Mixed LQR/H∞ non-fragile control with regional pole placement for flight kinematics system

Author

Huang, Yiqing ; Sun, Changyin ; Wang, Li ; Xia, Jianwei

Author_Institution

Sch. of Autom., Southeast Univ., Nanjing, China

fYear

2011

fDate

23-25 May 2011

Firstpage

1410

Lastpage

1414

Abstract

A kind of mixed LQR/ H∞ non-fragile controller with regional pole placement is designed for interval system model of flight kinematics system in this paper. H∞ performance, regional pole placement and robust guaranteed cost control of linear time invariant system are considered in this method and the existed conditions of the controller are deduction by linear matrix inequality (LMI) approach. Also, we consider the gain variation of controller due to parametric uncertainties and modeling errors which exist in fight kinematics system. Finally, simulation comparisons between non-fragile controller and traditional robust controller that without considering the gain variation of controller show the advantages and effectiveness of our approach.

Keywords

H^∞ control; aerospace control; control system synthesis; gain control; linear matrix inequalities; linear quadratic control; linear systems; pole assignment; robust control; H∞ performance; LMI approach; controller gain variation; flight kinematics system; interval system model; linear matrix inequality; linear time invariant system; mixed LQR/H∞ non-fragile control; modeling errors; nonfragile controller; parametric uncertainty; regional pole placement; robust controller; robust guaranteed cost control; simulation comparisons; Aerospace control; Atmospheric modeling; Control systems; Kinematics; Performance analysis; Robustness; Uncertainty; Flight kinematics system; Guaranteed cost control; H∞ control; Regional pole placement;

fLanguage

English

Publisher

ieee

Conference_Titel

Control and Decision Conference (CCDC), 2011 Chinese

Conference_Location

Mianyang

Print_ISBN

978-1-4244-8737-0

Type

conf

DOI

10.1109/CCDC.2011.5968412

Filename

5968412