• 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