Attitude Control and Stabilization of Spacecraft with a Captured Asteroid
Author:
Affiliation:
1. University of Illinois, Urbana-Champaign
2. Jet Propulsion Laboratory, California Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0596
Reference60 articles.
1. System design of the Hayabusa 2—Asteroid sample return mission to 1999 JU3
2. The European Union funded NEOShield project: A global approach to near-Earth object impact threat mitigation
3. The Rosetta Mission: Flying Towards the Origin of the Solar System
4. Asteroid Return Mission Feasibility Study
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