Study of Reduced-order and Non-linear Local Optimal Control Application to Aero Gas Turbines
نویسندگان
چکیده
In this work second order linear model, reduced order (first order) linear model and second order nonlinear model of a gas turbine engine have been obtained from the engine input-output data using evolutionary optimization technique. These three models have then been used in local optimal control design. The obtained controllers have been applied to the second order non-linear engine model and their performance has been compared.
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