On Stabilization of Bounded Trajectories of a Spacecraft with a Solar Sail near an Unstable Libration Point
Author:
Affiliation:
1. Moscow Aviation Institute (National Research University),Department of Mechatronics and Theoretical Mechanics,Moscow,Russia
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9807427/9807457/09807606.pdf?arnumber=9807606
Reference4 articles.
1. Generalized restricted circular three-body problem as a model for dynamics of binary asteroids
2. Solar Sails as a Tool for Spacecrafi Motion Control Near Solar-Terrestrial Libration Points;eismont;l8th International Symposium on Space Flight Dynamics Munich ESA-SP 548,2004
3. Controlled Motion of a Solar Sail in the Vicinity of a Collinear Libration Point
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