Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Uliana Monakhova"'
Publikováno v:
Aerospace, Vol 11, Iss 8, p 635 (2024)
A servicing spacecraft motion control approach for the problem of on-orbit truss structure assembly is developed in this paper. It is considered that a cargo container with a rod set and servicing spacecraft are in orbit initially. The assembly proce
Externí odkaz:
https://doaj.org/article/77d262ac94834485ab568e3f2e0198cb
Publikováno v:
Aerospace, Vol 10, Iss 12, p 975 (2023)
In this article, five feedback magnetic attitude control algorithms are compared in terms of stabilization accuracy and implementation problems. The control strategies are classic Lyapunov control with scalar gain; the same control strategy with matr
Externí odkaz:
https://doaj.org/article/42a7fba9ae364b0da829c33920d6ac46
Decentralized Differential Aerodynamic Control of Microsatellites Formation with Sunlight Reflectors
Autor:
Kirill Chernov, Uliana Monakhova, Yaroslav Mashtakov, Shamil Biktimirov, Dmitry Pritykin, Danil Ivanov
Publikováno v:
Aerospace, Vol 10, Iss 10, p 840 (2023)
The paper presents a study of decentralized control for a satellite formation flying mission that uses differential lift and drag to enforce the relative positioning requirements. All spacecraft are equipped with large sunlight reflectors so that, gi
Externí odkaz:
https://doaj.org/article/7871601734374ca0b353c49ecd20c817
Publikováno v:
Acta Astronautica. 199:471-479
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::610f7363ae627c45b84a5cb771ba546f
https://doi.org/10.1016/j.actaastro.2022.07.045
https://doi.org/10.1016/j.actaastro.2022.07.045
Publikováno v:
Aerospace, Vol 8, Iss 8, p 199 (2021)
A decentralized control algorithm for the construction of a tetrahedral configuration using differential lift and drag forces is proposed in this paper. Four 3U CubeSats launched in LEO are considered. Satellite attitude-controlled motion relative to
Externí odkaz:
https://doaj.org/article/f91e35e12c4045c68129b16631702ff7
Publikováno v:
Acta Astronautica. 192:15-29
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::24e820b2e4e510c5d52860c425e867eb
https://doi.org/10.1016/j.actaastro.2021.12.014
https://doi.org/10.1016/j.actaastro.2021.12.014
Autor:
Anna D. Guerman, Danil Ivanov, Uliana Monakhova, Mikhail Ovchinnikov, Dmitry Sergeevich Roldugin
Publikováno v:
Advances in Space Research. 67:3489-3503
Nanosatellites in the swarm initially move along arbitrary unbounded relative trajectories according to the launch initial conditions. Control algorithms developed in the paper are aimed to achieve the required spatial distribution of satellites in t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7b5983a8f761eedcfc739a31e4411b0f
https://doi.org/10.1016/j.asr.2020.05.024
https://doi.org/10.1016/j.asr.2020.05.024
Publikováno v:
Aerospace
Volume 8
Issue 8
Aerospace, Vol 8, Iss 199, p 199 (2021)
Volume 8
Issue 8
Aerospace, Vol 8, Iss 199, p 199 (2021)
A decentralized control algorithm for the construction of a tetrahedral configuration using differential lift and drag forces is proposed in this paper. Four 3U CubeSats launched in LEO are considered. Satellite attitude-controlled motion relative to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::70a027eace942f84da3332c1b7637ee6
Publikováno v:
Acta Astronautica. 159:646-657
The paper is devoted to the problem of nanosatellites swarm deployment immediately after their separation from the launcher. Some error in the ejection velocity during the launch is inevitable. It leads to a slightly different orbital period of the s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9e3db289761985ac95588580ac0a2dc4
https://doi.org/10.1016/j.actaastro.2019.02.006
https://doi.org/10.1016/j.actaastro.2019.02.006
Autor:
Yaroslav Vladimirovich Mashtakov, Alexey Shestoperov, Anna Sergeevna Okhitina, Uliana Monakhova, Danil Ivanov, Stepan Sergeevich Tkachev
Publikováno v:
XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration.
Algorithms for small satellite’s attitude determination and control system are studied. ADCS consists of sun sensor, angular velocity sensor, magnetometer, reaction wheels and magnetorquers. In order to determine current satellite attitude and angu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e6654a46cd2dbb3cfc2ba8d508468437
https://doi.org/10.1063/5.0035725
https://doi.org/10.1063/5.0035725