The present invention relates to a Stability and Command Augmentation System (SCAS) (10) for an aircraft, such as an aeroplane or a helicopter. According to the invention, there is provided a SCAS (10) for an aircraft, the SCAS comprising: a first input shaft (22) providing a first rotational input; a second input shaft (28) providing a second rotational input; and a device for summing the first and second rotational inputs to give a rotational output for controlling an actuator.


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    Title :

    Stability and control augmentation system


    Additional title:

    Stabilität und Steuerungssteigerungssystem
    Système d'augmentation de stabilité et de commande


    Contributors:

    Publication date :

    2019-07-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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