Trajectories Derived from Periodic Orbits around the Lagrangian Point L<sub>1</sub> and Lunar Swing-Bys: Application in Transfers to Near-Earth Asteroids

Авторы

Ribeiro R.S.¹ , De Melo C.F.² , Prado A.F.B.A. ^3, ⁴

Журнал

Symmetry

Издательство

MDPI AG

Номер выпуска

Язык

Английский

Статус

Опубликовано

Том

Год

2022

Организации

¹ Space Mechanics and Control Division (CMC)|National Institute for Space Research|INPE
² Department of Mechanical Engineering (DEMEC)|Federal University of Minas Gerais|UFMG
³ Graduate Division (DIPGR)|National Institute for Space Research|INPE
⁴ Academy of Engineering|Peoples’ Friendship University of Russia (RUDN University)

Дата создания

28.12.2023

Дата изменения

28.12.2023

Постоянная ссылка

https://repository.rudn.ru/ru/records/article/record/95101/

Статья

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Data. Том 7. 2022. 75 с.

Статья

Jamil F., Ahmad S., Whangbo T.K., Muthanna A., Kim D.H.

Computers & Industrial Engineering. Elsevier Science Publishing Company, Inc.. Том 170. 2022. 108327 с.

Trajectories Derived from Periodic Orbits around the Lagrangian Point L1 and Lunar Swing-Bys: Application in Transfers to Near-Earth Asteroids