A novel control system design method for missile with lateral jet and aerodynamic surfaces

Author

Zhen Shi ; Wenqiao Ma ; Yufang Zhang

Author_Institution

Coll. of Autom., Harbin Eng. Univ., Harbin, China

fYear

2013

fDate

9-11 June 2013

Firstpage

858

Lastpage

861

Abstract

Aiming at the characters of large jet interaction for missile with lateral jets and aerodynamic surfaces, a new control system design method based on adaptive genetic algorithm and improved fuzzy control theory is proposed, which don´t relay on accurate mathematical model. Firstly, adaptive genetic algorithm is used to design compound control allocation algorithm. Secondly, ignition algorithm of attitude control engines is designed based on variable universe adaptive fuzzy control theory. Finally, considering the discrete character of attitude control engines, Pulse-Width PulseFrequency (PWPF) method is used for application. Simulation results show the effectiveness of method.

Keywords

adaptive control; aerodynamics; attitude control; control system synthesis; fuzzy control; genetic algorithms; jets; missile control; PWPF method; adaptive genetic algorithm; aerodynamic surface; attitude control engine; compound control allocation algorithm; control system design method; fuzzy control theory; ignition algorithm; jet interaction; lateral jet; missile; pulse-width pulse-frequency method; variable universe adaptive fuzzy control theory; Aerodynamics; Algorithm design and analysis; Attitude control; Engines; Fuzzy control; Missiles; Resource management; fuzzy control; genetic algorithm; ignition algorithm; lateral jets;

fLanguage

English

Publisher

ieee

Conference_Titel

Intelligent Control and Information Processing (ICICIP), 2013 Fourth International Conference on

Conference_Location

Beijing

Print_ISBN

978-1-4673-6248-1

Type

conf

DOI

10.1109/ICICIP.2013.6568192

Filename

6568192