• DocumentCode
    1595098
  • Title

    Improved Algorithm Simulation of Adaptive Blade Pitch Control for Electrically Controlled Rotor

  • Author

    Dong Weisheng ; Lu Yang

  • Author_Institution
    Nat. Key Lab. of Rotorcraft Aeromechanics, Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
  • fYear
    2012
  • Firstpage
    691
  • Lastpage
    695
  • Abstract
    Based on the former adaptive blade pitch control method of the Electrically Controlled Rotor in time domain, two improved control algorithms are proposed. One method is through adding a weight-constrained function for active control filter, which can prevent the divergent of control system caused by interference signal of error channel. The other method is through adding a desired signal of scaling factor to replace the identification process of the forward path. The algorithm can enhance the real time characteristics and the response characteristics of control system. In addition, the comparison between two improved methods and the former method is conducted, and the simulation analysis is made based on the matlab/simulink. The simulation results show that the two proposed methods have better system robustness, and the control characteristics are obviously superior to the former system.
  • Keywords
    active filters; adaptive control; blades; helicopters; rotors; Matlab/Simulink; active control filter; adaptive blade pitch control method; electrically controlled rotor; helicopter; improved algorithm simulation; interference signal; simulation analysis; weight-constrained function; Adaptation models; Blades; Control systems; Helicopters; Noise; Rotors; Simulation; Adaptive Control; Blade Pitch Control; Electrically Controlled Rotor; Simulation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent System Design and Engineering Application (ISDEA), 2012 Second International Conference on
  • Conference_Location
    Sanya, Hainan
  • Print_ISBN
    978-1-4577-2120-5
  • Type

    conf

  • DOI
    10.1109/ISdea.2012.594
  • Filename
    6173300