• DocumentCode
    2072945
  • Title

    Flight Simulation Testbed of Unmanned Helicopter

  • Author

    Wu, Jiande ; Feng, Ting ; Fan, Yugang

  • Author_Institution
    Fac. of Inf. Eng. & Autom., Kunming Univ. of Sci. & Technol., Kunming, China
  • fYear
    2009
  • fDate
    26-28 Dec. 2009
  • Firstpage
    497
  • Lastpage
    499
  • Abstract
    This paper designed a flight simulation testbed of unmanned helicopter. This testbed has the advantage of simple structure, easy implement, low cost, convenient movement and so on. It is suitable for various flight test of mini-unmanned helicopter. It provides attitude needed by unmanned helicopter, such as pitch, yaw, roll and so on, to ensure that unmanned helicopter can be free flight within a certain range. Making use of the testbed can reproduce the actual flight of unmanned helicopter under laboratory conditions, and can be very convenient for attitude control, flight control, navigation and other scientific researches; accordingly, it ensures the security of flight test for unmanned helicopter.
  • Keywords
    aerospace simulation; attitude control; helicopters; mobile robots; remotely operated vehicles; attitude control; flight control; flight simulation testbed; mini unmanned helicopter; Aerospace engineering; Aerospace simulation; Computational modeling; Costs; Design engineering; Helicopters; Paper technology; Vehicle crash testing; Winches; Wire; flight simulation; testbed; unmanned helicopter;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Information Science and Engineering (ISISE), 2009 Second International Symposium on
  • Conference_Location
    Shanghai
  • Print_ISBN
    978-1-4244-6325-1
  • Electronic_ISBN
    978-1-4244-6326-8
  • Type

    conf

  • DOI
    10.1109/ISISE.2009.56
  • Filename
    5447291