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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Published in | IFAC Proceedings Volumes Vol. 31; no. 17; pp. 687 - 692 |
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Main Authors | , |
Format | Journal Article |
Language | English |
Published |
01.07.1998
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Subjects | |
Online Access | Get full text |
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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. |
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ISSN: | 1474-6670 |
DOI: | 10.1016/S1474-6670(17)40417-4 |