Engineering Journal: Science and InnovationELECTRONIC SCIENCE AND ENGINEERING PUBLICATION
Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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Search by keyword: "geostationary orbit"


Aspects of applying combined mass–time functional in solving the problem of optimizing the multiple-burn transfer of a spacecraft into a high-energy orbit

Published: 21.03.2022

Authors: Kiriliuk E.V., Stepanov M.N.

Published in issue: #3(123)/2022

DOI: 10.18698/2308-6033-2022-3-2164

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

End-to-end optimization of a payload transfers into the geostationary orbit using the combination of the upper stage energy capabilities and the spacecraft own propulsion system

Published: 22.02.2022

Authors: Kiriliuk E.V.

Published in issue: #2(122)/2022

DOI: 10.18698/2308-6033-2022-2-2155

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

Features of the orbital motion control of geostationary satellites in the conditions of their collocation

Published: 15.03.2019

Authors: Sukhoy Yu.G., Braginets V.F., Mescheryakov V.M.

Published in issue: #3(87)/2019

DOI: 10.18698/2308-6033-2019-3-1860

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

Features of the orbital motion control of geostationary satellites in the conditions of their collocation

Published: 15.03.2019

Authors: Sukhoy Yu.G., Braginets V.F., Mescheryakov V.M.

Published in issue: #3(87)/2019

DOI: 10.18698/2308-6033-2019-3-1860

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

The strategy for correcting the geostationary satellite orbit inclination, taking into account the long term inclination evolution under the gravitational potentials of the Sun and the Moon

Published: 27.06.2018

Authors: Sukhoy Yu.G., Braginets V.F.

Published in issue: #7(79)/2018

DOI: 10.18698/2308-6033-2018-7-1783

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

The strategy for correcting the geostationary satellite orbit inclination, taking into account the long term inclination evolution under the gravitational potentials of the Sun and the Moon

Published: 27.06.2018

Authors: Sukhoy Yu.G., Braginets V.F.

Published in issue: #7(79)/2018

DOI: 10.18698/2308-6033-2018-7-1783

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