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
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;
Conference_Titel :
Control and Decision Conference (CCDC), 2013 25th Chinese
Conference_Location :
Guiyang
Print_ISBN :
978-1-4673-5533-9
DOI :
10.1109/CCDC.2013.6561554