Rendezvous of two spacecraft in LEO with use tether

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DC Field	Value	Language
dc.date	2018
dc.date.accessioned	2025-08-22T12:19:37Z	-
dc.date.available	2025-08-22T12:19:37Z	-
dc.date.issued	2018
dc.identifier.identifier	Dspace\SGAU\20180516\69406
dc.identifier.citation	Aslanov V.S. Rendezvous of two spacecraft in LEO with use tether / V.S. Aslanov, R.S. Pikalov // Сборник трудов IV международной конференции и молодежной школы «Информационные технологии и нанотехнологии» (ИТНТ-2018) - Самара: Новая техника, 2018. - С.1960-1968.
dc.identifier.uri	http://repo.ssau.ru/jspui/handle/123456789/13988	-
dc.description.abstract	This study focuses on a dynamics of a rendezvous of a tug and a large space debris connected by a viscoelastic tether. It is assumed that the constant thrust acts on the space tug and a control is realized by changing the length of the tether. The goal is to find the control law that provides a soft docking of two bodies on an orbit. Three-body system with an additional damping device is also considered. The obtained results can be applied as applications for the tasks of implement rendezvous of two bodies using the tether.
dc.description.sponsorship	This work is supported by the Russian Foundation for Basic Research, Project No. 17-41-630274- region
dc.language	en_US
dc.publisher	Новая техника
dc.title	Rendezvous of two spacecraft in LEO with use tether
dc.type	Article
local.identifier.olduri	http://repo.ssau.ru/handle/Informacionnye-tehnologii-i-nanotehnologii/Rendezvous-of-two-spacecraft-in-LEO-with-use-tether-69406
local.identifier.olduri	http://repo.ssau.ru/handle/Informacionnye-tehnologii-i-nanotehnologii/Rendezvous-of-two-spacecraft-in-LEO-with-use-tether-69406
Appears in Collections:	Информационные технологии и нанотехнологии

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