Drag-free control for MiniSTEP

Details Drag-free control for MiniSTEP Drag-free control for MiniSTEP

Nov 1996

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1996cqgra..13a.179j&link_type=abstract

Classical and Quantum Gravity, Volume 13, Issue 11A, pp. A179-A184 (1996).

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 0264-9381/13/11A/025/img1 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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