Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Yuriy Zabolotnov"'
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2018, Vol. 90, Issue 8, pp. 1168-1179.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-02-2017-0067
Publikováno v:
In IFAC PapersOnLine 2016 49(17):272-277
Autor:
Yuriy Zabolotnov, Tatyana Ledkova
Publikováno v:
2020 International Conference on Information Technology and Nanotechnology (ITNT).
The space tethered system in a lunar orbit, consisting of a space station and two small spacecraft, is considered. It is assumed that the space tethered system is fully deployed and makes movements near the local vertical. The center of mass of the s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::db10228549ed9fbd40f7d2cc60b4fe98
https://doi.org/10.1109/itnt49337.2020.9253340
https://doi.org/10.1109/itnt49337.2020.9253340
Autor:
Yuriy Zabolotnov, Pavel Voevodin
Publikováno v:
2019 XXI International Conference Complex Systems: Control and Modeling Problems (CSCMP).
The problem of modeling the braking process of a nanosatellite using a current-conducting tether is considered. The task is related to the actual problem of removing nanosatellites from space that have exhausted their life without the use of jet engi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e3cb4363659ab8ee71a10e9a6f8a72b2
https://doi.org/10.1109/cscmp45713.2019.8976684
https://doi.org/10.1109/cscmp45713.2019.8976684
Publikováno v:
International Journal of Engineering Systems Modelling and Simulation. 11:176
Spinning electrodynamic tether systems are good platforms for payload transportation, but require orbit reboosts after one or several tossing manoeuvres. In this paper an impact analysis is proposed to predict the change of system orbits after payloa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::89a22fe5fdb9075abfe3f8c558046b82
https://doi.org/10.1504/ijesms.2020.10033464
https://doi.org/10.1504/ijesms.2020.10033464
Autor:
D. V. Elenev, Yuriy Zabolotnov
Publikováno v:
Collection of selected papers of the III International Conference on Information Technology and Nanotechnology.
Space tether system consists of two solid bodies connected by a tether. The deployment of this system is produced mainly by aerodynamic forces which act on the bodies. One of these bodies has higher ballistic coefficient thus acting as an aerodynamic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::18b3d0e8e742c81c7b656a252e97dd3d
https://doi.org/10.18287/1613-0073-2017-1904-85-88
https://doi.org/10.18287/1613-0073-2017-1904-85-88
Autor:
Yuriy Zabolotnov, Oleg Naumov
Publikováno v:
International Journal of Space Science and Engineering. 2:305
This paper studies analytical and numerical methods of the analysis of spatial motion concerning centre of mass of small space vehicles at deployment of space tether system. Deployment of space tether system is executed from the base space vehicle. T
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::027f63f92e8b1da30fe8d5b81897dc22
https://doi.org/10.1504/ijspacese.2014.066964
https://doi.org/10.1504/ijspacese.2014.066964
Publikováno v:
International Journal of Space Science and Engineering; 2016, Vol. 4 Issue: 2 p106-120, 15p