Abstract

This article discusses the automatic control system for parameters (rotor speed and gas temperature) of a gas turbine engine based on clear logic controllers. It is proposed to use clear logical controllers, consisting of a comparing device, a fuzzifier, an inference block with a system of production rules and with given membership functions of clear terms of variables, and a defuzzifier. Precise logical controllers, using the membership functions of precise terms, in the control loops of the object’s influence stably maintain the overshoot time.

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