• DocumentCode
    1099410
  • Title

    Nonlinear Model Predictive Formation Flight

  • Author

    Shin, Jongho ; Kim, H. Jin

  • Author_Institution
    Sch. of Mech. & Aerosp. Eng., Seoul Nat. Univ., Seoul, South Korea
  • Volume
    39
  • Issue
    5
  • fYear
    2009
  • Firstpage
    1116
  • Lastpage
    1125
  • Abstract
    This correspondence paper presents the validation of a formation flight control technique with obstacle avoidance capability based on nonlinear model predictive algorithms. Control architectures for multi-agent systems employed in this correspondence paper can be categorized as centralized, sequential decentralized, and fully decentralized methods. Centralized methods generally have better performance than decentralized methods. However, it is well known that the performance of the centralized methods for formation flight degrades when there exists communication failure among the vehicles, and they require more computation time than the decentralized method. This correspondence paper evaluates the control performance and the computation time reduction of the sequential decentralized and fully decentralized methods in comparison with the centralized method and shows that the fully decentralized method can be made effective against short term communication failure. The control inputs for formation flight are computed by nonlinear model predictive control (NMPC). The control input saturation and state constraints are incorporated as inequality constraints using Karush Kuhn Tucker conditions in the NMPC framework, and the collision avoidance can be considered in real time. The proposed schemes are validated by numerical simulations, which include the process and measurement noise for more realistic situations.
  • Keywords
    aerospace control; collision avoidance; multi-agent systems; nonlinear control systems; predictive control; Karush Kuhn Tucker inequality constraint condition; centralized method; decentralized method; formation flight control technique; multi-agent systems; nonlinear model predictive control; obstacle avoidance capability; realtime collision avoidance; Centralized method; Karush–Kuhn–Tucker (KKT) condition; decentralized method; extended Kalman filter (EKF); formation flight; nonlinear model predictive control (NMPC); trajectory generation;
  • fLanguage
    English
  • Journal_Title
    Systems, Man and Cybernetics, Part A: Systems and Humans, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    1083-4427
  • Type

    jour

  • DOI
    10.1109/TSMCA.2009.2021935
  • Filename
    5109714