Coplanar multi-turn rendezvous in near-circular orbit using a low-thrust engine

The authors describe an algorithm that allows calculating the parameters of maneuvers performed on several turns by the low-thrust engine, which ensure the flight of the active spacecraft to the specified vicinity of the target space object. The movement takes place in the vicinity of a circular orb...

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Bibliographic Details
Main Authors: Andrey A. Baranov, Adilson Pedro Olivio
Format: Article
Language:English
Published: Peoples’ Friendship University of Russia (RUDN University) 2022-12-01
Series:RUDN Journal of Engineering Research
Subjects:
Online Access:https://journals.rudn.ru/engineering-researches/article/viewFile/33690/21730