Missile control systems design based on model tracking GSVSC theory

Author

Dong Feiyao ; Lei Humin ; Yang Zhifeng ; Li Jiong

Author_Institution

Missile Inst., Air Force Eng. Univ., Xi´an, China

fYear

2011

fDate

22-24 July 2011

Firstpage

2622

Lastpage

2625

Abstract

Considering the over-load tracking problem of the pitch channel control system for STT missile, a new control algorithm is proposed based on model tracking global sliding mode variable structure control (GSVSC) theory. Combining the mathematical model of STT missile pitch plane, its tracking error model is presented together with the criteria for model complete tracking. According to the dynamic and stability index, the sliding mode parameter matrix and the global sliding mode factor are designed respectively. Lastly, the stability of the algorithm is analyzed. Simulation results show that the proposed approach has good dynamic properties and strong robustness.

Keywords

control system synthesis; matrix algebra; missile control; stability; tracking; variable structure systems; STT missile pitch plane; algorithm stability; dynamic index; global sliding mode factor; mathematical model; missile control system design; model tracking GSVSC theory; model tracking global sliding mode variable structure control theory; overload tracking problem; pitch channel control system; sliding mode parameter matrix; stability index; tracking error model; Algorithm design and analysis; Atmospheric modeling; Control systems; Mathematical model; Missiles; Stability criteria; GSVSC; Global Sliding Mode Factor; Model Tracking; Robustness;

fLanguage

English

Publisher

ieee

Conference_Titel

Control Conference (CCC), 2011 30th Chinese

Conference_Location

Yantai

ISSN

1934-1768

Print_ISBN

978-1-4577-0677-6

Electronic_ISBN

1934-1768

Type

conf

Filename

6001209