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http://dx.doi.org/10.5139/JKSAS.2012.40.5.431

Non-linear Control of Turbojet Engine for High Maneuverability UAV  

Han, Dong-Ju (극동대학교 항공정비학과)
Oh, Seong-Hwan (국방과학연구소 제7기술연구본부)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.40, no.5, 2012 , pp. 431-438 More about this Journal
Abstract
Non-linear turbojet engine controller with high operational performance has been designed for the high maneuverability UAV. The turbojet engine dynamic performance code has been developed to reflect the non-linear characteristics on controller design, by which the necessity of non-linear controller design was justified by investigating the limitation of linear model derived from the dynamic performance. The PI-like fuzzy controller was designed and enhanced by combining with conventional derivative control. This designed fuzzy controller proves its effectiveness by showing superior control performances over the conventional PID controller along with guaranteeing the safe operation within compressor surge, flame out and turbine temperature limits etc.
Keywords
Turbojet Engine; Dynamic Performance Analysis; Non-linear Control; Fuzzy Logic Control;
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1 Song, Q., Wilkie, J., Grimble, M. J., "Robust Controller for Gas Turbines based upon LQG/LTR Design with Self-Tuning Features", J. of Dynamic Systems, Measurement and Control,' Vol. 115, Sept., 1993, pp. 569-591.   DOI   ScienceOn
2 김석균, 기자영, 공창덕, "소형항공기용 터보제트엔진의 동적모사와 성능제어에 관한 연구", 한국항공우주학회지 추계학술발표회, 1996, pp. 285-290.
3 남세규, 한동주, 김병교, "제트엔진의 예견퍼지슬라이딩 제어에 관한 연구", 한국 자동제어학술회의, 1993, pp. 1068-1071.
4 Geyser, L. C., "DYABCD A Program for Calculating Linear A,B,C,D Matrices from a Nonlinear Dynamic Engine Simulation", NASA TP-1295, 1978.
5 Sellers, J. F., Daniele, C. J., "DYGEN A Program for Calculating Steady-State and Transient Performance of Turbojet and Turbofan Engines", NASA TN D-7901, April 1975.
6 Hafedh, A., Mohamed, C., Ahmed, A., "Robust Fuzzy Sliding Mode Controller for Discrete Nonlinear Systems", Int. J. of Computers, Communication & Control,' Vol. 3, No. 1, 2008, pp. 6-20.   DOI
7 Brent, J., Robert, R., Allan, J., "Nonlinear Model Predictive Control of an Aircraft Gas Turbine Engine", Proc. of 41th IEEE Coference on Decision and Control, 2002, pp. 4649-4651.
8 Lagrat, I., Ouakka, H., Boumhidi, I., "Fuzzy Sliding Mode PI Controller for Nonlinear Systems", Proc. of 6th Int. Coference on Simulation, Modelling and Optimization, 2006, pp. 534-539.
9 Romulus L., Alexandru N., Liviu D., "Double-Spool Single Jet Engine for Aircraft as Controlled Object", Int. J. of Math. Models and Methods in Applied Science Vol. 2, Issue 4, 2008, pp. 553-562.
10 Montazeri-Gh, M., Nasiri M., "Actuator-based hardware-in-the-loop testing of a jet engine fuel control unit in flight conditions", Simulation Modelling Practice and Theory, Vol. 21, Issue 1, 2012, pp. 65-77.   DOI   ScienceOn
11 신의석 외 6인, "터보 제트엔진에 대한 퍼지추론 제어시스템", 한국항공우주학회지, 제26권, 제4호, 1998, pp. 138-145.
12 한동주, "터보제트엔진의 퍼지제어기 설계 및 다목적함수 만족기법을 통한 제어성능 향상에 관한 연구", 한국항공우주학회지, 제31권, 제6호, 2003, pp. 61-71.
13 Rudolf, A., "Digital Electronic Control of a Small Turbojet Engine MPM 20", Acta Polytechnica Hungarica, Vol. 4, No. 4, 2007, pp. 83-95.
14 Sanjay Garg, "Turbofan Engine Control System Design Using LQG/LTR Methodology", NASA-CR-182303, June, 1989.