• DocumentCode
    693019
  • Title

    The application requirement analysis and system design of shipborne small multi-rotors unmanned aerial vehicle

  • Author

    Fan SongWei ; Bian HongWei

  • Author_Institution
    Dept. of Navig., Electr. Eng. Acad., Naval Univ. of Eng., Wuhan, China
  • fYear
    2013
  • fDate
    20-22 Dec. 2013
  • Firstpage
    2812
  • Lastpage
    2816
  • Abstract
    The small multi-rotors unmanned aerial vehicle (UAV) fits for complex narrow ship environment. Using it could improve the efficiency of the lots of ship task. The tasks include the carry mission and video mission could be performed by the small multi-rotors UAV. According to the mission requirements: low weight, small size, antivibration, low power consumption, and easy interfacing, the vehicle system is designed in four subsystems: flight power subsystem, long-range wireless data link subsystem, flight control subsystem and ground control subsystem. The model vehicle is constructed and the flying experiment shows that the model vehicle could realize steady flight and Airline flight, meets the design requirements.
  • Keywords
    autonomous aerial vehicles; rotors; UAV; airline flight; carry mission; design requirements; flight control subsystem; flight power subsystem; ground control subsystem; long-range wireless data link subsystem; mission requirements; ship environment; ship task; shipborne small multi-rotors unmanned aerial vehicle; steady flight; video mission; Aircraft; Aircraft propulsion; Humidity measurement; Magnetic field measurement; Navigation; Size measurement; Weight measurement; application requirement analysis; shipborne multi-rotors; system design;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronic Sciences, Electric Engineering and Computer (MEC), Proceedings 2013 International Conference on
  • Conference_Location
    Shengyang
  • Print_ISBN
    978-1-4799-2564-3
  • Type

    conf

  • DOI
    10.1109/MEC.2013.6885508
  • Filename
    6885508