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
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