DocumentCode
2241799
Title
The first stage studies of U-state space control system design
Author
Xin, Liu ; Quanmin, Zhu ; Pritesh, Narayan ; Ye, Yang
Author_Institution
Department of Engineering Design and Mathematics, University of the West of England, Frenchay Campus, Coldharbour Lane, Bristol, BS16 1QY, UK
fYear
2015
fDate
28-30 July 2015
Firstpage
946
Lastpage
951
Abstract
In this study, a basic idea of U-state feedback control system design method is proposed based on U-model principle. Compared with U-model based nonlinear polynomial systems, the U-state space design is to determine the desired state variable equation xd (t), therefore to find the controller output u(t−1). The desired state equation can be designed/specified and transformed into the U-state space expression easily. The controller output can be obtained from resolving the equation. The desired state variables are updated by the corresponding state variables x(t). Assume that the state variables are measurable or obtained by a proper observer in this study. In case studies, two nonlinear discrete time state space models are selected to test the proposed approach. Computational experiments, that is, simulation studies, are used to demonstrate the procedure effectiveness.
Keywords
Aerospace electronics; Algorithm design and analysis; Control systems; Mathematical model; Observers; Polynomials; System analysis and design; U-control approach; U-model framework; U-state space framework; feedback linearization;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2015 34th Chinese
Conference_Location
Hangzhou, China
Type
conf
DOI
10.1109/ChiCC.2015.7259761
Filename
7259761
Link To Document