DocumentCode :
1148249
Title :
Automatic Solution of Nthorder Optimal Control Problems
Author :
Kalaba, R. ; Spingarn, K.
Author_Institution :
Hughes Aircraft Company
Issue :
3
fYear :
1985
fDate :
5/1/1985 12:00:00 AM
Firstpage :
345
Lastpage :
350
Abstract :
An automatic method for obtaining the numerical solution of a certain class of nth-order nonlinear optimal control problems is described. The derivatives required for the solution of the two-point boundary value problem are computed automatically. The user of the program need only input the Hamiltonian function by calling the appropriate Fortran subroutines. This paper extends the methods described by the authors in previous papers in that it increases the order of the system that can be handled by the program from second order to the general nth order.
Keywords :
Aerospace control; Aircraft; Algorithms; Boundary conditions; Boundary value problems; Cost function; Equations; Gradient methods; Optimal control; Software packages;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.1985.310564
Filename :
4104063
Link To Document :
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