Drag-free control for fundamental physics missions

Details Drag-free control for fundamental physics missions Drag-free control for fundamental physics missions

Oct 2003

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2003adspr..32.1221d&link_type=abstract

Advances in Space Research, Volume 32, Issue 7, p. 1221-1226.

Physics

2

Scientific paper

The requirements for several quite different missions requiring drag-free control are presented. The various elements of a drag-free control system are discussed: proof mass design considerations; optical, capacitive and SQUID sensing of the displacements between the proof mass and the satellite; gas and electrical thrusters as actuators; and design considerations for drag-free control laws.

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