Electromagnetodynamic tether system in low-orbit satellite motion control tasks

Аuthors

Malyshev G. V., Kul'kov V. M.^*, Yegorov Y. G., Sharifullin R. R.

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 electromagnetodynamic tether system (EDTS) motion control methods are presented. Efficiency EDTS using for low-orbit satellite maneuvering analyze is described.

Keywords:

satellite, electromagnetodynamic tether system, maneuvering