Position and Attitude Control of Formation Flying Satellites for Restructuring Their Configurations by Electromagnetic Force at the Docking Phase
Author:
Affiliation:
1. Aoyamagakuin University
2. Japan Aerospace Exploration Agency (JAXA)
3. Waseda University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4540
Reference14 articles.
1. Result of Rendezvous Docking Experiment of ETS-VII.
2. Control of Electromagnetic Current at Final Docking Phase of Small Satellites
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