期刊
IFAC PAPERSONLINE
卷 48, 期 26, 页码 127-132出版社
ELSEVIER SCIENCE BV
DOI: 10.1016/j.ifacol.2015.11.125
关键词
Active vibration isolation; multi-harmonic microvibrations; LPV synthesis
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-infinity/LPV theroy is used to mitigate low frequency disturbances. The issue of multiple harmonic microvibrations is also investigated. The results are evaluated using H-infinity criteria and simulation results from a test benchmark provided by Airbus Defence and Space demonstrate the potential of the proposed method. (C) 2015, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.
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