• DocumentCode
    3175156
  • Title

    Robust backstepping control of missile lateral and rolling motions in the presence of unmatched uncertainties

  • Author

    Mattei, G. ; Monaco, S.

  • Author_Institution
    Inf., Autom. e Gestionale “Antonio Ruberti“, Sapienza Univ. of Rome, Rome, Italy
  • fYear
    2012
  • fDate
    10-13 Dec. 2012
  • Firstpage
    2878
  • Lastpage
    2883
  • Abstract
    The paper deals with the problem of nonlinear robust stabilization and tracking via state feedback. A robust version of backstepping is designed to control both lateral and rolling motions of a generic air-to-air missile, whose dynamics is highly nonlinear and uncertain. Two kinds of uncertainties are considered: matched and unmatched, whose bounds are assumed to be known a-priori. The nonlinear robust autopilot ensures tracking of sideslip angle reference signal and regulation of bank angle, while maintaining bounded yaw and roll rates. The novelty of the proposed approach relies in a direct compensation of control inputs cross-couplings between lateral and rolling motions, which are generated by differential pressure on the tail-fins.
  • Keywords
    control system synthesis; missile control; motion control; nonlinear control systems; robust control; state feedback; uncertain systems; air-to-air missile; bank angle regulation; missile lateral motion; missile rolling motion; nonlinear robust stabilization; robust backstepping control; sideslip angle reference signal tracking; state feedback; unmatched uncertainties; Aerodynamics; Backstepping; Missiles; Robustness; Tracking; Uncertainty; Lyapunov based design; Missile autopilot; Nonlinear control; Robust Backstepping; Unmatched uncertainties;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control (CDC), 2012 IEEE 51st Annual Conference on
  • Conference_Location
    Maui, HI
  • ISSN
    0743-1546
  • Print_ISBN
    978-1-4673-2065-8
  • Electronic_ISBN
    0743-1546
  • Type

    conf

  • DOI
    10.1109/CDC.2012.6426605
  • Filename
    6426605