• DocumentCode
    548367
  • Title

    Reduced order modeling for Unmanned Aerial Vehicle

  • Author

    Gadewadikar, J. ; Kuljaca, O. ; Horvat, K.

  • Author_Institution
    Syst. Res. Inst., Alcorn State Univ., Lorman, MS, USA
  • fYear
    2011
  • fDate
    23-27 May 2011
  • Firstpage
    664
  • Lastpage
    667
  • Abstract
    This paper presents a reduced order modeling procedure for Rotary wing Unmanned Aerial Vehicles. There is a growing interest in developing control strategies for unmanned autonomous helicopters, in particular a small scale one. The procedure for deriving a six degrees-of-freedom module form standard 12th order rigid body dynamics is given.
  • Keywords
    aerospace components; aircraft control; reduced order systems; remotely operated vehicles; reduced order modeling; rotary wing unmanned aerial vehicle; unmanned autonomous helicopter; Aerodynamics; Barium; Equations; Helicopters; Mathematical model; Reduced order systems; Vehicle dynamics;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    MIPRO, 2011 Proceedings of the 34th International Convention
  • Conference_Location
    Opatija
  • Print_ISBN
    978-1-4577-0996-8
  • Type

    conf

  • Filename
    5967137
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=548367