 | | Mechanics of Solids
A Journal of Russian Academy of Sciences | | Founded
in January 1966
Issued 6 times a year
Print ISSN 0025-6544
Online ISSN 1934-7936 |
Archive of Issues
| Total articles in the database: | | 12804 |
| In Russian (Èçâ. ÐÀÍ. ÌÒÒ): | | 8044
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| In English (Mech. Solids): | | 4760 |
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| Yu.M. Zabolotnov, P.S. Voevodin, and Lu Hongshi, "A Two-Stage Method for the Formation of a Rotating Electrodynamic Space Tether System," Mech. Solids. 57 (3), 462-475 (2022) |
| Year |
2022 |
Volume |
57 |
Number |
3 |
Pages |
462-475 |
| DOI |
10.3103/S0025654422030232 |
| Title |
A Two-Stage Method for the Formation of a Rotating Electrodynamic Space Tether System |
| Author(s) |
Yu.M. Zabolotnov (Samara National Research University, Samara, 443086 Russia, yumz@yandex.ru)
P.S. Voevodin (Joint Stock Company Space Rocket Centre Progress, Samara, 443009 Russia, p.voevodin@inbox.ru)
Lu Hongshi (Samara National Research University, Samara, 443086 Russia, 292969972@qq.com) |
| Abstract |
The process of deployment and transfer to rotation with a given angular velocity of an electrodynamic space tether system in low Earth orbit is considered. The tether system is a linear grouping of three microsatellites connected by current-conducting insulated tethers. The process of forming a tether system is divided into two stages. At the first stage, there is no current in the tether and the relay law for the tension forces is used for the deployment of the system for a given length of the tether. At the second stage, with the help of current control, the system is transferred to a given final state of rotation with a constant angular velocity. To describe the motion of the centers of mass of microsatellites, the Lagrange equations are used. Under the condition of a slow change in tension forces, an analytical estimate was obtained for the characteristics of the angular motion of microsatellites relative to the direction of the tethers. The effectiveness of the considered approach to the formation of a rotating space tether system and the accuracy of analytical solutions are confirmed by numerical examples. |
| Keywords |
tether constellation of microsatellites, rotation, control, conductive tethers, movement of microsatellites around the center of mass |
| Received |
29 March 2021 | Revised |
15 April 2021 | Accepted |
13 May 2021 |
| Link to Fulltext |
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