• DocumentCode
    857424
  • Title

    Automatic solution of optimal control problems III: Differential and integral constraints

  • Author

    Kalaba, R. ; Spingarn, K.

  • Author_Institution
    University of Southern California, Los Angeles, CA, USA and Hughes Aircraft Company, El Segundo, CA, USA
  • Volume
    4
  • Issue
    1
  • fYear
    1984
  • fDate
    2/1/1984 12:00:00 AM
  • Firstpage
    3
  • Lastpage
    8
  • Abstract
    An automatic method for obtaining the numerical solution of a certain class of second-order nonlinear optimal control problems with differential and integral constraints is described. The nonlinear two-point boundary value problem is solved using the Newton-Raphson method for obtaining successive approximations of the solution. The derivatives required for the solution of the problem are computed automatically using the table method. The user of the program need only input the integrand of the cost functional and the differential constraints and specify the intial conditions and the terminal time. None of the derivatives usually associated with Pontryagin´s maximum principle and the Newton-Raphson method need be calculated by hand. A set of FORTRAN subroutines in the program for solving the optimal control problems is described. An example is given with numerical results.
  • Keywords
    Newton-Raphson methods; Optimal control, nonlinear systems; Aerospace control; Aircraft propulsion; Algorithms; Automatic control; Cost function; Differential equations; Newton method; Optimal control;
  • fLanguage
    English
  • Journal_Title
    Control Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0272-1708
  • Type

    jour

  • DOI
    10.1109/MCS.1984.1104786
  • Filename
    1104786