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

fYear

2014

fDate

14-17 Dec. 2014

Firstpage

1

Lastpage

7

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;

fLanguage

English

Publisher

ieee

Conference_Titel

Computational Intelligence for Security and Defense Applications (CISDA), 2014 Seventh IEEE Symposium on

Conference_Location

Hanoi

Type

conf

DOI

10.1109/CISDA.2014.7035629

Filename

7035629