FIELD: tool-making industry, possible use in systems for automatic control of aircrafts under conditions of changing setting effects by sign and value.
SUBSTANCE: method for integrating control signal for astatic systems for controlling aircrafts includes setting control signal for integration, integrating current integration signal and integrated signal is scaled, scaled signal is amplified, amplified signal is inverted, threshold signal ε≥0 is set, setting control signal is multiplied with scaled signal, multiplication signal is compared to threshold signal, check connection signal is formed, equal to inverse signal during excess of multiplication signal over threshold signal, current integration signal is formed, equal to total of setting signal and check connection signal, and scaled integrated signal is limited. Device for realization of method contains integration signal set-point device, adder, integrating link, scaling amplifier, signal limiter, inverting amplifier, controlled key, multiplication block, relay element, threshold signal set-point device.
EFFECT: increased dynamic precision and simplified construction of device.
2 cl, 1 dwg
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