Zobrazeno 1 - 10
of 21
pro vyhledávání: '"Yu. G. Sikharulidze"'
Publikováno v:
Cosmic Research. 60:347-357
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6e97ae76fba734fef7b7d085a25a538e
https://doi.org/10.1134/s0010952522050082
https://doi.org/10.1134/s0010952522050082
Publikováno v:
Journal of Computer and Systems Sciences International. 61:104-122
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b8ab38217bf999feb8fa27b4732f7218
https://doi.org/10.1134/s1064230722010099
https://doi.org/10.1134/s1064230722010099
Publikováno v:
Journal of Computer and Systems Sciences International. 60:477-488
The complex problem of constructing the return trajectories of a spacecraft (SC) from a circumlunar orbit before entering the Earth’s atmosphere for subsequent landing on the southern territory of the Russian Federation is considered. The problem i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::18fa60633faa0e0cb50d9df6539ddc23
https://doi.org/10.1134/s106423072102012x
https://doi.org/10.1134/s106423072102012x
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
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:
Yu. G. Sikharulidze, Andrey Georgievich Tuchin, V. N. Likhachev, B. I. Zhukov, V. P. Fedotov, D. A. Tuchin
Publikováno v:
Journal of Computer and Systems Sciences International. 55:260-270
An algorithm is developed for terminal guidance during the main deceleration section of the lunar landing trajectory of a spacecraft with an integrated propulsion system, which has a main engine with variable thrust and four auxiliary nonthrottleable
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e292d5fe7de8d846049b358f3d48211a
https://doi.org/10.1134/s1064230716010111
https://doi.org/10.1134/s1064230716010111
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