• DocumentCode
    580688
  • Title

    Critical subsystem failure mitigation in an indoor UAV testbed

  • Author

    Mueller, Mark W. ; D´Andrea, Raffaello

  • Author_Institution
    Inst. for Dynamic Syst. & Control, ETH Zurich, Zurich, Switzerland
  • fYear
    2012
  • fDate
    7-12 Oct. 2012
  • Firstpage
    780
  • Lastpage
    785
  • Abstract
    An autonomous safety mechanism is presented, as implemented in an indoor flying vehicle research testbed. The safety mechanism relies on integration of onboard gyroscope measurements and thrust commands to estimate the vehicle state for short lengths of time. It is used in the case of loss of external control signal or loss of external measurement data, to reduce the likelihood of a vehicle crash, or at least reduce the severity of an unavoidable crash. As UAVs move into ever more mainstream applications with increased public interaction, such safety systems become more critical.
  • Keywords
    aircraft testing; autonomous aerial vehicles; failure analysis; gyroscopes; space vehicles; state estimation; vehicle dynamics; autonomous safety mechanism; critical subsystem failure mitigation; external control signal; external measurement data; indoor UAV testbed; indoor flying vehicle research testbed; onboard gyroscope measurements; public interaction; safety systems; thrust commands; unavoidable crash; vehicle crash; vehicle state estimation; Channel estimation; Gyroscopes; Propellers; Safety; Switches; Vehicle crash testing; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Robots and Systems (IROS), 2012 IEEE/RSJ International Conference on
  • Conference_Location
    Vilamoura
  • ISSN
    2153-0858
  • Print_ISBN
    978-1-4673-1737-5
  • Type

    conf

  • DOI
    10.1109/IROS.2012.6385910
  • Filename
    6385910