Title :
Design of Takagi-Sugeno fuzzy controller for automatic stabilization system of missiles with blended aerodynamic and lateral impulsive reaction-jet
Author :
Cao Huu Tinh ; Vu Hoa Tien ; Nguyen Cong Dinh ; Mai Ngoc Anh
Author_Institution :
Le Quy Don Tech. Univ., Hanoi, Vietnam
Abstract :
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.
Keywords :
aerodynamics; control system synthesis; fuzzy control; missile control; stability; Takagi-Sugeno fuzzy controller design; Takagi-Sugeno fuzzy system; automatic stabilization system; blended aerodynamic; blended control system; lateral impulsive reaction-jet; missile stabilization; missiles; parallel control systems; performance improvement; Aerodynamics; Computational modeling; Control systems; Mathematical model; Missiles; Nonlinear systems; Takagi-Sugeno model; Takagi-Sugeno fuzzy controller; aerodynamic fin; automatic stabilization system; blended aero-fin and reaction-jet control; lateral impulsive reaction-jet;
Conference_Titel :
Computational Intelligence for Security and Defense Applications (CISDA), 2014 Seventh IEEE Symposium on
Conference_Location :
Hanoi
DOI :
10.1109/CISDA.2014.7035629
