Zobrazeno 1 - 10
of 20
pro vyhledávání: '"Dmitry Pritykin"'
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:
Aerospace, Vol 9, Iss 8, p 419 (2022)
The paper presents a feasibility study of satellite formation-flying missions for space advertising. To estimate a space advertising mission viability, the global population coverage model is designed and the demonstration schedule with a focus on la
Externí odkaz:
https://doaj.org/article/d501d7c76db244e4b33e0295a025e754
Autor:
Dmitry Pritykin
Publikováno v:
Автоматика и телемеханика. :3-38
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::79cd14e66fae5bdd2ffb11a77690d29d
https://doi.org/10.31857/s0005231021080018
https://doi.org/10.31857/s0005231021080018
Publikováno v:
Automation and Remote Control. 82:1293-1320
We survey the progress in data mining methods for spacecraft health monitoring. The main emphasis is placed on the analysis of telemetry data enabling the identification of spacecraft states that are atypical during normal operation and the predictio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fef9e965e2bc35c4a46781220b5466e5
https://doi.org/10.1134/s0005117921080014
https://doi.org/10.1134/s0005117921080014
Publikováno v:
Advances in Space Research. 67:3294-3307
This note presents a study of a four-satellite tetrahedral formation to collect, process, and exchange multipoint measurements of geomagnetic field in a near-polar orbit. The study is conducted as a series of numerical experiments based on simulated
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::33d58d9f4722d0f0ed3facf2e6545af9
https://doi.org/10.1016/j.asr.2021.02.012
https://doi.org/10.1016/j.asr.2021.02.012
Publikováno v:
Journal of Guidance, Control, and Dynamics. 44:548-558
This paper addresses the attitude control of nano-spacecraft with three reaction wheels and three magnetorquers in low Earth orbits, and develops algorithms to maintain control when any one of the reaction wheels completely fails. In the event of a r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::080fd96bcfd04dfb351d099df70ca3ac
https://doi.org/10.2514/1.g005525
https://doi.org/10.2514/1.g005525
Publikováno v:
Aerospace; Volume 9; Issue 8; Pages: 419
The paper presents a feasibility study of satellite formation-flying missions for space advertising. To estimate a space advertising mission viability, the global population coverage model is designed and the demonstration schedule with a focus on la
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7fa680346ead470dc9441738e87eabf2
https://doi.org/10.3390/aerospace9080419
https://doi.org/10.3390/aerospace9080419
Autor:
Basel Omran, Dmitry Pritykin
Publikováno v:
International Conference of Control, Dynamic Systems, and Robotics.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b2b3ddce080ca068b8f65fc58be8feba
https://doi.org/10.11159/cdsr21.111
https://doi.org/10.11159/cdsr21.111
Publikováno v:
International Conference of Control, Dynamic Systems, and Robotics.
The paper delineates the magnetic controller gains tuning procedure for an active magnetic attitude control system of a CubeSat in the ISS orbit. The optimization is conducted for arbitrary required attitude given in the orbital reference frame of th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::82e331e070f700fff066c81b59e1390c
https://doi.org/10.11159/cdsr21.110
https://doi.org/10.11159/cdsr21.110
Publikováno v:
XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration.
An attitude determination and control system (ADCS) model is presented, which is used for CubeSat preliminary design stages in accordance with the European Space Agency (ESA) concurrent design approach. The model is implemented in Matlab/Simulink and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a06ed15d654082aa8e11f6f10d972a70
https://doi.org/10.1063/1.5133295
https://doi.org/10.1063/1.5133295