Please use this identifier to cite or link to this item: https://hdl.handle.net/2440/85334
Citations
Scopus Web of Science® Altmetric
?
?
Full metadata record
DC FieldValueLanguage
dc.contributor.authorTeo, K.L.-
dc.contributor.authorGoh, C.J.-
dc.contributor.authorLim, C.C.-
dc.date.issued1989-
dc.identifier.citationIMA Journal of Mathematical Control and Information, 1989; 6(1):81-95-
dc.identifier.issn0265-0754-
dc.identifier.issn1471-6887-
dc.identifier.urihttp://hdl.handle.net/2440/85334-
dc.description.abstractIn this paper, we consider a class of dynamical optimization problems in which the terminal time is determined by a stopping criterion. The dynamical system is described by a system of ordinary differential equations, and the cost functional is to be minimized with respect to the control together with the initial vector. A computational method based on the concept of control parametrization is developed for solving this class of dynamical optimization problems. For illustration, an aeronautical control problem is solved using the proposed method. © 1989 Oxford University Press.-
dc.description.statementofresponsibilityK. L. Teo, C. J. Goh and C. C. Lim-
dc.language.isoen-
dc.publisherOxford University Press-
dc.rights© Oxford University Press-
dc.source.urihttp://dx.doi.org/10.1093/imamci/6.1.81-
dc.titleA computational method for a class of dynamical optimization problems in which the terminal time is conditionally free-
dc.typeJournal article-
dc.identifier.doi10.1093/imamci/6.1.81-
pubs.publication-statusPublished-
dc.identifier.orcidLim, C.C. [0000-0002-2463-9760]-
Appears in Collections:Aurora harvest 2
Electrical and Electronic Engineering publications

Files in This Item:
There are no files associated with this item.


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.