Adjustable lateral thrust and aerodynamics blended control system design based on auto disturbance rejection controller

Author

Zhao Yuyu ; Yang Baoqing ; Li Xinglong

Author_Institution

Harbin Inst. of Technol., Harbin, China

fYear

2013

Firstpage

5041

Lastpage

5045

Abstract

This paper presents a control method for adjustable lateral thrust and aerodynamics blended control system based on auto disturbance rejection controller (ADRC). Firstly, the lateral thrust and aerodynamics blended control system model is established. Secondly, the blended control scheme is provided based on overload command distribution, and the aerodynamic control law based on ADRC is designed. In addition, the extended state observer is designed to estimate the target maneuver. Finally, the feasibility of the control method is verified by the simulation results.

Keywords

aerodynamics; control system synthesis; mechanical variables control; missile control; observers; ADRC; adjustable lateral thrust control system design; aerodynamic control law; aerodynamics blended control system design; auto disturbance rejection controller; control method; extended state observer; intercept missiles; overload command distribution; target maneuver estimation; Aerodynamics; Angular velocity; Control systems; Mathematical model; Missiles; Observers; adjustable lateral thrust; auto disturbance rejection controller; blended control system;

fLanguage

English

Publisher

ieee

Conference_Titel

Control Conference (CCC), 2013 32nd Chinese

Conference_Location

Xi´an

Type

conf

Filename

6640315