Three-dimensional deployment of electro-dynamic tether via tension and current control with constraints
Author:
Funder
National Natural Science Foundation of China
Foundation for the Author of National Excellent Doctoral Dissertation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference25 articles.
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3. Dynamics of nanosatellite deorbit by bare electrodynamic tether in low earth orbit;Zhong;J. Spacecr. Rockets,2013
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5. M.L. Cosmo, E.C. Lorenzini, Tethers in Space Handbook, 3rd ed., NASA, 1997.
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