Optimal principle for dynamical system with alterative orbiting

Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/29436

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DC Field	Value	Language
dc.contributor.author	Lysenko, O.I.	en
dc.contributor.author	Tachinina, O.M.	en
dc.date.accessioned	2017-06-15T19:30:20Z	-
dc.date.available	2017-06-15T19:30:20Z	-
dc.date.issued	2016	-
dc.identifier.issn	1990-5548	-
dc.identifier.uri	http://er.nau.edu.ua/handle/NAU/29436	-
dc.description.abstract	Lagrange 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.iso	en	en
dc.publisher	Electronics and Control Systems 2016. N 4(50).- p.108-113	en
dc.subject	optimization	en
dc.title	Optimal principle for dynamical system with alterative orbiting	en
dc.type	Article	en
Appears in Collections:	Наукові статті кафедри автоматизації та енергоменеджменту

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