Aircraft control surface controller and associated method

摘要: A control surface controller (200) and a method of controlling interface includes a control for controlling one or more of the aerodynamic surfaces (204) on an aircraft, such as ailerons, spoilers, elevators, rudder. control surface of also include variable resistance damper (220) that provides physical resistance to the in proportion surface interface input rate. Accordingly, resistance provided may be selected in order prevent cause pilot-induced-oscillation or airplane-pilot coupling. The be selected limit servovalve rate which reduces peak transient hydraulic fluid pressure the hydraulic system.