• DocumentCode
    488145
  • Title

    Finite Element Solution of Optimal Control Problems with Inequality Constraints

  • Author

    Bless, Robert R. ; Hodges, Dewey H.

  • Author_Institution
    Graduate Research Assistant, School of Aerospace Engineering. Student Member, AIAA; Georgia Institute of Technology, Atlanta, Georgia
  • fYear
    1990
  • fDate
    23-25 May 1990
  • Firstpage
    242
  • Lastpage
    247
  • Abstract
    A temporal finite element method based on a weak Hamiltonian form of the necessary conditions is summarized for optimal control problems. Very crude shape functions (so simple that element numerical quadrature is not necessary) can be used to develop an efficient procedure for obtaining candidate solutions (i.e., those which satisfy all the necessary conditions) even for highly nonlinear problems. An extension of the formulation allowing for discontinuities in the states and derivatives of the states is given. Furthermore, the theory to include control inequality constraints is fully developed. Finally, an Advanced Launch Vehicle (ALV) model is presented. The model involves staging and control constraints, thus demonstrating the full power of the weak formulation to date. Numerical results are presented along with total elapsed computer time required to obtain the results. The speed and accuracy in obtaining the results make this method a strong candidate for a real-time guidance algorithm.
  • Keywords
    Aerospace engineering; Constraint theory; Equations; Finite element methods; Intelligent vehicles; Lagrangian functions; Navigation; Optimal control; Performance analysis; Shape;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1990
  • Conference_Location
    San Diego, CA, USA
  • Type

    conf

  • Filename
    4790735