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- W4238087605 abstract "The paper concerns Drag-Free and Attitude Control (DFAC) of the European satellite GOCE to be employed during scientific mission phase. DFAC has been designed and tested on the end-to-end GOCE simulator. The design has followed the Embedded Model Control methodology, where a spacecraft/environment discrete-time model (embedded model) becomes the real-time core of the DFAC and is interfaced to the plant via tunable command and measurement laws. Simulation results are presented." @default.
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- W4238087605 date "2006-10-04" @default.
- W4238087605 modified "2023-09-23" @default.
- W4238087605 title "Drag-Free and Attitude Control for the GOCE satellite" @default.
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- W4238087605 doi "https://doi.org/10.1109/cdc.2005.1582794" @default.
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