On equilibrium positions and stabilization of electrodynamic tether system in the orbital frame

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Tikhonov A. A.,Shcherbakova L. F.

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Reference28 articles.

1. V. V. Beletsky and E. M. Levin, Dynamics of Space Tether Systems – Advances in the Astronautical Sciences, Vol. 83 (American Astronautical Society, San Diego, California, 1993).

2. R.L. Forward, “Electrodynamic drag terminator tether, Appendix K of high strength-to-weight tapered Hoytether for LEO to GEO payload transport,” Final Report on NASA SBIR Phase I Contract NAS8-40690 (NASA, 1996).

3. R.L. Forward, R.P. Hoyt, and C. Uphoff, “Application of the Terminator TetherTM electrodynamic drag technology to the deorbit of constellation spacecraft,” in Paper AIAA 98-3491, 34th Joint Propulsion Conference and Exhibition (1998).

4. Terminator Tether: A Spacecraft Deorbit Device

5. M.L. Cosmo and E.C. Lorenzini, eds., Tethers in Space Handbook, 3rd ed. (Smithsonian Astrophysical Observatory, Cambridge, MA, USA, 1997).

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1. The Effect of the Nonuniformity of the Earth’s Magnetic Field on Electrodynamic Space Tether System Dynamics;Vestnik St. Petersburg University, Mathematics;2020-07

2. On damping of the oscillations of electrodynamic tether system;XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration;2019

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