Analysis of the Dynamics and Choice of Parameters of an Electrodynamic Space Tether System in the Thrust Generation Mode-Reference-Cited by-同舟云学术

Analysis of the Dynamics and Choice of Parameters of an Electrodynamic Space Tether System in the Thrust Generation Mode

Published:2020-01 Issue:1 Volume:58 Page:42-52
ISSN:0010-9525
Container-title:Cosmic Research
language:en
Short-container-title:Cosmic Res

Author:

Voevodin P. S.,Zabolotnov Yu. M.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.1134/S0010952520010062.pdf

Reference20 articles.

1. Beletskii, V.V. and Levin, E.M., Dinamika kosmicheskikh trosovykh sistem (Dynamics of Space Tether Systems), Moscow: Nauka, 1990.

2. Levin, E.M., Dynamic Analysis of Space Tether Missions, San Diego: American Astronautical Society, 2007.

3. Zhong, R. and Zhu, Z.H., Dynamics of nanosatellite deorbit by bare electrodynamic tether in low earth orbit, J. Spacecr. Rockets, 2013, vol. 50, no. 3, pp. 691–700.

4. Chen, X. and Sanmartin, J.R., Bare-tether cathodic contact through thermionic emission by low-work-function materials, Phys. Plasmas, 2012, vol. 19, pp. 1–8.

5. Zhong, R. and Zhu, Z.H., Optimal control of nanosatellite fast deorbit using electrodynamic tether, J. Guid. Control. Dyn., 2014, vol. 37, no. 4, pp. 1182–1194.

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