| 主权项 |
1. A brake control system for a landing gear of an aircraft, comprising:
a first control channel configured to provide brake control signals to one or more brakes on the landing gear, wherein the first control channel comprises a first controller that controls an operation of the one or more brakes, wherein the first control channel receives braking commands from a brake pedal; a second control channel configured to provide brake control signals to another one or more brakes on the landing gear, wherein the second control channel comprises a second controller that controls an operation of the another one or more brakes, wherein the second control channel receives braking commands from the brake pedal; wherein at least one of the first control channel and the second control channel is configured to act as an executive in monitoring braking efforts applied by the one or more brakes as compared to braking efforts applied by the another one or more brakes, wherein the control channel configured to act as the executive determines a correction factor and wherein the control channel configured to act as a non-executive causes the braking efforts of at least one of the one or more brakes or the another one or more brakes to be modified in accordance with the correction factor. |
