METHOD FOR CONTROLLING VIBRATION INDUCED IN AN AIRCRAFT BY THE ROTATING OPERATION OF A BLOWER AND ELECTRIC FLIGHT CONTROL SYSTEM USING THE SAME

摘要

The method involves calculating an electric order of additional control for enabling a servo-control of a moving surface to resist induced vibrations. An electric order of flight control is added with the electric order of an additional control to obtain an order of global control for the surface. The servo-control is temporarily subjected to the order of global control. An independent claim is also included for an electronic flight control system.