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Electrodynamic forces in tethered satellite systems. I. System control

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2 Author(s)
E. Netzer ; RAFAEL, Haifa, Israel ; T. R. Kane

Part I of this work deals with the use of electrodynamic forces for control of tethered satellite system. A system formed by two massive end-bodies connected to each other by a current carrying tether is to be kept in an Earth-pointing orientation by means of joint actions of thrusters on one of the end-bodies and electrodynamic forces acting on the tether

Published in:

IEEE Transactions on Aerospace and Electronic Systems  (Volume:30 ,  Issue: 4 )