Uproszczony model matematyczny układu sterowania jednowirnikowym turbinowym silnikiem odrzutowym – silnik SO-3 – z uwzględnieniem stanów awaryjnych

The paper presents a synthesized physical model of SO-3 turbojet engine control system. On the basis of the physical model it also gives a mathematical model which contains all the constituent elements are shown in the form of polynomials of the n-degree. In addition to this the present work includes an algorythm of the model which consider the basic stages of break – down.