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