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YAZAR I., Yasa T., KIYAK E.
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, vol.89, no.2, pp.203-210, 2017 (SCI-Expanded)
Article / Article
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
Science Citation Index Expanded (SCI-EXPANDED), Scopus
ANFIS, Compressor performance prediction, Nonlinear mathematical model, Turboprop engine, GAS-TURBINE ENGINE, GENETIC ALGORITHMS, MAP GENERATION, PERFORMANCE, PREDICTION, COMPRESSOR, ANFIS
Anadolu University Affiliated:
Purpose - An aircraft engine control system consists of a large scale of control parameters and variables because of the complex structure of aero-engine. Monitoring and adjusting control variables and parameters such as detecting, isolating and reconfiguring the system faults/failures depend on the controller design. Developing a robust controller is based on an accurate mathematical model.