Zobrazeno 1 - 10
of 68
pro vyhledávání: '"Ye.I. Somov"'
Publikováno v:
Izvestiya of Samara Scientific Center of the Russian Academy of Sciences. 23:75-83
The problems of additional launching a space robot into a geostationary orbit and approaching a geostationary satellite for its maintenance are considered. The robot's attitude and orbit control system uses an electric propulsion unit, a propulsion s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8c8588eb8681231363228b6bd67d8582
https://doi.org/10.37313/1990-5378-2021-23-2-75-83
https://doi.org/10.37313/1990-5378-2021-23-2-75-83
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
Publikováno v:
IFAC-PapersOnLine. 52:538-543
Methods for spatial guidance and control of a space robot-manipulator at approach and capturing a non-cooperative satellite in conditions of uncertainty and incompleteness of measurements are considered. An operational strategy to estimate the resour
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f2c7ad03778b18fe041e736cdecb6d54
https://doi.org/10.1016/j.ifacol.2019.11.299
https://doi.org/10.1016/j.ifacol.2019.11.299
Publikováno v:
IFAC-PapersOnLine. 52:188-193
We consider problems on passive fault-tolerant control of a satellite during its inter-orbital flight and the transition of a vehicle from the trajectory of its passive motion into a circular orbit at failures of the working jet engines. We present t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8d223cf0dca74ed5ef761f40f6017699
https://doi.org/10.1016/j.ifacol.2019.11.198
https://doi.org/10.1016/j.ifacol.2019.11.198
Publikováno v:
IFAC-PapersOnLine. 52:182-187
The methods for modeling and detection of anomalous in the automatic control systems, and also practical methods for active analysis of anomalous situations, are presented. We develop algorithms for consecutive classification of onboard equipment fai
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::da95d74df263ddcbddebe06d56ff6c7d
https://doi.org/10.1016/j.ifacol.2019.11.197
https://doi.org/10.1016/j.ifacol.2019.11.197
Publikováno v:
IFAC-PapersOnLine. 52:544-548
Problems of nonlinear digital and pulse-width control for the spacecraft orientation in initial modes are considered – during their separation from a launcher rocket up to regular attitude stabilization in orbital reference frame. Developed methods
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::82fe755928031bf5b833d5c2f3e5c039
https://doi.org/10.1016/j.ifacol.2019.11.300
https://doi.org/10.1016/j.ifacol.2019.11.300
Publikováno v:
IFAC-PapersOnLine. 51:72-76
Methods for guidance and control of a space robot-manipulator at its approach to a non-cooperative space vehicle on a sun-synchronous orbit in conditions of uncertainty and incompleteness of measurements are considered. An operational strategy to est
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d0e654e28ffbd3d1e262732fb825e63a
https://doi.org/10.1016/j.ifacol.2018.11.251
https://doi.org/10.1016/j.ifacol.2018.11.251
Publikováno v:
IFAC-PapersOnLine. 51:66-71
Contemporary land-survey satellites are placed in the orbits with altitude from of 600 up to of 1000 km. For such spacecraft at a final stage of its manufacturing we present developed methods for in-flight identification and verification of its attit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dba7835551d25ff092375de9e766b8bc
https://doi.org/10.1016/j.ifacol.2018.11.247
https://doi.org/10.1016/j.ifacol.2018.11.247