Search by keyword: geostationary orbit | Engineering Journal: Science and Innovation

Search by keyword: "geostationary orbit"

Evaluation of the geostationary tow truck spacecraft design parameters

Published: 02.12.2024

Authors: Shcheglov G.A., Merkulova A.A.

Published in issue: #12(156)/2024

DOI: 10.18698/2308-6033-2024-12-2409

Category: Aviation and Rocket-Space Engineering | Chapter: Design, construction and production of aircraft

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

Analysis of the concept of a long-term orbital station for the of interorbital cargo traffic serving

Published: 27.03.2017

Authors: Sobolev I.A., Leonov V.V., Volkova T.V., Bechasnov P.M.

Published in issue: #4(64)/2017

DOI: 10.18698/2308-6033-2017-4-1609

Category: Power, Metallurgic and Chemical Engineering | Chapter: Hydraulic Machines and Hydropneumatic units

Calculation of illumination conditions during putting the spacecraft into geostationary orbit using low thrusters

Published: 28.11.2016

Authors: Kazakovtsev V.P., Koryanov V.V., Prosuntsov P.V., Toporkov A.G.

Published in issue: #12(60)/2016

DOI: 10.18698/2308-6033-2016-12-1568

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

Final ascent to the geostationary orbit with the electric propulsion engine

Published: 26.02.2016

Authors: Yakovlev A.V., Vnukov A.A., Balandina T.N.

Published in issue: #2(50)/2016

DOI: 10.18698/2308-6033-2016-2-1466

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