turbojet engineunmanned aircraftfuel flow controlThis paper proposes a turbojet engine controller for unmanned aircraft using Fuzzy-PI(Proportional Integral) algorithm. To prevent surge or flame out which could occur during engine acceleration or de...
Simulation-based dynamic model and speed controller design of a small-scale turbojet engine Purpose This paper aims to present a nonlinear mathematical model of a small-scale turbojet aeroengine and also a speed controller design that is conducted... I Yazar,E Kiyak,F Caliskan,... - 《Aircra...
Machine learning application to forecasting performance and thermodynamics parameters of small turbojet engine The common use of micro-turbojet engines to meet various needs of the modern world makes these more popular day by day; hence, some scientists have devoted... Suat Toraman,Hakan Aygun,Ome...
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kwlee@mail.hangkong.ac.kr Abstract. This paper proposes a turbojet engine controller for unmanned aircraft using Fuzzy-PI(Proportional Integral) algorithm. To prevent surge or flame out which could occur during engine acceleration or deceleration operation, the PI type fuzzy system controls the fuel...
For this purpose, different union and intersection fuzzy norms are used in control strategy instead of using minimum and maximum functions to investigate the impact of this idea in gas turbine engines controller design and optimization. A turbojet engine with an industrial Min–Max control strategy ...
For this purpose, different union and intersection fuzzy norms are used in control strategy instead of using minimum and maximum functions to investigate the impact of this idea in gas turbine engines controller design and optimization. A turbojet engine with an industrial Min–Max control strategy ...
Engine modellingEngine controlANFISThis contribution presents a proposal and practical implementation of a digitally controlled fuel system for control of fuel supply into a small turbojet engine, iSTJ-21V. In the past, for the purposes of fuel metering to the engine MPM-20, which was a ...
CONSTITUTION: A jet nozzle 1 mounted to a downstream end of a gas injection pipe 2 comprises an inner structure 4 and an outer structure 3 having substantially rectangular cross section. The inner structure 4 has partition walls comprising two vertical fixed panels 9, 10 and two parallel ...
Electronic controller i.e. full authority digital engine controller, for e.g. turbojet engine of aircraft, has module insulated thermically such that module remains operational until disconnection of electrical supply of controller by fuseThe controller (1) has an electronic protection module (5A) ...