DocumentCode :
485924
Title :
Automatic Solution of Optimal Control Problems II. First-Order Nonlinear Systems
Author :
Kalaba, R. ; Spingarn, X.
Author_Institution :
Departments of Economics and Biomedical Engineering, University of Southern California, Los Angeles, California 90007
fYear :
1983
fDate :
22-24 June 1983
Firstpage :
1035
Lastpage :
1040
Abstract :
An automatic method for obtaining the numerical solution for first-order nonlinear optimal control problems is described. The nonlinear two-point boundary value Euler-Lagrange equation 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 specify the initial conditions and the terminal time. None of the derivatives usually associated with the Euler-Lagrange equation and the Newton-Raphson method need be calculated by hand. An example is given with numerical results.
Keywords :
Aircraft; Airports; Calculus; Cost function; Differential equations; Integral equations; Newton method; Nonlinear systems; Optimal control; Tellurium;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1983
Conference_Location :
San Francisco, CA, USA
Type :
conf
Filename :
4788266
Link To Document :
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