Electrodynamics Tether System Design Parameter Analyze and Orbit Motion Control Modes Investigation

2011, vol. 18, no. 2, pp. 41-46

Spacecraft and Rockets

Аuthors

Kul'kov V. M.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

e-mail: vmk_1@mail.ru

Abstract

Low-orbit satellite with electrodynamics tether system (EDTS) motion control methods are presented. Efficiency EDTS using satellite maneuvering analyze is described.

Keywords:

satellite, electrodynamics tether system, maneuvering

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