AUTOMATIC FLIGHT CONTROL SYSTEM FOR HIGHLY-MANOEUVRABLE AIRCRAFT Russian patent published in 2012 - IPC G05D1/00 

FIELD: physics.

SUBSTANCE: system includes a computer of given path acceleration values, a normal acceleration sensor, a pitching velocity sensor, a first controlled limiter, a first adder, a second controlled limiter, an integrator, a second, third, fourth and fifth adder, a dynamic limiter, a servo driver, an isodromic filter, a strapdown inertial reference system, a first, second and third functional unit an a 'minimum' circuit.

EFFECT: limiting extreme values of the angle of attack, angular velocity and pitch acceleration, and required control characteristics in the entire range of variation of the control signal.

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