Optimal flights with close circular orbits when accounting for the shadow
The problem of an optimal transfer of a space vehicle with the maximalpayload between nearby nonconplanar circular orbits in the spherical gravi-tation field is solved. The space vehicle is equipped with a constant powersolar electric propulsion and an energy storage. The payload increase due tothe...
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| Datum: | 2015 |
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| 1. Verfasser: | |
| Format: | Artikel |
| Sprache: | Ukrainisch |
| Veröffentlicht: |
Інститут математики НАН України
2015
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| Online Zugang: | https://trim.imath.kiev.ua/index.php/trim/article/view/38 |
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| Назва журналу: | Transactions of Institute of Mathematics of NAS of Ukraine |
| Завантажити файл: |  |