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.
Stability and control augmentation system
Stabilität und Steuerungssteigerungssystem
Système d'augmentation de stabilité et de commande
2019-07-17
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |