the ABSC, an error between the force command and the expected brake behavior; filtering, by the ABSC, the force command in response to the error and target performance data; outputting, by the ABSC, a smoothed force command in response to the filtering; and translating, by the ABSC and via an electric brake actuator, a brake assembly based on the smoothed force command, the translating the brake assembly occurring after the outputting the smoothed force command.