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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Bibliographic Details
Date:	2015
Author Affiliations:	Я. В. Ткаченко
Keywords:	keywords
Main Author:	Ткаченко, Я. В.
Format:	Article
Language:	Ukrainian
Published:	Інститут математики НАН України 2015
Online Access:	https://trim.imath.kiev.ua/index.php/trim/article/view/38
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Journal Title:	Transactions of Institute of Mathematics of NAS of Ukraine
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Transactions of Institute of Mathematics of NAS of Ukraine

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