DocumentCode
582336
Title
Robustification of backstepping design technique: A jet engine compressor model example
Author
Li, Wang ; Chang-yin, Sun ; Yi-qing, Huang
Author_Institution
Sch. of Autom., Southeast Univ., Nanjing, China
fYear
2012
fDate
25-27 July 2012
Firstpage
4556
Lastpage
4561
Abstract
Backstepping technique is one of the most poplar frameworks for designing controllers for nonlinear systems. Robustification of backstepping design is proposed because of the flexibilities presented in backstepping design, which include choosing various Lyapunov functions which are not limited in quadratic form, making the time derivative of Lyapunov function negative in different forms and some modifications in virtual controls, some of them have the possibility to avoid cancellation of useful nonlinearities. Several results about robustification of backstepping design was presented in strict feedback and less strict feedback nonlinear system, and these are demonstrated and compared with the conventional backstepping via the Moore-Greitzer model of a jet engine compressor system.
Keywords
Lyapunov methods; compressors; control system synthesis; jet engines; nonlinear control systems; stability; Lyapunov functions; backstepping design technique; controller design; jet engine compressor model example; less strict feedback nonlinear system; robustification; virtual controls; Backstepping; Educational institutions; Equations; Jet engines; Lyapunov methods; Nonlinear systems; Robustness; Backstepping technique; Lyapunov function; robustification; virtual control;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2012 31st Chinese
Conference_Location
Hefei
ISSN
1934-1768
Print_ISBN
978-1-4673-2581-3
Type
conf
Filename
6390727
Link To Document