METHOD FOR CONTROLLING ELEVATOR OF AIRCRAFT Russian patent published in 2019 - IPC B64C13/00 G05D1/00 

FIELD: control systems.

SUBSTANCE: invention relates to a method for controlling the elevator of an aircraft. To control the elevator, the pitch angle, the roll angle, the overload vector, the angular velocity vector, the complex velocity parameters, the deviation angles of the control surfaces of the aircraft are measured, the correction signals of the increment of the normal overload and the angular velocity of the pitch is determined, the specified value of the increment of normal overload is determined, the values of the positional and integral control signals is calculated, the control signal of the elevator drive is formed in a certain way, the control signal is transmitted to the elevator drives.

EFFECT: enhanced stability, manageability and safety, as well as reduced aerodynamic loads.

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