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.<>
Electrodynamic forces in tethered satellite systems. I. System control
IEEE Transactions on Aerospace and Electronic Systems ; 30 , 4 ; 1031-1038
1994-10-01
610995 byte
Article (Journal)
Electronic Resource
English
Electrodynamic Forces in Tethered Satellite Systems: Part I System Control
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