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- W2005498462 abstract "New approach for modelling a physical hysteresis damping the flexible spacecraft structure oscillations, is developed. New results on communication satellite attitude guidance and digital robust control with precise pointing the large-scale flexible antennas, are presented." @default.
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- W2005498462 date "2010-01-01" @default.
- W2005498462 modified "2023-10-16" @default.
- W2005498462 title "Robust Attitude Control of a Communication Satellite with Large-scale Flexible Antennas" @default.
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- W2005498462 doi "https://doi.org/10.3182/20100906-5-jp-2022.00050" @default.
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