Artificial Equilibrium Points for Electric Sail with Constant Attitude
Author:
Affiliation:
1. Department of Civil and Industrial Engineering, University of Pisa, I-56122 Pisa, Italy
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.A32540
Reference8 articles.
1. Survey of Highly Non-Keplerian Orbits with Low-Thrust Propulsion
2. Artificial equilibrium points for a generalized sail in the elliptic restricted three-body problem
3. Simulation study of solar wind push on a charged wire: basis of solar wind electric sail propulsion
4. Solar Sail Equilibria in the Elliptical Restricted Three-Body Problem
5. SzebehelyV., Theory of Orbits: The Restricted Problem of Three Bodies, Academic Press, New York, 1967, pp. 587–602.
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