Отрывок: We compare the motion of the system without damping device (8) and with it (16). The simulations are run for 3000 seconds for the initial altitude is 800 km and the initial velocities of the space tug and space debris to each other and correspond to a circular orbit. The rendezvous maneuver is performed within the first 2500 seconds, during which the tether length is reduced to the value L . After...
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dc.contributor.authorAslanov, V.S.-
dc.contributor.authorPikalov, R.S.-
dc.date.accessioned2018-05-18 10:50:47-
dc.date.available2018-05-18 10:50:47-
dc.date.issued2018-
dc.identifierDspace\SGAU\20180516\69406ru
dc.identifier.citationAslanov 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.ru
dc.identifier.urihttp://repo.ssau.ru/handle/Informacionnye-tehnologii-i-nanotehnologii/Rendezvous-of-two-spacecraft-in-LEO-with-use-tether-69406-
dc.description.abstractThis 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.ru
dc.description.sponsorshipThis work is supported by the Russian Foundation for Basic Research, Project No. 17-41-630274- regionru
dc.language.isoen_USru
dc.publisherНовая техникаru
dc.subjectspace debris removalru
dc.subjectspacecraft rendezvousru
dc.subjectspace tetherru
dc.subjectcontrol lawru
dc.subjectsoft dockingru
dc.titleRendezvous of two spacecraft in LEO with use tetherru
dc.typeArticleru
dc.textpartWe compare the motion of the system without damping device (8) and with it (16). The simulations are run for 3000 seconds for the initial altitude is 800 km and the initial velocities of the space tug and space debris to each other and correspond to a circular orbit. The rendezvous maneuver is performed within the first 2500 seconds, during which the tether length is reduced to the value L . After...-
Располагается в коллекциях: Информационные технологии и нанотехнологии

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