• DocumentCode
    3632238
  • Title

    Attitude control of a quadrotor

  • Author

    I. Can Dikmen;Aydemir Arisoy;Hakan Temeltas

  • Author_Institution
    Air Force Academy, ASTIN, Istanbul/TURKEY
  • fYear
    2009
  • Firstpage
    722
  • Lastpage
    727
  • Abstract
    This study includes altitude stabilization, hovering control any desired position and attitude control of quadrotor. Classically PD controller derived and applied to this system. Inverse dynamic control, feedback linearization control and sliding mode control methods have used to derive as nonlinear controllers. Linear and nonlinear control techniques applied to attitude control of this vehicle. Derived control methods have been performed using computer simulations and compared the results according to this study objective.
  • Keywords
    "Sliding mode control","Linear feedback control systems","Vehicle dynamics","PD control","Unmanned aerial vehicles","Nonlinear dynamical systems","Control systems","Computer simulation","Propellers","Consumer electronics"
  • Publisher
    ieee
  • Conference_Titel
    Recent Advances in Space Technologies, 2009. RAST ´09. 4th International Conference on
  • Print_ISBN
    978-1-4244-3626-2;978-1-4244-3627-9
  • Type

    conf

  • DOI
    10.1109/RAST.2009.5158286
  • Filename
    5158286