05 - Propulsion
APPLICATION OF "VIRTUAL" CONTROLLERS FOR INTEGRATED PROPULSION AND AIRCRAFT CONTROL
O.S. Gurevich¹, F.D. Golberg¹, S.A. Smetanin¹, N.E. Romanenko¹; ¹Central Institute of Aviation Motors, Russia
It describes a new approach to the gas turbine engine control, based on the use of the engine mathematic model, which are built in the automatic control system, providing engine performance improvement by deeper control integration of a power plant and an aircraft.