Innovative outputs from the Laboratory of Intelligent Control Systems of Aircraft Engines

Abstract

Summary form only given. The Laboratory of Intelligent Control Systems of Aircraft Engines has been built around the idea of design implementation and testing of progressive algorithms in the areas of identification, modeling, control and diagnostics of complex systems. As such complex system a class of small turbojet engines suitable for laboratory experiments and utilization has been used, the engine MPM-20 derived from turbo-starter TS-20 in particular. Such small turbojet engines exhibit similar dynamic behavior as normal sized engines and have many properties of complex systems like non-linear characteristics, variable cross bindings, broad operational range, non stationary parameters and elements of stochastic behavior.