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- W2317202942 abstract "In aeronautics, two of the main key design drivers are the reduction of the fuel consumption and the reduction of its environmental impact. These two considerations are taken into account by both aircraft and engine manufacturers. On the engine regulation system level, the first objective is reached by reducing its mass. The second one can be achieved with a more advanced fuel system. This paper deals with the control of a new fuel system of a turbojet. In comparison with classical fuel systems, a hydraulic equipment of the original system has been removed to reduce the mass, which means that standard control of the turbojet is no more effective. After modeling the new system, its couplings are studied and a controller is designed. This paper is organized as follows: Section II introduces the system and its functioning; the dynamic model is described in Section III and Section IV presents the design of the control system and its performances. Section V compares different methods of simulation, in order to find the most effective one for the system. At last, conclusions are presented in Section VI." @default.
- W2317202942 created "2016-06-24" @default.
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- W2317202942 date "2014-01-01" @default.
- W2317202942 modified "2023-10-17" @default.
- W2317202942 title "Modeling and Analysis of a Turbojet Fuel System" @default.
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- W2317202942 doi "https://doi.org/10.7763/ijcte.2014.v6.872" @default.
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