FIELD: aviation.
SUBSTANCE: aircraft automatic control system at reduction of circle height at stabilization stage contains navigation and measurement system, two scaling units, five adders, two nonlinear units, an integrator, a signal multiplying unit, a longitudinal transfer control automatic device, a steering drive, a height elevator, two switches, a circle height setting device, an aircraft flight speed sensor, a logic unit connected to a certain method.
EFFECT: higher safety of piloting due to elimination of deviations along height below preset height of circle, improved dynamic characteristics.
1 cl, 4 dwg
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