Design for Attitude Control Method of Combined Control Interceptor

Author

Yin, Yong-xin ; Yang, Ming ; Wang, Zi-cai

Author_Institution

Control & Simulation Center, Harbin Inst. of Technol.

fYear

2006

fDate

13-16 Aug. 2006

Firstpage

523

Lastpage

527

Abstract

An attitude fuzzy control method is presented for the interceptor in aerosphere. The force and moment received by interceptor are given and mathematical equations of attitude are constructed. In order to adjust the attitude movement of combined control interceptor, a fuzzy control method is designed, and the detailed control rule and gradation of attitude control are presented. This control method chooses the error of attitude angle and change of this error as the inputs, and chooses the control force as output. The simulation results show that this method can avoid employ frequently lateral thrust, implements efficiently the attitude redressal of the combined control interceptor, and has satisfactory control precision

Keywords

aircraft control; attitude control; control system synthesis; fuzzy control; aerosphere; attitude fuzzy control method; combined control interceptor; lateral thrust; mathematical equation; Aerodynamics; Attitude control; Cybernetics; Design methodology; Equations; Error correction; Force control; Fuzzy control; Machine learning; Motion control; Attitude control; Combined control; Fuzzy control; Lateral thrust;

fLanguage

English

Publisher

ieee

Conference_Titel

Machine Learning and Cybernetics, 2006 International Conference on

Conference_Location

Dalian, China

Print_ISBN

1-4244-0061-9

Type

conf

DOI

10.1109/ICMLC.2006.258328

Filename

4028120