| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 711577 | IFAC-PapersOnLine | 2015 | 6 Pages |
Abstract
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.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
