Dynamic behavior of electrodynamic tether deorbit system on elliptical orbit and its control by Lorentz force

DOI10.1016/J.AST.2004.09.005zbMath1195.70043OpenAlexW2068433857MaRDI QIDQ4929457

Tomoko Kishimoto, Eiji Hiragi, Yoshiki Yamaigiwa

Publication date: 23 September 2010

Published in: Aerospace Science and Technology (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ast.2004.09.005

zbMATH Keywords

tetherelectrodynamicdebrisdeorbitspace system

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Technical applications of optics and electromagnetic theory (78A55) Orbital mechanics (70M20)

Related Items (3)

A control method for angular stabilization of an electrodynamic tether system ⋮ Advances in dynamics and control of tethered satellite systems ⋮ The effect of the nonuniformity of the Earth's magnetic field on electrodynamic space tether system dynamics

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