DocumentCode
620325
Title
A novel nonlinear model predictive control method based on LMI and feedback linearization
Author
Rui Pang ; Zhongke Shi
Author_Institution
Sch. of Autom., Northwestern Polytech. Univ., Xi´an, China
fYear
2013
fDate
25-27 May 2013
Firstpage
3503
Lastpage
3508
Abstract
Nonlinear model predictive control (NMPC) mainly deals with complex dynamic systems with different kinds of nonlinearities, which is much more difficult to solve than normal linear model predictive. The non-convex optimization method inside MPC is its main challenging problem. A LMI based NMPC method is proposed combined with nonlinear feedback linearization can efficiently convert complex non-convex optimization problem to convex. The method minimizes the upper bound of cost function instead of itself, which can stabilize the whole system and achieve the control performance. A high angle of attack (HAOA) aircraft controller design example is illustrated in the end to demonstrate the validity of proposed method.
Keywords
aircraft control; control nonlinearities; control system synthesis; convex programming; feedback; large-scale systems; linear matrix inequalities; linearisation techniques; nonlinear control systems; predictive control; HAOA aircraft controller design; LMI based NMPC method; complex dynamic systems; convex optimization; cost function; high angle of attack aircraft controller design; nonlinear feedback linearization; nonlinear model predictive control method; nonlinearities; Aerospace control; Aircraft; Asymptotic stability; Cost function; Predictive control; Predictive models; LMI; NMPC; convex optimization; feedback linearization;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2013 25th Chinese
Conference_Location
Guiyang
Print_ISBN
978-1-4673-5533-9
Type
conf
DOI
10.1109/CCDC.2013.6561554
Filename
6561554
Link To Document