• DocumentCode
    3206844
  • Title

    A UAS capability description framework: Reactive, adaptive, and cognitive capabilities in robotics

  • Author

    Visnevski, Nikita A. ; Castillo-Effe, Mauricio

  • Author_Institution
    Signal Electron. & Embedded Syst., Gen. Electr. Global Res., Niskayuna, NY
  • fYear
    2009
  • fDate
    7-14 March 2009
  • Firstpage
    1
  • Lastpage
    7
  • Abstract
    This paper offers a framework that helps in characterizing, analyzing, and developing Unmanned Autonomous Systems (UAS) capabilities including autonomy, adaptability, and machine cognition. We propose a technical reference model that brings these levels of capabilities together into a three-dimensional graphical model. Based on this technical reference model, we offer a system-theoretic analysis framework that includes three views into systems capabilities - reactive, adaptive and cognitive. For illustration purposes, this framework is applied to the analysis of capabilities of autonomous systems derived from four fundamental schools of thought in robotics - deliberative, reactive, hybrid and probabilistic. This exercise helps in understanding where the state of the art currently is in terms of UAS capabilities, what capabilities modern UAS lack, and what capabilities could be expected in the near future. The approach presented in this work provides a useful foundation for capability development and capability testing in UAS.
  • Keywords
    aerospace robotics; mobile robots; remotely operated vehicles; capability testing; machine cognition; robotic adaptive capabilities; robotic cognitive capabilities; robotic reactive capabilities; unmanned autonomous systems; Cognition; Cognitive robotics; Control systems; Educational institutions; Embedded system; Graphical models; Humans; Signal analysis; System testing; Unmanned aerial vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace conference, 2009 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4244-2621-8
  • Electronic_ISBN
    978-1-4244-2622-5
  • Type

    conf

  • DOI
    10.1109/AERO.2009.4839601
  • Filename
    4839601