Stabilizing the motion of a low-orbit electrodynamic tether system

DOI10.1134/S1064230719020175zbMath1432.93265OpenAlexW2949764638WikidataQ127772561 ScholiaQ127772561MaRDI QIDQ2290489

Yu. M. Zabolotnov, P. S. Voevodin

Publication date: 28 January 2020

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230719020175

zbMATH Keywords

stabilizationnanosatelliteslow-orbit electrodynamic tether system

Mathematics Subject Classification ID

Application models in control theory (93C95) Lyapunov and other classical stabilities (Lagrange, Poisson, (L^p, l^p), etc.) in control theory (93D05)

Related Items (2)

Method of forming a triangular rotating tethered constellation of spacecraft using electromagnetic forces ⋮ A two-stage method for the formation of a rotating electrodynamic space Tether system

Cites Work

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