Amirreza kosari - Corresponding Author Assistant Professor of Aerospace Engineering, Faculty of New Sciences and Technologies, University of Tehran
Hosein Maghsoudi - Ph.D. student of Aerospace Engineering, Faculty of New Sciences and Technologies, University of Tehran
Puya Gorji - M.S. student of Aerospace Engineering, Faculty of New Sciences and Technologies, University of Tehran

In this paper, a new method to optimal control law development based on the predictive optimal control algorithm for a non-minimum phase flying system is presented. The rules for guiding the optimum line of sight for ideal control model of first, second and third order of a non-minimum phase system model has been extracted. At first, some of the features of non-minimum phase systems have been mentioned, then a simple model of the system is offered. Optimization algorithm of the model predictive control has been described and the results of model predictive control design simulation of a non-minimum phase system is provided. The results indicates performance enhancement of the proposed controller

Optimal control law, predictive model control, third order non-minimum phase system