• DocumentCode
    1319496
  • Title

    The GRASP Multiple Micro-UAV Testbed

  • Author

    Michael, Nathan ; Mellinger, Daniel ; Lindsey, Quentin ; Kumar, Vijay

  • Author_Institution
    Mech. Eng., Univ. of Pennsylvania, Philadelphia, PA, USA
  • Volume
    17
  • Issue
    3
  • fYear
    2010
  • Firstpage
    56
  • Lastpage
    65
  • Abstract
    In the last five years, advances in materials, electronics, sensors, and batteries have fueled a growth in the development of microunmanned aerial vehicles (MAVs) that are between 0.1 and 0.5 m in length and 0.1-0.5 kg in mass [1]. A few groups have built and analyzed MAVs in the 10-cm range [2], [3]. One of the smallest MAV is the Picoftyer with a 60-mmpropellor diameter and a mass of 3.3 g [4]. Platforms in the 50-cm range are more prevalent with several groups having built and flown systems of this size [5]-[7]. In fact, there are severalcommercially available radiocontrolled (PvC) helicopters and research-grade helicopters in this size range [8].
  • Keywords
    aerospace control; helicopters; mobile robots; remotely operated vehicles; GRASP; MAV; flown systems; microunmanned aerial vehicles; multiple micro-UAV testbed; research grade helicopters; Acceleration; Mathematical model; Robot kinematics; Rotors; Software; Trajectory; Unmanned aerial vehicles;
  • fLanguage
    English
  • Journal_Title
    Robotics & Automation Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    1070-9932
  • Type

    jour

  • DOI
    10.1109/MRA.2010.937855
  • Filename
    5569026