OPTIMAL ENGINE CONTROL WITH TWO DEGREES OF FREEDOM

Abstract

In this paper devoted to the optimal engine control with two degrees of freedom will be processed about jet engine control, where will be described effects of controlled parameters to the regulated parameters. The main contribution of this paper is part, which deals with design of engine control MPM-20 for maximum thrust in every time. There will be described the way of nozzle changing, which is located in laboratory. In conclusion there will be theoretically calculated thrust that we acquired at this optimal control of MPM-20 engine.