Method of energy estimation of interorbital transfers for LEO spacecraft on-orbit servicing

The problem of planning the circumnavigation of space objects requiring servicing is considered. It is assumed that system of base stations for servicing the given array of the satellites on different LEO orbits has been deployed. For a fixed time it is needed to flyby each satellite which requires servicing. The servicing is conducted using the detachable orbital modules (OM) from the base stations (BS). Basing on the longitude of ascending node deviation portrait for all serviceable satellites and base stations it is defined which OM should transfer to the vicinity of which satellite in order to have the lowest Delta-V budget. © 2017 Univelt Inc. All rights reserved.

Authors
Baranov A.A. 1, 2 , Razoumny V.Yu. 1 , Razoumny Y.N. 1 , Malyshev V.V.3
Journal
Advances in the Astronautical Sciences
Publisher
Univelt Inc.
Language
English
Pages
701-709
Status
Published
Volume
161
Year
2017
Organizations
  • 1 Peoples' Friendship University of Russia (RUDN University), 6, Mikluho-Maklaya Str, Moscow, 117198, Russian Federation
  • 2 Keldysh Institute of Applied Mathematics of Russian Academy of Science, 4, Miusskaya Sqr, Moscow, 125047, Russian Federation
  • 3 Moscow Aviation Institute, 4, Volokalamskoe Ave, Moscow, 125993, Russian Federation
Keywords
Base stations; Budget control; Cobalt compounds; Dysprosium compounds; Satellites; Space flight; Ascending nodes; Delta-V; Energy estimation; Fixed time; On-orbit servicing; Orbital module; Space objects; Orbits
Date of creation
19.10.2018
Date of change
21.04.2021
Short link
https://repository.rudn.ru/en/records/article/record/6196/
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