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- W2091925892 abstract "A simple guidance equation for spinning electrodynamic tethers that can be used to provide approximate closed-loop guidance for orbital transfers was studied. A spinning tether system can utilize the electrodynamic Lorentz forces more effectively for maneuvers that require out-of-plane thrust forces. The added stability created by the centrifugal stiffening from the rotation of a flexible tether system makes spinning an atrractive method for enhancing electrodynamic tether system. The result showed that the efficiency of the hanging tether was slightly superior to a spinning tether for changing the semimajor axis." @default.
- W2091925892 created "2016-06-24" @default.
- W2091925892 date "2006-01-01" @default.
- W2091925892 modified "2023-09-23" @default.
- W2091925892 title "Simple Approach to Orbital Control Using Spinning Electrodynamic Tethers" @default.
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- W2091925892 doi "https://doi.org/10.2514/1.16608" @default.
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