FIELD: transport.
SUBSTANCE: invention relates to ACS for minimum-phase objects, in particular, aircraft pitch automatic control. Proposed system comprises pitch setting device, first adder, first amplifier, second adder, integrator and angle transducer, parameter transducer, parameter setting device, multiplier and fourth adder. Angle transducer output is connected with first adder second input. Controlled object output is connected via angular speed transducer, differentiator, second amplifier and third adder with second adder second input. Angular speed transducer output is connected via third amplifier with third adder second input. Integrator output is connected via amplifier with adder third input. Parameter transducer output is connected via fourth adder to multiplier second input. Parameter setting device output is connected with fourth adder second input.
EFFECT: improved transition processes.
1 dwg
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