SYSTEM OF AUTOMATIC CONTROL OF THE AIRCRAFT AT THE CLIMB AND STABILIZATION OF THE TOTAL HEIGHT OF THE FLIGHT Russian patent published in 2017 - IPC B64C13/18 G05D1/04 

FIELD: aviation.

SUBSTANCE: system of automatic control of the aircraft in the recruitment and stabilization Altitude contains sensors the desired and actual speed of the aircraft, seven adders, six large-scale units, integrator, steering gear, steering wheel height sensor longitudinal overload sensor normal overload, sensor angle of attack sensor vertical Aircraft speed sensors desired and actual flight altitude calculation unit trigonometric functions, two signal multiplying block, two blocks forming a predetermined overload signal block signal limit value, logic block, the switch block signal mining predetermined overload, two filters, an additional block signal limit value, connected in a certain way.

EFFECT: improved accuracy, speed, reliability and safety of piloting.

3 cl, 3 dwg