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http://dx.doi.org/10.12673/jant.2011.15.6.1187

Practical Civil UAV Engine Control using High-gain Observer  

Jung, Byeong-In (Department of Avionics Engineering, HanSeo University)
Ahn, Dong-Man (Department of Avionics Engineering, HanSeo University)
Hong, Gyo-Young (Department of Avionics Engineering, HanSeo University)
Hong, Seung-Beom (Department of Avionics Engineering, HanSeo University)
Min-Seok, Jie (Department of Avionics Engineering, HanSeo University)
Publication Information
Journal of Advanced Navigation Technology / v.15, no.6, 2011 , pp. 1187-1193 More about this Journal
Abstract
In this paper, proposed controller preventing compressor surge and reducing the acceleration time of the fuel flow control system for turbo-jet engine. Turbo-jet engine controller is designed by applying fuzzy PID control algorithm and high-gain observer. Observer is used to estimate to compressor rotation speed of turbo-jet engine. Result of fuzzy inference is used as the fuel flow control inputs for preventing compressor surge and flame-out in turbo-jet engine. The controller is designed to converge to the desired speed quickly and safely. Using MATLAB to perform computer simulations verified the performance of the proposed controller.
Keywords
turbojet engine control; high-gain observer; fuzzy PID controller; fuel flow control; surge control;
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