• DocumentCode
    2405226
  • Title

    Revisited Dos Samara Unmanned Aerial Vehicle: Design and control

  • Author

    Alexis, Kostas ; Tzes, Anthony

  • Author_Institution
    Electr. & Comput. Eng. Dept., Univ. of Patras, Greece
  • fYear
    2012
  • fDate
    14-18 May 2012
  • Firstpage
    3645
  • Lastpage
    3650
  • Abstract
    In this article, the design, system modeling and control of a new hybrid type of Unmanned Aerial Vehicle (UAV) is presented. Based on the flight principles of the Dos Samara UAV, a new vehicle that combines the capability of hovering, like a helicopter, and high speed-increased endurance flying, like a fixed-wing aircraft, is designed. The nonlinear dynamics model of the aircraft operating in helicopter mode is derived and linearized around hovering operation. Based on this model an LQ-controller is designed. The performance of the overall system is examined in simulation studies.
  • Keywords
    autonomous aerial vehicles; control system synthesis; helicopters; linear quadratic control; nonlinear dynamical systems; ίight principles; Dos Samara unmanned aerial vehicle; LQ-controller design; fixed-wing aircraft; helicopter; high speed-increased endurance flying; hovering operation; nonlinear dynamics model; system modeling; Aerodynamics; Brushless motors; Helicopters; Nonlinear dynamical systems; Propellers; Solid modeling;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Robotics and Automation (ICRA), 2012 IEEE International Conference on
  • Conference_Location
    Saint Paul, MN
  • ISSN
    1050-4729
  • Print_ISBN
    978-1-4673-1403-9
  • Electronic_ISBN
    1050-4729
  • Type

    conf

  • DOI
    10.1109/ICRA.2012.6224559
  • Filename
    6224559