Robust Stabilization of the Angular Velocity for an Underactuated Rigid Spacecraft

We consider the asymptotic stabilization of the angular velocity for a rigid spacecraft with two control torques. While this is a classical problem in the nonlinear control literature, the issue of robust performance in the presence of perturbations has received less attention. In this paper, we int...

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Bibliographic Details
Published inIFAC Proceedings Volumes Vol. 31; no. 17; pp. 687 - 692
Main Authors Lucibello, Pasquale, Oriolo, Giuseppe
Format Journal Article
LanguageEnglish
Published 01.07.1998
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Summary:We consider the asymptotic stabilization of the angular velocity for a rigid spacecraft with two control torques. While this is a classical problem in the nonlinear control literature, the issue of robust performance in the presence of perturbations has received less attention. In this paper, we introduce a new feedback control strategy, based on the recently proposed iterative steering approach. The resulting controller is very simple and prescribes the repeated application of a finite-time steering control designed for the nominal system. Robustness with respect to errors on inertia moments and actuator misalignments is proven theoretically and shown by simulation.
ISSN:1474-6670
DOI:10.1016/S1474-6670(17)40417-4