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George Pescod

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Open access Oct 2026

GRACE Follow-On LRI measurements of linear accelerations produced by attitude control thrust firings

The attitude of the GRACE Follow-On satellites is controlled by six pairs of attitude control thrusters.  An ideal thruster system would produce a change only in angular momentum.  The imperfect system, however, also produces undesired linear accelerations that must be removed for orbit analysis and gravity recovery.  ...

Shin-Chan Han, George Pescod · 0 citations

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