Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Irina V. Chernyakina"'
Publikováno v:
Advances in Space Research. 67:2757-2766
Detailed dynamic modelling of a solar sail requires recording of solar radiation pressure influence. A photon-solar sail is determined by the thrust value and the direction. We define the solar sail’s reflectivity depending on the film materials, t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::84c39dc138a12ec79816d75d2f2d1289
https://doi.org/10.1016/j.asr.2020.06.017
https://doi.org/10.1016/j.asr.2020.06.017
Autor:
Irina V. Chernyakina
Publikováno v:
Advances in Space Research. 67:2844-2854
Ballistic design of solar sailing missions in the solar system is composed of defining the design parameters, the control programs, and the trajectories that provide performance goals of a flight. The use of a solar sail spacecraft imposes specific r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e48636e5772c0cb8f441d7339ed4ecdf
https://doi.org/10.1016/j.asr.2020.01.032
https://doi.org/10.1016/j.asr.2020.01.032
Publikováno v:
Advances in Astronautics Science and Technology. 1:81-85
Ballistic design of the mission in the near circumsolar space is composed of a variety of control programs and the corresponding trajectories, which provide performance goals and satisfy the set of constraints. The use of a solar-sail spacecraft impo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a71efc8ba56c56996d929de2f874b35b
https://doi.org/10.1007/s42423-018-0018-0
https://doi.org/10.1007/s42423-018-0018-0
Autor:
Elizaveta A. Nikolaeva, Irina V. Chernyakina, Yaroslav S. Kiunov, Andrey U. Shornikov, Olga L. Starinova
Publikováno v:
2019 9th International Conference on Recent Advances in Space Technologies (RAST).
In this paper we consider objects with a nonspherical gravity field and small gravitational pull, for example, asteroids, planet's satellites, and comets. The publication discusses controlling of motion in the vicinity object with the irregular gravi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::67aa1706dac019343c0ec1d8f1903089
https://doi.org/10.1109/rast.2019.8767870
https://doi.org/10.1109/rast.2019.8767870
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 984:012027
Solar sailing spacecraft uses the light pressure to change the trajectory and are most effective in the immediate Sun vicinity, but the sail surface temperature most significant increases in the same area. Therefore, when designing solar sailing “h
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a841396e580c184b0cdcf2d1502450cc
https://doi.org/10.1088/1757-899x/984/1/012027
https://doi.org/10.1088/1757-899x/984/1/012027
Publikováno v:
AIP Conference Proceedings.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a955bb8ff23d204d1fcb9207732a5600
https://doi.org/10.1063/1.5081540
https://doi.org/10.1063/1.5081540
Publikováno v:
AIP Conference Proceedings.
The ballistic design of interplanetary missions consists of a choice of control programs and associated trajectories that ensure the achievement of the objective while meeting a variety of constraints. The use of solar-sails spacecraft for interplane
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3cb1eead4b34406aea4165c0c501ad3c
https://doi.org/10.1063/1.5081620
https://doi.org/10.1063/1.5081620
Publikováno v:
AIP Conference Proceedings.
Nonlinear angular motion of the electric propulsion spacecraft is analyzed. The spacecraft transfers are considered between L1 and L2 libration points of the Earth-Moon system. The influence of the shaded areas and gravitational effects of the Earth,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::38bed64f45629c84dadd53ab91f88ec5
https://doi.org/10.1063/1.5081548
https://doi.org/10.1063/1.5081548
Publikováno v:
AIP Conference Proceedings.
The paper considers a three-dimension nonlinear motion of a spacecraft with frame-type solar sail. The mathematical model of a guided heliocentric motion is described within combined polar coordinate system. The locally optimal control laws of orbita
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4fbd08075a84292b98ba23bc7133ceb6
https://doi.org/10.1063/1.5081564
https://doi.org/10.1063/1.5081564