Optimizing Electrodynamic Tether System Performance
Author:
Affiliation:
1. Northrop Grumman Corporation
2. University of Michigan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6734
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3. Expansion and electron emission characteristics of a hollow‐cathode plasma contactor
4. Plasma turbulence enhanced current collection: Results from the plasma motor generator electrodynamic tether flight
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1. Chip-Scale Satellite Control with Multiple Electrodynamic Tethers;Journal of Guidance, Control, and Dynamics;2016-07
2. Attitude Control for Chip Satellites using Multiple Electrodynamic Tethers;AIAA/AAS Astrodynamics Specialist Conference;2012-08-13
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