عنوان مقاله English
Jet engine Fuel Control Unit (FCU) has been manufactured recently in the SSAC laboratory of Iran University of science and technology, and is being tested now using HIL testing. Regarding there is no possibility utilizing a jet engine in this test set; an induction motor was used as an actuator to transit rotation acquired using jet engine real time simulation to the FCU pump. In this paper, the induction motor’s velocity control is presented considering condition for the test set. To do so, system identification method is used to model the components employed in induction motor velocity control system. Then, the model is evaluated using experimental test results. Afterward, it is used to design ANFIS controller, and the controller parameters is adjusted employing IWO optimization algorithm as a strong tool for seeking in vast disorder spaces. Subsequently, the controller designed is implemented on a real system. Results gained using simulation and the designed controller implementation show that ANFIS controller designed using IWO algorithm works appropriately.
کلیدواژهها English
