Design of autopilot for Aerodynamic/Reaction-jet Multiple control missile using variable structure control

Author

Yonghua, Fan ; Xin, Li ; Jun, Yang ; Yuzhuo, Zhang

Author_Institution

Coll. of Autom., Northwestern Polytech. Univ., Xian

fYear

2008

fDate

16-18 July 2008

Firstpage

642

Lastpage

645

Abstract

A switch scheme of reaction-jet/aerodynamic multi-control missile using pose controlled pulse-engine is present. In order to increase response speed of autopilot and reducing the coupling form Reaction-jet to aerohelm, in the last stage of attacking the aerodynamic controller is disconnection and Reaction-jet controller is used only. In the first part, the model of the Reaction-jet control system is given; then, the Reaction-jet controller has been designed by using variable structure control. Finally it is proved by simulation that this multiple controller can greatly enhance response speed and has well robustness to the effect of jet interaction.

Keywords

aerodynamics; control system synthesis; missile control; multivariable control systems; position control; variable structure systems; aerodynamic controller; aerodynamic jet; autopilot design; multiple missile control; pose controlled pulse-engine; reaction-jet; reaction-jet controller; variable structure control; Aerodynamics; Automation; Control system synthesis; Control systems; Educational institutions; Engines; Equations; Missiles; Robust control; Switches; Aerodynamic/Reaction-jet Multi-controller; Pulse-Engine; Variable Structure Control;

fLanguage

English

Publisher

ieee

Conference_Titel

Control Conference, 2008. CCC 2008. 27th Chinese

Conference_Location

Kunming

Print_ISBN

978-7-900719-70-6

Electronic_ISBN

978-7-900719-70-6

Type

conf

DOI

10.1109/CHICC.2008.4604993

Filename

4604993