Intelligent Controller of Helicopter Turboshaft Engines’ Gas Temperature with Compensation of Transient Process’s Inertial Delays and Optimization

This research presents the development of an intelligent controller for the helicopter turboshaft engines gas temperature, aimed at compensating for the measuring sensor’s inertial delays and optimizing transient processes. The aim is to compensate for inertial delays τ ≈ 0.025 seconds and optimi…