Physics
Scientific paper
Oct 2003
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2003adspr..32.1383j&link_type=abstract
Advances in Space Research, Volume 32, Issue 7, p. 1383-1386.
Physics
Scientific paper
The MiniSTEP drag-free control system must reduce the atmospheric drag forces acting on the spacecraft by seven orders of magnitude, to yield an average residual acceleration of less than 3.10-14 m s-2 averaged over the measurement bandwidth. The origins of the drag-free requirements are discussed, and a control system is presented which meets the requirements under realistic assumptions for noise levels.
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