IMPLEMENTATION OF AN ANALYTICAL MODEL OF COMPRESSOR OF SMALL JET ENGINE TO ITS CONTROL SYSTEM

Abstract

The thesis is focused on the transformation of existing mathematical model for calculating the parameters of the engine compressor ISTC-21V, which will serve to manage and diagnose engine in real time. The engine is located in the laboratory of intelligent control systems for aircraft engines in areas Faculty of Aeronautics. Existing mathematical model is created using Matlab, but motor control is carried out at laboratories in Simulink. Start of work is devoted to describing the object management software tool used Matlab / Simulink, while this chapter is an analysis of the issue. Other chapters deal with specific transformation, modifying and implementing existing matematickéh. The content of the thesis is a detailed description of the type of transformation in Matlab Simulink. The modification of an existing mathematical model required, as calculated by a compressor which is suitable for the management of the engine. The final section describes the implementation of the modified and transformed into a mathematical model of situational engine management ISTC-21V.