FIELD: instrument making.
SUBSTANCE: control system comprises angle sensor, angular speed sensor, angle setter, comparison unit, digital-to-analog converter, summing amplifier, actuating device and element of feedback delay. Value of delay time τde of feedback delay element makes τde=(0.1÷0.4)τc, where τc - value of aircraft time constant.
EFFECT: expansion of functional capabilities.
1 dwg
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