Multivariable Robust Control for a Type of Missiles
一类飞行器的多变量鲁棒控制

In this paper the mathematical model of a type of missiles has been obtained and analyzed, then a multivariable robust control system of the missile is designed by means of intelligent approach to non-minimum phase control system design.Simulation of the control system based on the genuine model showed the effectiveness of the approach. The described design approach can serve as a means for aeronautical and astronautical control engineering.