Zobrazeno 1 - 10
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pro vyhledávání: '"V. L. Balakin"'
Autor:
V. L. Balakin, M. M. Krikunov
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 18, Iss 3, Pp 16-28 (2019)
Disturbed motion of the hypersonic first stage of an aerospace system in climb is analyzed. Deviations of atmospheric density from standard values and deviations of aerodynamic force coefficients from reference values are taken as disturbances. Distu
Externí odkaz:
https://doaj.org/article/43f369282bbc444aa2749171256155b6
Autor:
V. L. Balakin, M. M. Krikunov
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 18, Iss 2, Pp 7-20 (2019)
Disturbed motion of a hypersonic vehicle in climb is analyzed. Deviations of atmospheric density from standard values and deviations of aerodynamic force coefficients from nominal values are taken as disturbances. Disturbed motion of a hypersonic veh
Externí odkaz:
https://doaj.org/article/bce4c4374d694b7a9d02d1425c80d287
Autor:
V. L. Balakin, M. M. Krikunov
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 18, Iss 1, Pp 18-29 (2019)
Control programs and flight paths of the hypersonic first stage of an aerospace system in climb with acceleration to hypersonic velocity are analyzed. Two approaches to determining the control programs and flight paths are identified: the "traditiona
Externí odkaz:
https://doaj.org/article/3cd241284b55465c9a6494ef12119d85
Autor:
V. L. Balakin, M. M. Krikunov
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 17, Iss 4, Pp 18-26 (2018)
Control programs and flight paths of a hypersonic vehicle in climb are analyzed. Two approaches to solving the task of determining the control programs and flight paths are identified: the traditional approach and the optimization one. The traditiona
Externí odkaz:
https://doaj.org/article/6f6c93eeee82421f86aa2a0735757fa5
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 17, Iss 2, Pp 23-36 (2018)
The task of optimizing the space vehicle combined orbital plane change maneuver with the aim of maximizing its final mass is considered in the paper. Burst of power is used for the vehicles exit from the initial low earth orbit and subsequent re-entr
Externí odkaz:
https://doaj.org/article/0ade091175464bcaacd9f9f1d6cc2b0a
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 17, Iss 1, Pp 7-19 (2018)
The task of optimizing trans-atmospheric motion of a flight vehicle in order to maximize its final velocity with prescribed finite values of the height and flight path angle is considered. The angle of attack acts as control in passive motion of a ve
Externí odkaz:
https://doaj.org/article/1fdc365f5f4f4cf1856761c5284433ed
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 16, Iss 3, Pp 17-26 (2017)
The paper deals with the task of optimizing a space vehicles trans-atmospheric motion in order to maximize its terminal velocity at prescribed finite values of the height and trajectory inclination angle. The angle of attack acts as control in a vehi
Externí odkaz:
https://doaj.org/article/1d655f92bc0c4e0facf9111d13c7c6e2
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 15, Iss 3, Pp 9-16 (2016)
Multi-step terminal control of the subhypersonic first stage of an aerospace system in trans-atmospheric climb is considered. Passive motion of spacecraft in conditions of joint influence of atmospheric and aerodynamic disturbance is analyzed. Achiev
Externí odkaz:
https://doaj.org/article/b348f1488a9a4963a980b31c515a1166
Autor:
V. L. Balakin, A. V. Kovalyov
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 15, Iss 2, Pp 9-21 (2016)
The problem of forming command control of the subhypersonic first stage of an aerospace system in climb is considered. Passive motion of spacecraft in conditions of maximum atmospheric density disturbance is analyzed. Achieving the prescribed value o
Externí odkaz:
https://doaj.org/article/8310e6fa59e9435f9bc4f8148c0ec89c
Autor:
A. S. Zaitsev, V. L. Balakin, K. E. Voronov, V. I. Abrashkin, Victor Vasil’yevich Sazonov, I. V. Belokonov, N. D. Semkin, V. V. Ivanov, A. E. Kazakova
Publikováno v:
Cosmic Research. 41:39-50
The results of determination of the uncontrolled attitude motion of the Foton-12 satellite (placed in orbit on September 9, 1999, terminated its flight on September 24, 1999) are presented. The determination was carried out by the onboard measurement
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7f4928639de5a9e322e5fe5f13143523
https://doi.org/10.1023/a:1022351529382
https://doi.org/10.1023/a:1022351529382