Bumpless switching scheme design for continuous-time controller switched systems

Author

Qi Yiwen ; Bao Wen

Author_Institution

Hypersonic Technol. Res. Center, Harbin Inst. of Technol., Harbin, China

fYear

2011

fDate

22-24 July 2011

Firstpage

1702

Lastpage

1706

Abstract

The paper deals with a switching performance optimal control for continuous-time controller switched systems. Steady-state bumpless switching is considered. An linear matrix inequality (LMI) based static bumpless switching compensator design is given via internal model principle, guaranteed cost and regional pole placement technique. The corresponding bumpless switching scheme is also presented. The proposed scheme is simple in structure, and easy to be implemented. Simulations for the generic hypersonic vehicle model show the effectiveness of the proposed method.

Keywords

aircraft; compensation; continuous time systems; control system synthesis; linear matrix inequalities; optimal control; pole assignment; LMI based static bumpless switching compensator design; continuous time controller switched system; hypersonic vehicle model; internal model principle; linear matrix inequality; regional pole placement technique; steady-state bumpless switching scheme design; switching performance optimal control; Switches; Controller switched systems; Disk pole constraints; LMI; Steady-state bumpless switching;

fLanguage

English

Publisher

ieee

Conference_Titel

Control Conference (CCC), 2011 30th Chinese

Conference_Location

Yantai

ISSN

1934-1768

Print_ISBN

978-1-4577-0677-6

Electronic_ISBN

1934-1768

Type

conf

Filename

6000495