• DocumentCode
    3073434
  • Title

    Successive Galerkin approximation of nonlinear optimal attitude

  • Author

    Lawton, Jonathan ; Beard, Randal W. ; Mclain, Tim

  • Author_Institution
    Dept. of Electr. & Comput. Eng., Brigham Young Univ., Provo, UT, USA
  • Volume
    6
  • fYear
    1999
  • fDate
    1999
  • Firstpage
    4373
  • Abstract
    This paper presents the application of the successive Galerkin approximation (SGA) to the Hamilton-Jacobi-Bellman equation to obtain solutions of the optimal attitude control problem. Galerkin´s method approximates the value function by a truncated Galerkin series expansion. To do so, a truncated Galerkin basis set is formed. A sufficient number of functions must be included in this Galerkin basis set in order to guarantee that the solution will be a stabilizing control. By increasing the size of the Galerkin basis the quality of the approximation is improved at the cost of rapid growth in the computation load of the SGA. A major result of this paper is the development of the Galerkin basis set in the context of the optimal attitude control problem
  • Keywords
    Galerkin method; approximation theory; attitude control; dynamics; feedback; kinematics; nonlinear control systems; optimal control; robust control; Galerkin approximation; Hamilton-Jacobi-Bellman equation; aerospace control; attitude control; dynamics; feedback; kinematics; nonlinear control systems; optimal control; robust control; Angular velocity; Angular velocity control; Attitude control; Equations; Kinematics; Linear feedback control systems; Moment methods; Optimal control; Performance analysis; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1999. Proceedings of the 1999
  • Conference_Location
    San Diego, CA
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-4990-3
  • Type

    conf

  • DOI
    10.1109/ACC.1999.786394
  • Filename
    786394