• DocumentCode
    1751588
  • Title

    Robust state dependent Riccati equation based guidance laws

  • Author

    Balakrishnan, Sivasubramanya N. ; Xin, Ming

  • Author_Institution
    Dept. of Mech. & Aerosp. Eng., Missouri Univ., Rolla, MO, USA
  • Volume
    5
  • fYear
    2001
  • fDate
    2001
  • Firstpage
    3352
  • Abstract
    A robust state dependent Riccati equation based guidance/control is investigated in this study. In order to have a better design tool in terms of required interceptor accelerations, the target intercept geometry is formulated in a set of polar coordinates. With this formulation, we formulate a cost function with state dependent weights. In this study, we investigate the effects of such cost functions on the levels of interceptor accelerations. We also synthesize a neural network based extra controller to achieve the robustness in the presence of the target acceleration. In this manner, we will not need target acceleration estimation explicitly in the guidance law
  • Keywords
    Riccati equations; control system synthesis; missile guidance; neurocontrollers; robust control; cost function; homing missile guidance; intercept geometry; interceptor accelerations; missile control; neural network based extra controller; polar coordinates; robust state dependent Riccati equation based guidance laws; state dependent weights; Acceleration; Cost function; Missiles; Navigation; Nonlinear equations; Optimal control; Riccati equations; Robust control; Robustness; Sliding mode control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 2001. Proceedings of the 2001
  • Conference_Location
    Arlington, VA
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-6495-3
  • Type

    conf

  • DOI
    10.1109/ACC.2001.946146
  • Filename
    946146