作者: Joseph A. Carroll , Eugene M. Levin
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摘要: A tether system for space applications includes at least one electron collector, emitter, a power system, and electrodynamic electrically coupled to the system. The conducts electrical current between collector emitter. Electric voltage are measured. Selected dynamics electrodynamics based on measured electric ascertained. and/or distribution is adjusted thereby control state ascertained selected electrodynamics.