This paper presents a LPV (Linear Parameter Varying) solution for the active part of a mixed passive-active control architecture to mitigate the microvibrations generated by reaction wheels in satellites. H ∞ /LPV theroy is used to mitigate low frequency disturbances. The issue of multiple harmonic microvibrations is also investigated. The results are evaluated using H ∞ criteria and simulation results from a test benchmark provided by Airbus Defence and Space demonstrate the potential of the proposed method.
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Preda et al. (2015) studied this question.
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