Zobrazeno 1 - 10
of 57
pro vyhledávání: '"Yu. M. Zabolotnov"'
Autor:
S. Chen, Yu. M. Zabolotnov
Publikováno v:
Космические аппараты и технологии, Vol 6, Iss 4, Pp 235-245 (2022)
The problem of controlling a rotating hub-spoke tethered formation system in low Earth orbit is considered, in which microsatellites are located radially around the central spacecraft (hub) and connected to it by tethers (spokes). To analyze the dyna
Externí odkaz:
https://doaj.org/article/01a38302c6a54c7bbade004263a3e356
Autor:
Shumin Chen, Yu. M. Zabolotnov
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 21, Iss 3, Pp 69-84 (2022)
The problem of forming a rotating ring-shaped tethered system consisting of three nanosatellites is considered. To analyze the dynamics of the tether system, a mathematical model is developed in the orbital coordinate system using the Lagrange method
Externí odkaz:
https://doaj.org/article/9e1b64323e224065a60e1c64b5df4c6d
Autor:
T. A. Ledkova, Yu. M. Zabolotnov
Publikováno v:
Космические аппараты и технологии, Vol 5, Iss 3, Pp 153-159 (2021)
The development of space transport systems for the delivery of payloads and the study of the lunar surface is an important scientific and technical challenge. The article considers a near-lunar space tether system consisting of a station and a micros
Externí odkaz:
https://doaj.org/article/1dd4c4e17b374696bb4d8217728f31b9
Autor:
T. A. Ledkova, Yu. M. Zabolotnov
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 20, Iss 2, Pp 63-73 (2021)
The motion of a space tether system, consisting of a constellation of two microsatellites and a space station, is investigated. The station moves in a circular undisturbed circular lunar orbit. The process of deployment of tethers to bring the system
Externí odkaz:
https://doaj.org/article/3cdd0a9cf3424cf69e2125f6da344e85
Publikováno v:
Космические аппараты и технологии, Vol 5, Iss 1, Pp 27-34 (2021)
The dynamic analysis and motion control of a spinning tether system for an interplanetary mission to Mars is considered. The space system consists of two spacecraft connected by a tether with thrusts to control its movement. The movements of the teth
Externí odkaz:
https://doaj.org/article/10f693e366004d17a9ce34b899a51587
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 19, Iss 1, Pp 64-77 (2020)
The paper considers parametric optimization of the process of changing orbital parameters by using a spinning electrodynamic tether system. Changes in the semi-major axis and eccentricity are taken as the two major goals, and two control laws are pro
Externí odkaz:
https://doaj.org/article/f1338f571b7142f6a1b3027f39ab6cb0
Autor:
Ch. Wang, Yu. M. Zabolotnov
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 16, Iss 2, Pp 7-17 (2017)
Control of deploying an extended tether system into the vertical position is considered in the paper. It is assumed that in the initial state the system consisting of two space vehicles moves in a circular Earth orbit. We propose nominal control prog
Externí odkaz:
https://doaj.org/article/5a19c864773b4b8698ff1b02bbb5cf2b
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 15, Iss 2, Pp 102-113 (2016)
The stability of motion of a space tether system with an atmospheric probe is investigated in the paper. The equilibrium position stability of a space tether system near the local vertical (static stability) and deployment stability (dynamic stabilit
Externí odkaz:
https://doaj.org/article/268782b82a764be59a3409e0b92f018e
Autor:
Yu. M. Zabolotnov, A. A. Lobankov
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 15, Iss 1, Pp 46-54 (2016)
The problem of stabilizing the motion of small spacecraft relative to the center of mass in the process of deploying an orbital tether system is presented in the paper. Stabilization is carried out with respect to the direction of the tether and is c
Externí odkaz:
https://doaj.org/article/738dece57a2c480a8c49f83d27fbaeab
Publikováno v:
Cosmic Research. 60:375-386
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::16a3a21f5d65fe898324f490628fb273
https://doi.org/10.1134/s0010952522050070
https://doi.org/10.1134/s0010952522050070