• DocumentCode
    162389
  • Title

    Influence of complexity relaxation and convex hull manipulation on LMI based control design

  • Author

    Szollosi, Alexandra ; Baranyi, Peter

  • Author_Institution
    3D Internet-Based Control & Commun. Lab., Comput. & Autom. Res. Inst., Budapest, Hungary
  • fYear
    2014
  • fDate
    15-17 May 2014
  • Firstpage
    145
  • Lastpage
    151
  • Abstract
    The paper investigates how the complexity and the convex hull determined by the vertexes of the TP model representation of a given quasi Linear Parameter Varying state-space model influence the stable parameter region achievable via Linear Matrix Inequality based control design. The paper applies the Relaxed TP model transformation based Control Design Framework that supports both the complexity-accuracy trade-off of the TP model representation and convex hull manipulation separately executable on all components of the control system to be derived. Some specialization and further relaxation of the framework is also proposed here for frequent cases when all components of the system is handled in TP model form. The framework is also extended with a TP model interpolation technique to perform a systematic convex hull manipulation. The overall investigation is done on the complex NATA model of the three degree of freedom aeroelastic wing section model including Stribeck friction. The paper concludes and via the example proofs that both the complexity and the convex hull strongly influences the feasibility of the design. Further the paper proofs that the separate convex hull manipulation of the given model done for controller and the observer design also has to be taken into consideration.
  • Keywords
    convex programming; interpolation; linear matrix inequalities; observers; state-space methods; LMI based control design; Stribeck friction; TP model interpolation technique; TP model representation; complex NATA model; complexity relaxation; complexity-accuracy trade-off; control design framework; control system; degree of freedom aeroelastic wing section model; linear matrix inequality based control design; observer design; quasi linear parameter varying state-space model; relaxed TP model transformation; stable parameter region; systematic convex hull manipulation; Computational modeling; Iron;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Applied Computational Intelligence and Informatics (SACI), 2014 IEEE 9th International Symposium on
  • Conference_Location
    Timisoara
  • Type

    conf

  • DOI
    10.1109/SACI.2014.6840094
  • Filename
    6840094