AbstractDynamics and control of two-body and -body tethered satellites are considered. At first, nonlinear roll and pitch motions of two-body systems are examined. Then the effects of aerodynamic and electrodynamic forces on the stability of a tethered satellite are discussed. Various control schemes to stabilize the dynamics during retrieval of the subsatellite are described. Finally, some dynamics and stability results for -body tethered satellites are presented.
Dynamics and control of tethered satellite systems
Acta Astronautica ; 63 , 11-12 ; 1169-1177
2008-06-25
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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