Robust Control of Small Turbojet Engines

• DOI: 10.3390/machines7010003
• Publication Date: 2019-01-04T16:34:26Z
• Authors: Rudolf Andoga; Ladislav Főző; Radovan Kovács; Károly Beneda; Tomáš Moravec; Michal Schreiner
• Keywords: Turbojet

Modern turbojet engines mainly use computerized digital engine control systems. This opens the way for application of advanced algorithms aimed at increasing their operational efficiency and safety. The theory robust is a set methods known good results in complex tasks, making them ideal candidates current units. Different methodologies design controllers, utilizing small with variable exhaust nozzle designated as iSTC-21v, were therefore investigated article. resulting controllers evaluated laboratory conditions. aim was to find suitable approach method taking into account limitations specifics real its hardware, contrary most studies which have used only simulated environments. article shows effective speed class engines, can be applied discrete environment.