Zobrazeno 1 - 10
of 15
pro vyhledávání: '"S N, Evdokimov"'
Autor:
E. A. Mikrin, S. I. Klimanov, S. N. Evdokimov, Andrey Georgievich Tuchin, Andrey Nikolaevich Korchagin, Alexander Sergeevich Samotokhin, Yu. G. Sikharulidze
Publikováno v:
Cosmic Research. 58:122-137
The task of guidance of a spacecraft, returning from the Moon, to a given landing area, under an effect of “magnified” disturbing factors, is considered. The earlier developed terminal algorithm for control of the descent from a near-Earth orbit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::351bf04a41b26d308d702537456fb57d
https://doi.org/10.1134/s0010952520020033
https://doi.org/10.1134/s0010952520020033
Autor:
E. A. Mikrin, Yu. G. Sikharulidze, Andrey Georgievich Tuchin, Alexander Sergeevich Samotokhin, S. I. Klimanov, S. N. Evdokimov, Andrey Nikolaevich Korchagin
Publikováno v:
Cosmic Research. 57:176-187
The problem of reentry vehicle control during its descent from a near-Earth orbit is considered under conditions of “enhanced” disturbances. The earlier developed terminal descent control algorithm is considerably improved to satisfy constraints
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::102804336f74b5003cdf1a885d285623
https://doi.org/10.1134/s0010952519030031
https://doi.org/10.1134/s0010952519030031
Publikováno v:
Russian Journal of Organic Chemistry. 55:161-167
The NMR spectra of several heterocyclic compounds synthesized at Omsk universities revealed manifestation of a diasteomerism at a large (up to fifteen bonds) distance between the stereogenic centers. This phenomenon was explained by a regular helical
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f9a6bcd1d0aab785844a168f537d088f
https://doi.org/10.1134/s1070428019020064
https://doi.org/10.1134/s1070428019020064
Autor:
V. P. Talsi, S. N. Evdokimov
Publikováno v:
Russian Journal of Organic Chemistry. 53:1630-1636
Dynamic NMR was applied to measuring the value ΔG≠ characterizing the height of the barrier to the pyramidal inversion of the nitrogen atom in carbamate and thiocarbamate anions formed at the reaction of 2-aminoethanol with CO2 and COS. The refine
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d88636edc19c199c8e7b7a4077a9f5ff
https://doi.org/10.1134/s1070428017110021
https://doi.org/10.1134/s1070428017110021
Autor:
E. A. Mikrin, A. N. Korchagin, Andrey Georgievich Tuchin, Yu. G. Sikharulidze, S. I. Klimanov, S. N. Evdokimov
Publikováno v:
Journal of Computer and Systems Sciences International. 56:483-491
We consider the problem of attitude control of a descent vehicle in the Earth’s atmosphere returning from the Moon. A stabilization algorithm with a deadband and the optimal parameters, obtained with the numerical method, provide adequate landing a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::815f9acaa8f36d28476a98d2426eca74
https://doi.org/10.1134/s1064230717030091
https://doi.org/10.1134/s1064230717030091
Autor:
Andrey Georgievich Tuchin, E. A. Mikrin, A. N. Korchagin, Yu. G. Sikharulidze, S. N. Evdokimov, S. I. Klimanov
Publikováno v:
Journal of Computer and Systems Sciences International. 56:300-310
The algorithm of the two-point boundary problem is developed for choice the nominal deorbit point, from which a descent vehicle is enabled to land at a given place without a cross-range maneuver. The method is suggested and the example is given of co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::75590cb79cc3e96d7a7dec848d6f1daa
https://doi.org/10.1134/s106423071702006x
https://doi.org/10.1134/s106423071702006x
Autor:
S. I. Klimanov, A. N. Korchagin, D. A. Tuchin, Yu. G. Sikharulidze, Andrey Georgievich Tuchin, E. A. Mikrin, S. N. Evdokimov
Publikováno v:
Journal of Computer and Systems Sciences International. 53:908-924
Results of the boundary value problem solution for determining the trajectory of returning from the lunar orbit and landing on the Vostochnyi launch site are presented. The solution includes the calculation of the required expenditure of the characte
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8a21117268fb1cfbd1bd1320ced4b69b
https://doi.org/10.1134/s1064230714060069
https://doi.org/10.1134/s1064230714060069
Publikováno v:
Journal of Computer and Systems Sciences International. 53:267-274
A concept of the terminal descent control algorithm of the descent module at reentry into the Earth atmosphere with near-parabolic velocity is proposed. Trajectories with one and two (skip reentry) reentries are considered. Simultaneously, downrange
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e13e9f580aee20a081d63decede0255
https://doi.org/10.1134/s1064230714020075
https://doi.org/10.1134/s1064230714020075
Publikováno v:
Journal of Computer and Systems Sciences International. 53:137-148
A model of the general motion of the descent module that includes the motion of its center of mass and the attitude motion is constructed. An improved estimate of the reachability region in the case of descent in the disturbed Earth atmosphere is obt
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ac4aa5b7cc266cf1d0e69eeb94f52d78
https://doi.org/10.1134/s1064230714010043
https://doi.org/10.1134/s1064230714010043
Publikováno v:
Journal of Computer and Systems Sciences International. 51:802-817
Results concerning the terminal guidance algorithm at the reentry of the descent module into the Earth atmosphere are presented. This algorithm simultaneously eliminates predicted deviations in the downrange and crossrange directions. The restriction
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::07436f6859642a08fb6bbf4ab3b38c62
https://doi.org/10.1134/s1064230712060020
https://doi.org/10.1134/s1064230712060020