In this paper we consider a spacecraft with one main thruster for translational control and reaction wheels for full attitude control. This is an underactuated control problem, which in this paper is solved using backstepping in order to couple the position tracking problem with the attitude. Assuming that the thrust is non-zero the nonlinear tracking control law is shown to be uniformly globally exponentially stable, and simulations validate these results.
Underactuated translational control of a rigid spacecraft
2013-03-01
1608372 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Detumbling and Reorienting Underactuated Rigid Spacecraft
Online Contents | 1996
|Detumbling and Reorienting Underactuated Rigid Spacecraft
British Library Conference Proceedings | 1996
|Reduced-Effort Control Laws for Underactuated Rigid Spacecraft
British Library Conference Proceedings | 1997
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