Part I 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. In Part II, electrodynamic forces are used for orbit transfer.
Electrodynamic forces in tethered satellite systems. Part I: System control
Elektrodynamische Kräfte in Satellitensystemen: Teil I: Systemsteuerung
IEEE Transactions on Aerospace and Electronic Systems ; 30 , 4 ; 1031-1038
1994
8 Seiten, 7 Bilder, 10 Quellen
Article (Journal)
English
Bewegungsanalyse , Satellit , Satellitenbahn , Umlaufbahn (Orbit) , Vektor , automatische Steuerung , magnetisches Feld , Modellsimulation , Stromversorgung , Masse (physikalische Größe) , Bewegungsgleichung , Mechanik , Erdmagnetismus , Feldverteilung , Eigenwert , Koordinatensystem , Matrizenrechnung
Electrodynamic Forces in Tethered Satellite Systems: Part I System Control
Online Contents | 1994
|Electrodynamic Forces in Tethered Satellite Systems: Part II Orbit Transfer
Online Contents | 1994
Uses of electrodynamic forces in tethered satellite systems. Part II: Orbit transfer
Tema Archive | 1994
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