• DocumentCode
    1786341
  • Title

    Non-smooth missiles guidance: Interceptor-defender scenario with uncertainties

  • Author

    Poznyak, Alexander

  • Author_Institution
    CINVESTAV-IPN, Mexico City, Mexico
  • fYear
    2014
  • fDate
    June 29 2014-July 2 2014
  • Firstpage
    1
  • Lastpage
    6
  • Abstract
    Here the dynamic scenario with two participants (an interceptor interpreted as an anti-missile and a defender treated as an anti-anti-missile) is considered. The first one (an interceptor) is intended to reach a capture zone, associated with a given nominal trajectory of a missile which is assumed to be non-maneuvered. But in the same time it should maintain a large enough distance from the second player (a defender) whose individual aim is to protect the nominal plant (a missile). The second participant realizes its behavior in such a way that its position would be as close as possible to an interceptor and far enough from a missile which it protects. Individual cost functions related with non-smooth feedback control strategies for each participant are introduced. The gain parameters of the non-smooth feedbacks are selected in an “optimal manner” providing the biggest rate of convergence to the desired regime. The effective zones in the state space, where the designed control decreases the cost functions, are obtained. Illustrative numerical simulations confirm the workability of the suggested approach.
  • Keywords
    control system synthesis; convergence; feedback; missile guidance; numerical analysis; optimal control; state-space methods; trajectory control; uncertain systems; anti-anti-missile; capture zone; control design; convergence rate; cost functions; dynamic scenario; gain parameters; interceptor-defender scenario; missile position; nominal plant; nominal trajectory; nonsmooth feedback control strategies; nonsmooth missiles guidance; numerical simulations; optimal manner; state space; uncertainties; Bismuth; Cost function; Missiles; Numerical models; Trajectory; Uncertainty; Vectors; Missile guidance; finite time convergence; non-smooth feedback;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Variable Structure Systems (VSS), 2014 13th International Workshop on
  • Conference_Location
    Nantes
  • Type

    conf

  • DOI
    10.1109/VSS.2014.6881125
  • Filename
    6881125