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http://dx.doi.org/10.12673/jkoni.2013.17.01.107

Design of PID Type Fuzzy Logic Acceleration Controller for Turbojet Engine Using High-gain Observer  

Jie, Min-Seok (School of Avionics, HanSeo University)
Kim, Dae-Gi (School of Avionics, HanSeo University)
Hong, Gyo-Young (School of Avionics, HanSeo University)
Ahn, Dong-Man (School of Avionics, HanSeo University)
Hong, Seung-Beom (School of Avionics, HanSeo University)
Publication Information
Journal of Advanced Navigation Technology / v.17, no.1, 2013 , pp. 107-114 More about this Journal
Abstract
In this paper, we propose controller to control the acceleration of unmanned aircraft turbojet engine. The high-gain observer to estimate the rotational speed of compressor is used, and the turbojet engine controller applying fuzzy heuristic techniques and PID control algorithm are designed. fuzzy PID controller produces the flow control input to prevent the surge and flame-out phenomena at the acceleration and deceleration of the turbojet engine. The standard acceleration is set and the fuel flow control is defined by the fuzzy heuristic. Computer simulations are performed using MATLAB in order to verify the performance of the proposed controller.
Keywords
Turbojet engine; High-gain observer; Fuzzy PID controller; Surge control;
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