Modified Algorithm for Calculating the Parameters of Maneuvers of Coplanar Meeting of Spacecraft in a Near-Circular Orbit Using Low-Thrust Engines

Modified Algorithm for Calculating the Parameters of Maneuvers of Coplanar Meeting of Spacecraft in a Near-Circular Orbit Using Low-Thrust Engines

A modified algorithm is presented for solving the problem of spacecraft rendezvous in a near-circular orbit. The study considers the calculation of maneuver parameters executed on several turns using a low-thrust propulsion system. It is assumed that the active spacecraft performs maneuvers within a...

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Bibliographic Details
Main Authors: Andrey A. Baranov, Adilson P. Olivio
Format: Article
Language:English
Published: Peoples’ Friendship University of Russia (RUDN University) 2025-07-01
Series:RUDN Journal of Engineering Research
Subjects:
spacecraft rendezvous
near-circular orbit
velocity impulse
maneuver parameters
approximate mathematical models
low-thrust propulsion
Online Access:https://journals.rudn.ru/engineering-researches/article/viewFile/45007/25000
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