• DocumentCode
    3573474
  • Title

    Fractional PIλ control of anti-aircraft artillery servo system

  • Author

    Gang Yang ; Chongwei Han ; Tengfei Chen ; Jing Guo

  • Author_Institution
    Northwest Inst. of Mech. & Electr. Eng., Xianyang, China
  • fYear
    2014
  • Firstpage
    4617
  • Lastpage
    4621
  • Abstract
    Anti-aircraft artillery servo system requires high tracking accuracy and strong robustness. In this paper, an algebraic tuning rule is presented for fractional PIλ controllers to control anti-aircraft artillery. A group of suitable parameters can be chosen out by drawing the curve describing relation between gain kp, ki and integral order λ when the crossover frequency and phase margin are given. The oscillation index is introduced to help decide appropriate crossover frequency and phase margin that should be set. Simulation results are brought to demonstrate the effectiveness and robustness of this parameter tuning method.
  • Keywords
    PI control; aircraft control; autonomous aerial vehicles; control system synthesis; missile control; mobile robots; servomechanisms; weapons; algebraic tuning rule; anti aircraft artillery servo system; crossover frequency; cruise missile; curve describing relation; fixed-wing aircraft; fractional PIλ controllers; gain; gunship; high tracking accuracy; integral order; oscillation index; parameter tuning method; phase margin; strong robustness; tactical UAV; DC motors; Indexes; Mathematical model; Oscillators; Robustness; Servomotors; Torque; anti-aircraft artillery; fractional PIλ control; servo system;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Control and Automation (WCICA), 2014 11th World Congress on
  • Type

    conf

  • DOI
    10.1109/WCICA.2014.7053492
  • Filename
    7053492