• DocumentCode
    517537
  • Title

    Linear vs. nonlinear control techniques for a quadrotor vehicle

  • Author

    Al-Younes, Younes M. ; Al-Jarrah, Mohammed A. ; Jhemi, Ali A.

  • Author_Institution
    Dept. of Mech. Eng., American Univ. of Sharjah, Sharjah, United Arab Emirates
  • fYear
    2010
  • fDate
    20-22 April 2010
  • Firstpage
    1
  • Lastpage
    10
  • Abstract
    The aim of this paper is to propose a nonlinear control algorithm that is able to stabilize the attitude and altitude of a quadrotor vehicle, and then to compare it with the classical techniques, such as PID and LQR. The nonlinear algorithm is based on the backstepping methodology integrated with the integral and adaptation schemes. It´s called “Adaptive Integral Backstepping Controller” (AIBC). The recursive Lyapunov methodology in the backstepping technique will ensure the system stability, the integral action will increase the system robustness against disturbances and model uncertainties, and the adaptation law will estimate the modeling errors caused by assumptions in simplifying the complexity of the quadrotor model. Furthermore, a quadrotor vehicle is designed and modeled in this paper to perform the controlling task.
  • Keywords
    Lyapunov methods; adaptive control; aircraft control; attitude control; control system synthesis; helicopters; nonlinear control systems; position control; AIBC; LQR; PID; adaptive integral backstepping controller; altitude stability; attitude stability; helicopters; linear control techniques; nonlinear control techniques; quadrotor vehicle; recursive Lyapunov methodology; Attitude control; Backstepping; Mathematical model; Mechatronics; Navigation; Robust stability; Sliding mode control; Software testing; Three-term control; Unmanned aerial vehicles; Adaptation; Altitude; Attitude; Backstepping; Lyapunov;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronics and its Applications (ISMA), 2010 7th International Symposium on
  • Conference_Location
    Sharjah
  • Print_ISBN
    978-1-4244-6665-8
  • Type

    conf

  • Filename
    5478427