Development of a control system for an aeronautical engine

Valenti, Carlo Alberto (2019) Development of a control system for an aeronautical engine. [Laurea magistrale], Università di Bologna, Corso di Studio in Aerospace engineering / ingegneria aerospaziale [LM-DM270] - Forli', Documento full-text non disponibile
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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.

Tipologia del documento
Tesi di laurea (Laurea magistrale)
Autore della tesi
Valenti, Carlo Alberto
Relatore della tesi
Corso di studio
Ordinamento Cds
Parole chiave
Simulink, LabVIEW, engine control, software-in-the-loop
Data di discussione della Tesi
21 Marzo 2019

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