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
SERVO-AKTUATORARCHITEKTUR MIT ELEKTROMECHANISCHER STABILITÄT UND STEUERUNGSERWEITERUNGSSYSTEM
ARCHITECTURE DE SERVO-ACTIONNEUR COMPORTANT UN SYSTÈME D'AUGMENTATION DE COMMANDE ET DE STABILITÉ ÉLECTROMÉCANIQUE
2023-05-10
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Servo-actuator architecture with electromechanical-stability and control augmentation system
European Patent Office | 2023
|SERVO-ACTUATOR ARCHITECTURE WITH ELECTROMECHANICAL-STABILITY AND CONTROL AUGMENTATION SYSTEM
European Patent Office | 2021
|A global sliding mode controller for missile electromechanical actuator servo system
SAGE Publications | 2014
|A global sliding mode controller for missile electromechanical actuator servo system
Online Contents | 2014
|