Solar Sail Body-Fixed Hovering over Elongated Asteroids
Author:
Affiliation:
1. Beijing Institute of Technology, 100081 Beijing, People’s Republic of China
2. Tsinghua University, 100084 Beijing, People’s Republic of China
3. Texas A&M University, College Station, Texas 77840
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.G001061
Reference29 articles.
1. The Actual Dynamical Environment About Itokawa
2. Satellite Dynamics about Small Bodies: Averaged Solar Radiation Pressure Effects
3. Control of Hovering Spacecraft Using Altimetry
4. Control of Hovering Spacecraft Near Small Bodies: Application to Asteroid 25143 Itokawa
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