Libration Control of Tethered Satellites in Elliptical Orbits
Author:
Affiliation:
1. Royal Melboume Institute of Technology University, Melbourne, Victoria 3083, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.17499
Reference24 articles.
1. Advantages of tether release of satellites from elliptic orbits
2. Interplanetary Injection for MXER Tether Payloads
3. Dynamic Behavior of a Tethered System with Multiple Subsatellites in Elliptic Orbits
4. Line-of-sight pointing stability for "drifting" satellites
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