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...
Збережено в:
| Дата: | 2015 |
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| Автори та афіліації: |
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| Ключові слова: | keywords |
| Автор: | |
| Формат: | Стаття |
| Мова: | Українська |
| Опубліковано: |
Інститут математики НАН України
2015
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| Онлайн доступ: | 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 |
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Репозитарії
Transactions of Institute of Mathematics of NAS of Ukraine| Резюме: | 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 energy storage is evaluated. It is shown that the storage usage increasesthe effectiveness when the shadow phases of the trajectory exist. |
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