• DocumentCode
    1785860
  • Title

    Modeling control and simulation of two axes gimbal seeker using fuzzy PID controller

  • Author

    Abdo, Maher ; Vali, Ahmad Reza ; Toloei, Ali Reza ; Arvan, Mohammad Reza

  • Author_Institution
    Electr. Eng., Malek Ashter Univ., Tehran, Iran
  • fYear
    2014
  • fDate
    20-22 May 2014
  • Firstpage
    1342
  • Lastpage
    1347
  • Abstract
    The application of the guided missile seeker is to provide stability to the sensor by isolating it from the missile motion and vibration. The aim of this paper is to present the model of two axes gimbal seeker and improve its performance using proposed fuzzy controller. The equations of gimbals motion are derived using Lagrange equation and the stabilization system is constructed considering the missile rates, torque disturbances, and cross coupling between elevation and azimuth channels. The overall control system is simulated using MATLAB/Simulink. This model is evaluated comparing with conventional PI control system. The comparative simulation results in different conditions have shown that the proposed fuzzy PID method offers a better performance than the classical one.
  • Keywords
    PI control; fuzzy control; mathematics computing; missile control; motion control; simulation; stability; three-term control; vibration control; Lagrange equation; Matlab; PI control system; Simulink; fuzzy PID controller; guided missile seeker; missile motion; missile vibration; modeling control; simulation; stabilization system; two axes gimbal seeker; Azimuth; Control systems; Dynamics; Equations; Mathematical model; Missiles; Zirconium; gimbal seeker; guided missile; line of sight; rate gyro; servo tracking loop;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electrical Engineering (ICEE), 2014 22nd Iranian Conference on
  • Conference_Location
    Tehran
  • Type

    conf

  • DOI
    10.1109/IranianCEE.2014.6999742
  • Filename
    6999742