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Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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Investigating the optimal three-impulse transfer into the high orbit of the artificial lunar satellite

Published: 03.07.2017

Authors: Gordienko E.S.

Published in issue: #9(69)/2017

DOI: 10.18698/2308-6033-2017-9-1667

Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control

    spacecraft, trajectory optimization, artificial lunar satellite, three-impulse bi-elliptic scheme, "Sternfeld" transfer, Powell’s quasi-Newton method
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