A H∞/mixed sensitivity based dynamic inversion algorithmfor BTT missile system

Author

Feng Tian-yu ; Hu Qiong ; Xu ling ; Shao Li-yong

Author_Institution

Sch. of Mechatronical Eng., Beijing Inst. of Technol., Beijing, China

fYear

2013

fDate

20-22 Dec. 2013

Firstpage

2720

Lastpage

2724

Abstract

As for the strong coupling, time-varying and nonlinear characteristics of Bank-to-turn missile system, a control which involves dynamic inversion algorithm, linear quadratic regulator (LQR) and H∞/mixed sensitivity algorithm was proposed. The dynamic inversion algorithm was applied to translate the nonlinear mathematical model of missile system into a pseudo-linear one. Linear quadratic regulator (LQR) realized optimal control through state feedback. H∞/ mixed sensitivity algorithm tackled the possible uncertainty in the mathematical model. Simulation of the closed loop control system was implemented via Matlab / Simulink software, from which the results showed that this control strategy could obtain desirable performance.

Keywords

H^∞ control; closed loop systems; digital simulation; linear systems; missile control; nonlinear control systems; sensitivity analysis; state feedback; time-varying systems; BTT missile system nonlinear characteristics; BTT missile system time-varying characteristics; H∞ sensitivity based dynamic inversion algorithm; Matlab; Simulink software; bank-to-turn missile system; closed loop control system; linear quadratic regulator; mixed sensitivity based dynamic inversion algorithm; nonlinear mathematical model; optimal control; pseudolinear mathematical model; state feedback; Equations; MATLAB; Mathematical model; Robustness; Sensitivity; Bank-to-turn(BTT); Dynamic inversion algorithm; H∞/Mixed sensitivity; Liner Quadratic Regulator; Matlab/Simulink Simulation;

fLanguage

English

Publisher

ieee

Conference_Titel

Mechatronic Sciences, Electric Engineering and Computer (MEC), Proceedings 2013 International Conference on

Conference_Location

Shengyang

Print_ISBN

978-1-4799-2564-3

Type

conf

DOI

10.1109/MEC.2013.6885489

Filename

6885489