A Stability and Control Augmentation System (“SCAS”) module comprising one or more SCAS actuators, the or each SCAS actuator comprising a mechanical component that translates rotational motion to linear motion along a first axis of said SCAS; one or more electric motors for driving linear movement of the mechanical component in response to a command signal; and one or more angular transducers to detect the position of the SCAS actuator along the first axis.
SERVO-ACTUATOR ARCHITECTURE WITH ELECTROMECHANICAL-STABILITY AND CONTROL AUGMENTATION SYSTEM
2021-08-19
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
SERVO-ACTUATOR ARCHITECTURE WITH ELECTROMECHANICAL-STABILITY AND CONTROL AUGMENTATION SYSTEM
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