• DocumentCode
    530734
  • Title

    Backstepping control of each channel for a quadrotor aerial robot

  • Author

    Yali, Yu ; Changhong, Jiang ; Haiwei, Wu

  • Author_Institution
    Eng. Training Center, Harbin Eng. Univ., Harbin, China
  • Volume
    3
  • fYear
    2010
  • fDate
    24-26 Aug. 2010
  • Firstpage
    403
  • Lastpage
    407
  • Abstract
    This paper has presented a model of vertical take-off and landing(VTOL) unmanned air vehicle. It has four rotors, so as quadrotor aerial robot. It can hover or fly at low speed indoor or unwinded outdoor. The quadrotor aerial robot is a highly nonlinear, multivariable, strongly coupled and under-actuated subsystem because it has 6-DOF but only has four inputs. Nonlinear mathematical model of quadrotor aerial robot which is based on Newton-Euler formalism is deduced in the paper, also described nonlinear control strategy for it. Backstepping of nonlinear controller design was based on constructing Lyapunov function for closed-loop system. The controller guarantees stability, tracking performance and robotness of the system. The effective control design scheme is shown through nonlinear simulations.
  • Keywords
    Lyapunov methods; aircraft control; closed loop systems; control system synthesis; helicopters; mobile robots; multivariable control systems; nonlinear control systems; remotely operated vehicles; Lyapunov function; Newton-Euler formalism; backstepping control; closed-loop system; nonlinear controller design; nonlinear mathematical model; quadrotor aerial robot; under-actuated subsystem; vertical take-off and landing unmanned air vehicle; Bismuth; Educational institutions; Force; Lead; Robots; Torque; Yttrium; Backstepping; Newton-Euler formalism; VTOL; quadrotor aerial robot;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computer, Mechatronics, Control and Electronic Engineering (CMCE), 2010 International Conference on
  • Conference_Location
    Changchun
  • Print_ISBN
    978-1-4244-7957-3
  • Type

    conf

  • DOI
    10.1109/CMCE.2010.5610299
  • Filename
    5610299