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.
Index Terms—Analysis, control, coupling methods,
modeling, simulation.
C. Le Brun, E. Godoy and D. Beauvois are with the Automatic Control
Department of Supelec, Gif-sur-Yvette, France (e-mail: {christophe.lebrun,
emmanuel.godoy,dominique.beauvois}@supelec.fr).
G. Le Pacheis with the System Division of SNECMA (SAFRAN group),
Villaroche, France (e-mail: gwenole.lepache@snecma.fr).
R. Noguera is with the DynFluid Laboratory of Arts & Métiers ParisTech,
Paris, France (e-mail: ricardo.noguera@ensam.eu).
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Cite:C. Le Brun, E. Godoy, D. Beauvois, G. Le Pache, and R. Noguera, "Modeling and Analysis of a Turbojet Fuel System," International Journal of Computer Theory and Engineering vol. 6, no. 3, pp. 260-266, 2014.
