Design of Autopilot for Aerodynamic/Reaction-Jet Multiple Control Missile

Author

Sui, Qi SHeng ; Li, Xin ; Fan, Yong Hua

Author_Institution

Coll. of Astronaut., Northwestern Polytech. Univ., Xi´´an

Volume

1

fYear

2008

fDate

20-22 Oct. 2008

Firstpage

337

Lastpage

340

Abstract

A new scheme of reaction-jet/aerodynamic multi-control missile using pose controlled pulse-engine is present. In this scheme, aerodynamic is used as feedback control, and reaction-jet is feed-forward control. In the first part, the model of the multi-control system is given; then, the aerodynamic controller is designed by using pole assignment, and the reaction-jet controller has been designed by using the term of entirely compensated. Finally it has been proved by simulation that this multiple controller can greatly enhance response speed and the scheme is feasible.

Keywords

aerodynamics; control system synthesis; feedback; feedforward; jet engines; missile control; pole assignment; aerodynamic multicontrol missile; autopilot; feed-forward control; feedback control; pole assignment; pose controlled pulse-engine; reaction-jet multiple control missile; Aerodynamics; Automatic control; Control systems; Educational institutions; Engines; Equations; Feedback control; Feedback loop; Feedforward systems; Missiles;

fLanguage

English

Publisher

ieee

Conference_Titel

Intelligent Computation Technology and Automation (ICICTA), 2008 International Conference on

Conference_Location

Hunan

Print_ISBN

978-0-7695-3357-5

Type

conf

DOI

10.1109/ICICTA.2008.101

Filename

4659501