Design of H∞ proportional-integral thrust controller for ramjet engine

• Autorzy: Zorić Nemanja Dušan , Radulović Radoslav Danilo , Jazarević Vladimir Miloš , Petrović Trajko Borivoje

Identyfikatory

DOI

10.15632/jtam-pl/126664

• Języki publikacji: EN

Abstrakty

EN

This paper presents the design of a thrust controller for a ramjet engine. The mathematical model for controller synthesis is based on a numerical solution of a set of nonlinear equations. Transfer functions of the engine are found for certain operation points defined by the altitude, Mach number and angle of attack. Local controllers are developed by using H∞ control methodology, finally reduced to proportional-integral (PI) controllers. For gain scheduling, linear interpolation of parameters of the local PI controllers is used. Next, simulations are performed in order to show performances of the presented control algorithm.

Słowa kluczowe

EN

ramjetH∞ control; proportional-integral control; gain scheduling

• Wydawca: Polskie Towarzystwo Mechaniki Teoretycznej i Stosowanej
• Czasopismo: Journal of Theoretical and Applied Mechanics
• Rocznik: 2020
• Tom: Vol. 58 nr 4
• Strony: 997--1007
• Opis fizyczny: Bibliogr. 7 poz., rys., tab.

Twórcy

autor

Zorić Nemanja Dušan

• University of Belgrade, Faculty of Mechanical Engineering, Serbia

autor

Radulović Radoslav Danilo

• University of Belgrade, Faculty of Mechanical Engineering, Serbia

autor

Jazarević Vladimir Miloš

• Must Solutions, Belgrade, Serbia

autor

Petrović Trajko Borivoje

• University of Belgrade, Faculty of Electrical Engineering, Serbia

Bibliografia

• 1. Chandra K.P.B, Gupta N.K., Ananthkrishnan N., Park I.S., Yoon H.G., 2010,Modeling, simulation, and controller design for an air-breathing combustion system, Journal of Propulsion and Power, 26, 3, 562-574.
• 2. Chandra K.P.B, Gupta N.K., Ananthkrishnan N., Renganathan V.S., 2009, Modeling, dynamic simulation and controller design for an air-breathing combustion system, 47th AIAA Aerospace Science Meeting and The New Horizons Forum and Aerospace Exhibit, Orlando, Florida.
• 3. Gupta N.K., Gupta B.K., Ananthkrishnan N., Shevare G.R., Park I.S., Yoon H.G., 2007, Integrated modeling and simulation of an air-breathing combustion system dynamics, AIAA Paper 2007-6374, AIAA Modeling and Simulation Technologies Conference and Exhibit, Hilton Head, South Carolina.
• 4. Skogestad S., Postlethwaite I., 2001, Multivariable Feedback Control: Analysis and Design, 2nd Edition, John Wiley & Sons.
• 5. Turns S.R., 2000, An Introduction to Combustion: Concepts and Applications, 2nd Edition, McGraw-Hill Education.
• 6. Zamani M., Sadati N., Ghartemani M.K., 2009, Design of an H∞ PID controller using particle swarm optimization, International Journal of Control, Automation, and Systems, 7, 2, 273-80.
• 7. Zhou K., 1997, Essentials of Robust Control, 1st Edition, Pearson.

Uwagi

Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).