Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/29436
Full metadata record
DC FieldValueLanguage
dc.contributor.authorLysenko, O.I.en
dc.contributor.authorTachinina, O.M.en
dc.date.accessioned2017-06-15T19:30:20Z-
dc.date.available2017-06-15T19:30:20Z-
dc.date.issued2016-
dc.identifier.issn1990-5548-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/29436-
dc.description.abstractLagrange problem with the account of functional limitation at any functional limitations at any moment in a given interval is presented. The required conditions for optimal trajectories of the determinated dynamic system synthesized as space vehicle trajectories have been obtained.en
dc.language.isoenen
dc.publisherElectronics and Control Systems 2016. N 4(50).- p.108-113en
dc.subjectoptimizationen
dc.titleOptimal principle for dynamical system with alterative orbitingen
dc.typeArticleen
Appears in Collections:Наукові статті кафедри автоматизації та енергоменеджменту

Files in This Item:
File Description SizeFormat 
etsu_2016_4_21.pdfСтаття673.48 kBAdobe PDFView/Open


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