The MiniSTEP drag-free control system

Physics

Scientific paper

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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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