Zobrazeno 1 - 10
of 16
pro vyhledávání: '"S. O. Firsyuk"'
Publikováno v:
Космические аппараты и технологии, Vol 6, Iss 2, Pp 133-143 (2022)
The conceptual options for small spacecraft on the basis of a unified space platform are analyzed, the areas of rational use of the unified space platform as part of the small spacecraft for solving a wide range of tasks, including monitoring of the
Externí odkaz:
https://doaj.org/article/92614188962f4c0abd747b610dba7a1b
Publikováno v:
Доклады Академии наук. 488:377-382
The problem of modeling the attitude-control modes of small spacecraft with the use of electromagnetic systems, interacting with the Earths magnetic field is considered. A small spacecraft angular motion mathematical model is developed. A control law
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::36ccc0f6d0b201e14f14f9e1b854ba75
https://doi.org/10.31857/s0869-56524884377-382
https://doi.org/10.31857/s0869-56524884377-382
Publikováno v:
Doklady Physics. 64:389-393
The problem of modeling the attitude control modes of small spacecraft using electromagnetic systems interacting with the Earth’s magnetic field is considered. A mathematical model for the angular motion dynamics of small spacecraft has been develo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7c65b513df87ee793ed83d9f2f17cc91
https://doi.org/10.1134/s1028335819100021
https://doi.org/10.1134/s1028335819100021
Publikováno v:
Доклады Академии наук. 484:415-419
The problem of modeling the angular momentum control modes of small spacecraft using electromagnetic systems interacting with the Earth’s magnetic field is considered. The electromagnetic system control law has been constructed for various composit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b525c48ab90fdd77f2548128ee38fbaf
https://doi.org/10.31857/s0869-56524844415-419
https://doi.org/10.31857/s0869-56524844415-419
Publikováno v:
XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration.
The modes of braking control of small satellite (SS) cubesat type using inflatable aerodynamic decelerator (IAD) are discussed in the paper. The project-ballistic analysis is carried out to determine the trajectory parameters of the motion of SS usin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2b14cc04455e9a2418c9d7fb18a0308b
https://doi.org/10.1063/5.0035800
https://doi.org/10.1063/5.0035800
Publikováno v:
Solar System Research. 52:606-612
The article discusses proposals for creating a standard unit based on CubeSat technology, an independent autonomous aerobraking device based on inflatable balloons or a solar sail cone section. The proposed devices have a simple start-up system and a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::30a9370beeab4c21aa2c388391f29764
https://doi.org/10.1134/s003809461807016x
https://doi.org/10.1134/s003809461807016x
Publikováno v:
Doklady Physics. 62:543-546
The problem of spacecraft attitude control using electromagnetic systems interacting with the Earth’s magnetic field is considered. A set of dimensionless parameters has been formed to investigate the spacecraft orientation regimes based on dynamic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::baa93ad4d9d86efb3b711fab6ed487e3
https://doi.org/10.1134/s1028335817120011
https://doi.org/10.1134/s1028335817120011
Publikováno v:
XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9e23900a2b4dff3be131fb917680f349
https://doi.org/10.1063/1.5133196
https://doi.org/10.1063/1.5133196
Publikováno v:
Doklady Physics. 61:558-561
The problem of controlling the angular momentum of spacecraft using magnetic attitude control systems interacting with the Earth’s magnetic field is considered. A mathematical model for the angular motion dynamics of a spacecraft has been construct
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1061f200a46a88eb4270de04a09c087d
https://doi.org/10.1134/s1028335816110069
https://doi.org/10.1134/s1028335816110069
Publikováno v:
Contemporary Engineering Sciences. 9:1273-1281
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::20e30af5df2ec4491b676d49e4ae758d
https://doi.org/10.12988/ces.2016.67123
https://doi.org/10.12988/ces.2016.67123