Generating Solar Sail Trajectories in the Earth-Moon System Using Augmented Finite-Difference Methods
Using a solar sail, a spacecraft orbit can be offset from a central body such that the orbital plane is displaced from the gravitational center. Such a trajectory might be desirable for a single-spacecraft relay to support communications with an outpost at the lunar south pole. Although trajectory d...
Uloženo v:
| Hlavní autoři: | , |
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| Médium: | Artigo |
| Jazyk: | Inglês |
| Vydáno: |
Wiley
2011-01-01
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| Edice: | International Journal of Aerospace Engineering |
| On-line přístup: | http://dx.doi.org/10.1155/2011/476197 |
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