Zobrazeno 1 - 7
of 7
pro vyhledávání: '"A. S. Chekashov"'
Publikováno v:
Advances in Space Research. 67:2577-2588
A torus-shaped sail consists of a reflective membrane attached to an inflatable torus-shaped rim. The sail’s deployment from its stowed configuration is initiated by introducing inflation pressure into the toroidal rim with an attached circular fla
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d175384013436dc0020a9dbf523db669
https://doi.org/10.1016/j.asr.2020.06.041
https://doi.org/10.1016/j.asr.2020.06.041
Autor:
A S Chekashov, A V Kramlikh
Publikováno v:
Journal of Physics: Conference Series. 1745:012071
Nanosatellites have serious limitations on the onboard energy. Therefore, it is necessary to find a method of constructing a nominal reorientation trajectory that will optimally use the resources available onboard. In this paper the process of constr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4523954f99be51db4f04c256a7e1b8d8
https://doi.org/10.1088/1742-6596/1745/1/012071
https://doi.org/10.1088/1742-6596/1745/1/012071
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 984:012029
This work aims to simulate the flight of a spacecraft with an electric propulsion system to the near-Earth asteroid 2011ES4. A control law was formed that ensures the minimum fuel consumption when the engine is running without shutdowns. The simulati
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::86323b0a41445a34a0ff9413a9cd0ea4
https://doi.org/10.1088/1757-899x/984/1/012029
https://doi.org/10.1088/1757-899x/984/1/012029
Publikováno v:
2018 IEEE 12th International Conference on Application of Information and Communication Technologies (AICT).
In operation, the solar sail is under influence of external forces, the most significant is the pressure of sunlight for motion. The influence of external forces causes vibrations of solar sail, which can affect flight of the spacecraft and lead to d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::26c60b322f3cd1362ab80466810d16f4
https://doi.org/10.1109/icaict.2018.8747162
https://doi.org/10.1109/icaict.2018.8747162
Publikováno v:
2017 8th International Conference on Recent Advances in Space Technologies (RAST).
The heliocentric motion of the solar sail spacecraft (SSS) is described in classical Keplerian elements. The solar sail with an ideal reflection coefficient is considered. The spacecraft performs a non-coplanar motion with the sun gravity and the lig
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::459170741ea6a69aa9d0fa6b3c4f8a88
https://doi.org/10.1109/rast.2017.8003002
https://doi.org/10.1109/rast.2017.8003002
Publikováno v:
Journal of Physics: Conference Series. 1096:012064
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6e6945d709244963070a209edf2667cd
https://doi.org/10.1088/1742-6596/1096/1/012064
https://doi.org/10.1088/1742-6596/1096/1/012064
Publikováno v:
Journal of Physics: Conference Series; Dec2018, Vol. 1096 Issue 1, p1-1, 1p