Stabilizing the Motion of a Low-Orbit Electrodynamic Tether System

This paper considers the motion of a low-orbit electrodynamic tether system designed to raise the orbit of a small spacecraft or nanosatellites. The system operates in the thrust generation mode. The orbit is raised by the Ampere force resulting from the interaction of the conducting tether with the...

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Veröffentlicht in:	Journal of computer & systems sciences international 2019-03, Vol.58 (2), p.270-285
Hauptverfasser:	Voevodin, P. S., Zabolotnov, Yu. M.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamic forces Control Control Systems of Moving Objects Dynamic programming Electrodynamic tethers Engineering Mechatronics Nanosatellites Robotics Spacecraft Stress concentration
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