• DocumentCode
    681152
  • Title

    Attitude control of a quadrotor aircraft using LQR state feedback controller with full order state observer

  • Author

    Panomrattanarug, Benjamas ; Higuchi, Kohji ; Mora-Camino, Felix

  • Author_Institution
    Department of Control Systems and Instrumentation Engineering, King Mongkuts University of Technology Thonburi, Bangkok 10140 Thailand
  • fYear
    2013
  • fDate
    14-17 Sept. 2013
  • Firstpage
    2041
  • Lastpage
    2046
  • Abstract
    This paper presents an attitude control scheme that can track the desired Euler angle trajectories. The proposed controller is based on an optimization technique designed in the discrete time domain. All state variables are estimated using a full-order state observer. The simulation results show tracking performance of the designed controller compared with a classical PD controller.
  • Keywords
    Aerospace electronics; Aircraft; Atmospheric modeling; Attitude control; Observers; Simulation; Trajectory; Aircraft; Attitude control; LQR; Quadrotor;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    SICE Annual Conference (SICE), 2013 Proceedings of
  • Conference_Location
    Nagoya, Japan
  • Type

    conf

  • Filename
    6736320
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=681152