Development of a control system for an aeronautical engine

The goal of this thesis is to develop a control system for an aeronautical engine. In particular, the engine considered is an automotive one which will be adapted for aeronautical purposes. Therefore, the engine control unit is built in Simulink®, starting from a model in LabVIEW®. The purpose of this unit is to control the engine next cycle parameters and its setpoints. Then, in order to test its effectiveness a simplified engine model is built and the whole system is tested, after a first trial of the control system. The results are presented and discussed.