• DocumentCode
    164216
  • Title

    Dynamic performance improvement of linear induction motor using DTFC method and considering end-effect phenomenon

  • Author

    Shadabi, Hamed ; Sadat, Amin Rahnama ; Nabavi, Mohammad H. ; Azari, Mehran A. ; Sharifian, Mohammad B. B.

  • Author_Institution
    Fac. of Electr. & Comput. Eng., Univ. of Tabriz, Tabriz, Iran
  • fYear
    2014
  • fDate
    Sept. 28 2014-Oct. 1 2014
  • Firstpage
    1
  • Lastpage
    6
  • Abstract
    In this paper the control method of LIM which lead to optimal control characteristic of motor such as thrust, flux and current has been proposed. The performance of the proposed DTFC method has been analyzed with considering End-Effect. To evaluate and approve improved controlling characteristics, the results of the DTFC method have been compared with the results obtained from Indirect Vector Control (IVC). IVC is one of the conventional control methods for LIM. The obtained results from MATLAB/Simulink show that the DTFC control method with considering End-Effect in comparison with the IVC has caused increase response time of speed about 50%. Also it has led to a considerable reduction in FORCER thrust ripples amplitude about 25%. The most important feature of DTFC method is its performance robustness against the End-Effect phenomena.
  • Keywords
    induction motors; machine vector control; optimal control; torque control; DTFC method; FORCER thrust ripple amplitude; IVC; LIM; MATLAB-Simulink; end-effect phenomenon; indirect vector control; linear induction motor; optimal control characteristics; Educational institutions; Induction motors; Machine vector control; Mathematical model; Rotors; Stators; Vectors; direct thrust control; end-effect phenomenon; indirect vector control; linear induction motor;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Power Engineering Conference (AUPEC), 2014 Australasian Universities
  • Conference_Location
    Perth, WA
  • Type

    conf

  • DOI
    10.1109/AUPEC.2014.6966485
  • Filename
    6966485