Zobrazeno 1 - 9
of 9
pro vyhledávání: '"T.Ye. Somova"'
Autor:
S.Ye. Somov, T.Ye. Somova
Publikováno v:
Izvestiya of Samara Scientific Center of the Russian Academy of Sciences. 23:66-74
A method for ensuring the survivability of the spacecraft attitude control system with a minimally redundant cluster of flywheels by General Electric scheme and a magnetic drive in the event of the flywheels' failures is presented. The results of com
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4209d8ead5dca1b29ca537a1575e9e52
https://doi.org/10.37313/1990-5378-2021-23-2-66-74
https://doi.org/10.37313/1990-5378-2021-23-2-66-74
Publikováno v:
Izvestiya of Samara Scientific Center of the Russian Academy of Sciences. 23:84-90
A comparative analysis of the dynamic properties clusters of flywheels and gyrodines for a space robot attitude control when it is addition launching into geostationary orbit and approaches a geostationary satellite for its maintenance is carried out
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f72c0b645df554910d0c4758b5bc386d
https://doi.org/10.37313/1990-5378-2021-23-2-84-90
https://doi.org/10.37313/1990-5378-2021-23-2-84-90
Publikováno v:
Izvestiya of Samara Scientific Center of the Russian Academy of Sciences. 22:132-137
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c968cdc84c15998c0f80a8f6781aadeb
https://doi.org/10.37313/1990-5378-2020-22-2-132-137
https://doi.org/10.37313/1990-5378-2020-22-2-132-137
Publikováno v:
Izvestiya of Samara Scientific Center of the Russian Academy of Sciences. 22:124-131
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f34684d71b19706f80536add37ec07cb
https://doi.org/10.37313/1990-5378-2020-22-2-124-131
https://doi.org/10.37313/1990-5378-2020-22-2-124-131
Autor:
T.Ye. Somova
Publikováno v:
2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS).
The paper presents the algorithms for economical digital attitude control of an information satellite at initial modes: from the time it separates from a launcher rocket up to its regular attitude stabilization in the orbital reference frame. The com
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::34f66520378ad8b6733a9c709f52abeb
https://doi.org/10.23919/icins.2018.8405936
https://doi.org/10.23919/icins.2018.8405936
Autor:
T.Ye. Somova
Publikováno v:
2017 24th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS).
We consider problems of synthesis of the vector spline guidance laws and digital attitude control of a maneuvering land-survey satellite. We have presented the results on the efficiency of the developed algorithms.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::19434a27e8f424e633d6792acbe87add
https://doi.org/10.23919/icins.2017.7995680
https://doi.org/10.23919/icins.2017.7995680
Publikováno v:
IFAC Proceedings Volumes. 46:25-30
Obtained in the space photos a ground resolution depends on a spacecraft spatial angular motion during optoelectronic survey. The paper studies case of optimal equalization of an image longitudinal velocity in the focal plane of telescope and tackles
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2e23a29ae996eac3df98be7381ac3f02
https://doi.org/10.3182/20130902-5-de-2040.00013
https://doi.org/10.3182/20130902-5-de-2040.00013
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Conference
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