anti-unwinding attitude control with fixed-time convergence for a flexible spacecraft

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ID: 190942
2017
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Ranked #38 of 48 articles by views in shanghai kou qiang yi xue = shanghai journal of stomatology

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Abstract
This paper investigates the fixed-time attitude tracking control problem for flexible spacecraft with unknown bounded disturbances. First, with the knowledge of norm upper bounds of external disturbances and the coupling effect of flexible modes, a novel robust fixed-time controller is designed to deal with this problem. Second, the controller is further enhanced by an adaptive law to avoid the knowledge of norm upper bounds of external disturbances and coupling effect of flexible modes. This control law guarantees the convergence of attitude tracking errors in fixed time where the settling time is bounded by a constant independent of initial conditions. Moreover, the proposed controllers can prevent the unwinding phenomenon. Simulation results are presented to demonstrate the performance of the proposed control scheme.
Reference Key
pukdeboon2017internationalanti-unwinding Use this key to autocite in the manuscript while using SciMatic Manuscript Manager or Thesis Manager
Authors ;Chutiphon Pukdeboon;Anuchit Jitpattanakul
Journal shanghai kou qiang yi xue = shanghai journal of stomatology
Year 2017
DOI
10.1155/2017/5018323
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