Modeling and Analysis of a Turbojet Fuel System
Abstract
The aim of this paper is to study a new concept of fuel system of a turbojet, to design its control system and to validate its behavior using simulation. AMESim is used to represent the physical system and Simulink has been adopted for the implementation of the control laws. A multi-loop PID strategy is then selected. Simulation tools and different methods of their couplings, including exchange, cosimulation and FMI are benchmarked to find which strategy is the best suitable.