Authors:
Yongyan Ge
;
Hongsen Yan
and
Lingchen Xia
Affiliation:
School of Automation, Southeast University, China
Keyword(s):
Missile control, Multi-dimensional Taylor network (MTN) controller, Attitude control, Optimal control
Abstract:
In this paper, we present the design of the multi-dimensional Taylor network (MTN) optimal controller in the flight control of cruise missile. The MTN optimal control, which combines the classical architecture of feedback control system and the new controller structure, it is not only suitable for the analysis of the stability of the closed-loop system, but also for the control of nonlinear systems with mechanism known or unknown models. Firstly, this paper will briefly introduce the theoretical basis of the MTN optimal control. Secondly, the characteristics of the missile mathematical model and the theory of missile control will be explained, accompanied with the design of controller. Finally, the feasibility of the method is validated through numerical simulation of the PID controller, PIDNN controller and the MTN optimal controller. The results show that the MTN optimal controller has the best control effect of them.