• DocumentCode
    489513
  • Title

    A Feedback Descent Method for Solving Constrained LQG Control Problems

  • Author

    Beseler, Jan ; Chow, Joe H. ; Minto, K.D.

  • Author_Institution
    GE Aircraft Engine, Lynn, MA. 01910
  • fYear
    1992
  • fDate
    24-26 June 1992
  • Firstpage
    1044
  • Lastpage
    1048
  • Abstract
    This paper presents a new method for the numerical solution of LQG optimal control problems subject to constraints. In general, solutions to these problems necessarily satisfy a set of coupled Lyapunov and/or Riccati equations. These equations are solved in an iterative manner based on a quasi-Newton type algorithm. Key features of the method are the simplicity afforded in developing iterative algorithms satisfying the necessary conditions for solution of such problems, and the speed and efficiency of these algorithms. The technique is illustrated for the optimal static output feedback problem and the optimal LQG problem with an H¿ norm bound on a closed-loop transfer function.
  • Keywords
    Aircraft propulsion; Helium; Newton method; Optimal control; Output feedback; Research and development; Riccati equations; Robustness; Transfer functions; White noise;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1992
  • Conference_Location
    Chicago, IL, USA
  • Print_ISBN
    0-7803-0210-9
  • Type

    conf

  • Filename
    4792244