Electrodynamic Tethers Under Forced-Current Variations Part II: Flexible-Tether Estimation and Control
Author:
Affiliation:
1. Delft University of Technology, 2629 HS Delft, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.45733
Reference25 articles.
1. Electrodynamic tethers for spacecraft propulsion
2. Orbital Maneuvering with Electrodynamic Tethers
3. Simple Approach to Orbital Control Using Spinning Electrodynamic Tethers
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