Zobrazeno 1 - 10
of 46
pro vyhledávání: '"Tatyana Somova"'
Autor:
Sergey Somov, Tatyana Somova
Publikováno v:
Havacılık ve Uzay Teknolojileri Dergisi, Vol 14, Iss 1, Pp 89-98 (2021)
A method for ensuring the survivability of a spacecraft attitude control system with minimally redundant cluster of the flywheels and magnetic actuator at the faults of any reaction wheels are presented. The results of computer simulation were obt
Externí odkaz:
https://doaj.org/article/cc7fd16010bc40a6bf8fa163e5681c24
Autor:
Tatyana Somova
Publikováno v:
Havacılık ve Uzay Teknolojileri Dergisi, Vol 9, Iss 2, Pp 35-45 (2016)
We present simple methods for attitude guidance and control of the land-survey mini-satellites, algorithms and software for simulation and animation of their spatial orbital motion.
Externí odkaz:
https://doaj.org/article/83fae58c4a8b4914915ea92f7a67fbdc
Publikováno v:
Cybernetics and Physics. :157-164
An image velocity stabilization system built into a space telescope for scanning optoelectronic observation of terrestrial targets with a physical hysteresis of a piezoceramic drive is considered. Elaborated algorithms for discrete filtering, results
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::64e00e070b1bc41ca9f7bf7184b0f748
https://doi.org/10.35470/2226-4116-2022-11-3-157-164
https://doi.org/10.35470/2226-4116-2022-11-3-157-164
Publikováno v:
Cybernetics and Physics. :30-36
The problems of approaching a space robot to a geostationary satellite and visual checking its technical state are considered. The robot’s control system uses both plasma and catalytic electric propulsion units as well as a cluster of four control
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7ef4b49b19a3a26ec99a32403548b713
https://doi.org/10.35470/2226-4116-2022-11-1-30-36
https://doi.org/10.35470/2226-4116-2022-11-1-30-36
Publikováno v:
IEEE Journal on Miniaturization for Air and Space Systems. 2:51-58
The problems of autonomous digital control of a spacecraft (SC) orientation and checking the operability of its attitude control system (ACS) in the initial orientation modes are considered. The developed methods, algorithms, and simulation results f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4eb594bbf90281be792d617e75e8b6c8
https://doi.org/10.1109/jmass.2020.3036484
https://doi.org/10.1109/jmass.2020.3036484
Publikováno v:
2022 IEEE 9th International Workshop on Metrology for AeroSpace (MetroAeroSpace).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6e3a65f859dffea202009b3e53545e36
https://doi.org/10.1109/metroaerospace54187.2022.9856212
https://doi.org/10.1109/metroaerospace54187.2022.9856212
Publikováno v:
2022 16th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ada493dc6ed3b029d5ccf895cde3f4c0
https://doi.org/10.1109/stab54858.2022.9807557
https://doi.org/10.1109/stab54858.2022.9807557
Publikováno v:
2022 29th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::36cc43f5af456115d6a3d50a02081974
https://doi.org/10.23919/icins51784.2022.9815397
https://doi.org/10.23919/icins51784.2022.9815397
Publikováno v:
Volume: 02, Issue: 02 57-63
International Journal of Aviation Science and Technology
International Journal of Aviation Science and Technology
In a class of diffusion Markov processes, we formulate a problem of identification of nonlinear stochastic dynamic systems with random parameters, multiplicative and additive noises, control functions, and the state vector at a final time moment. For
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::257b28e328da6f88a160b52ddc1688d3
https://dergipark.org.tr/tr/pub/ijast/issue/66334/1000229
https://dergipark.org.tr/tr/pub/ijast/issue/66334/1000229
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