Design of intelligent control systems of gas-turbine engine on the basis of minimal complexity principle

Abstract

A problem solutionofmethodology and theoretic basis ofdesignofintelligentcontrolsystems ofcomplexdynamic objects on the basis of system analysis and structural optimization of hierarchical levels of control with application of minimal complexity is discussed. Peculiarities of realization of proposed approaches in designing process ofcontrol systems of aviation engines are presented.