A controller for a brake may comprise an error detector configured to determine an error in a motor angular position signal and a synthetic angle generator configured to generate a synthetic motor angular position signal. The controller may control an actuator motor via the synthetic motor angular position signal in response to the error in the motor angular position signal being determined. In various embodiments, the synthetic motor angular position may cause the controller to retract an electromechanical brake actuator.
FAILSAFE SYNTHETIC ANGLE GENERATION ALGORITHM FOR AIRCRAFT ELECTRIC BRAKING SYSTEM
2019-01-31
Patent
Electronic Resource
English
FAILSAFE SYNTHETIC ANGLE GENERATION ALGORITHM FOR AIRCRAFT ELECTRIC BRAKING SYSTEM
European Patent Office | 2020
|European Patent Office | 2024
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