• DocumentCode
    2467385
  • Title

    Safe Receding Horizon Control of an Aerial Vehicle

  • Author

    Anisi, David A. ; Ögren, Petter ; Robinson, John W C

  • Author_Institution
    Dept. of Optimization & Syst. Theor., R. Inst. of Technol., Stockholm
  • fYear
    2006
  • fDate
    13-15 Dec. 2006
  • Firstpage
    57
  • Lastpage
    62
  • Abstract
    This paper addresses the problem of designing a real time high performance controller and trajectory generator for air vehicles. The control objective is to use information about terrain and enemy threats to fly low and avoid radar exposure on the way to a given target. The proposed algorithm builds on the well known approach of receding horizon control (RHC) combined with a terminal cost, calculated from a graph representation of the environment. Using a novel safety maneuver, and under an assumption on the maximal terrain inclination, we are able to prove safety as well as task completion. The safety maneuver is incorporated in the short term optimization, which is performed using nonlinear programming (NLP). Some key characteristics of the trajectory planner are highlighted through simulations
  • Keywords
    aircraft control; graph theory; nonlinear programming; position control; aerial vehicle; graph representation; nonlinear programming; optimization; real time high performance controller; receding horizon control; safety maneuver; trajectory generator; trajectory planning; Control systems; Helicopters; Mobile robots; Radar; Real time systems; Remotely operated vehicles; Trajectory; USA Councils; Unmanned aerial vehicles; Vehicle safety;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 2006 45th IEEE Conference on
  • Conference_Location
    San Diego, CA
  • Print_ISBN
    1-4244-0171-2
  • Type

    conf

  • DOI
    10.1109/CDC.2006.377657
  • Filename
    4177206