• DocumentCode
    3608478
  • Title

    Smooth switching linear parameter-varying control for hypersonic vehicles via a parameter set automatic partition method

  • Author

    Weilai Jiang ; Chaoyang Dong ; Qing Wang

  • Author_Institution
    Sch. of Aeronaut. Sci. & Eng., Beihang Univ., Beijing, China
  • Volume
    9
  • Issue
    16
  • fYear
    2015
  • Firstpage
    2377
  • Lastpage
    2386
  • Abstract
    This study presents a systematic approach to design smooth switching linear parameter-varying (LPV) controllers for hypersonic vehicles (HVs). Considering the switched LPV model of HVs, the smooth switching controllers are designed by means of dividing the scheduling parameter set into subsets with overlaps and the controllers in the overlapped subsets are smoothly scheduled between controllers in adjacent subsets. A switching law without constraint on average dwell time is obtained which makes the conclusion less conservative. To divide the parameter set automatically, a novel set partition method, in which the selecting of datum vertex and the handling of unpartitioned subset are innovative, is proposed. The switching LPV controllers that achieve a desired performance are constructed efficiently by solving a convex optimisation problem. Simulation results for HVs demonstrate the effectiveness of the proposed smooth switching LPV controllers and parameter set division method.
  • Keywords
    aerospace control; aircraft; convex programming; linear systems; set theory; time-varying systems; HV; LPV controllers; adjacent subsets; convex optimisation problem; datum vertex; hypersonic vehicles; parameter set automatic partition method; parameter set division method; scheduling parameter; set partition method; smooth switching linear parameter varying control; switching law;
  • fLanguage
    English
  • Journal_Title
    Control Theory Applications, IET
  • Publisher
    iet
  • ISSN
    1751-8644
  • Type

    jour

  • DOI
    10.1049/iet-cta.2015.0178
  • Filename
    7299710