Design of Takagi-Sugeno fuzzy controller for automatic stabilization system of missiles with blended aerodynamic and lateral impulsive reaction-jet

In this paper, the design of a fuzzy-based controller for automatically stabilizing missiles with blended control system of aerodynamic and lateral impulsive reaction-jet is presented. The controller uses a Takagi-Sugeno fuzzy system that allows the parallel control systems to operate together at a moment to improve performance of the system and minimize energy usage of lateral impulsive reaction-jet. The designed system is objectively tested through simulation experiments on the computer.