On equilibrium positions and stabilization of electrodynamic tether system in the orbital frame-Reference-Cited by-同舟云学术

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

Published:2018 Issue: Volume: Page:
ISSN:0094-243X
Container-title:AIP Conference Proceedings
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Author:

Tikhonov A. A.,Shcherbakova L. F.

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Link

http://aip.scitation.org/doi/pdf/10.1063/1.5034626

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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