Gas Turbine Engine Control Design Using Fuzzy Logic and Neural Networks
This paper presents a successful approach in designing a Fuzzy Logic Controller (FLC) for a specific Jet Engine. At first, a suitable mathematical model for the jet engine is presented by the aid of SIMULINK. Then by applying different reasonable fuel flow functions via the engine model, some important engine-transient operation parameters (such as thrust, compressor surge margin, turbine inlet temperature, etc.) are obtained. These parameters provide a precious database, which train a neural network. At the second step, by designing and training a feedforward multilayer perceptron neural network according to this available database; a number of different reasonable fuel flow functions for various engine acceleration operations are determined. These functions are used to define the desired fuzzy fuel functions. Indeed, the neural networks are used as an effective method to define the optimum fuzzy fuel functions. At the next step, we propose a FLC by using the engine simulation model and the neural network results. The proposed control scheme is proved by computer simulation using the designed engine model. The simulation results of engine model with FLC illustrate that the proposed controller achieves the desired performance and stability.
- Record URL:
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Availability:
- Find a library where document is available. Order URL: http://worldcat.org/issn/16878086
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Authors:
- Bazazzadeh, M
- Badihi, H
- Shahriari, A
- Publication Date: 2011
Language
- English
Media Info
- Media Type: Digital/other
- Features: Figures; References; Tables;
- Pagination: 12 p
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Serial:
- Advances in Civil Engineering
- Volume: 2011
- Publisher: Hindawi Publishing Corporation
- ISSN: 1687-8086
- EISSN: 1687-8094
- Serial URL: http://www.hindawi.com/journals/ace/
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Publication flags:
Open Access (libre)
Subject/Index Terms
- TRT Terms: Aircraft; Fuel systems; Fuzzy controllers; Fuzzy logic; Jet engines; Mathematical models; Neural networks; Simulation; Turbine engines
- Subject Areas: Aviation; Vehicles and Equipment; I91: Vehicle Design and Safety;
Filing Info
- Accession Number: 01352779
- Record Type: Publication
- Files: TRIS
- Created Date: Sep 26 2011 8:38PM