Результаты исследований: Научные публикации в периодических изданиях › статья в журнале по материалам конференции › Рецензирование
Structural features of photogravitational celestial mechanics. / Korolev, V.; Polyakhova, E.; Pototskaya, I.; Stepenko, N.; Tureshbaev, A.
в: Journal of Physics: Conference Series, Том 1959, № 1, 012038, 01.07.2021.Результаты исследований: Научные публикации в периодических изданиях › статья в журнале по материалам конференции › Рецензирование
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TY - JOUR
T1 - Structural features of photogravitational celestial mechanics
AU - Korolev, V.
AU - Polyakhova, E.
AU - Pototskaya, I.
AU - Stepenko, N.
AU - Tureshbaev, A.
N1 - Publisher Copyright: © 2021 Published under licence by IOP Publishing Ltd.
PY - 2021/7/1
Y1 - 2021/7/1
N2 - The features of mathematical models of controlled motion of a spacecraft with a solar sail, which take into account the translational and rotational motion of all parts of the structure, are considered. Equations for motion in a photogravitational field are used on the basis of the two-body problem, taking into account perturbations, or a more general model of the bounded three-body problem. The gravitational field is supplemented by the field of light pressure forces, which makes it possible to simulate real dynamics processes. When approximating the system of equations of perturbed motion for different orbits and parameters of the main bodies, control capabilities and stability conditions of motion are obtained at the specified orbits, as well as in the vicinity of libration points. Stability of orientation or rotation relative to the center of mass is provided by the moment of light pressure forces on the elements of the sail system or additional actions of special engines.
AB - The features of mathematical models of controlled motion of a spacecraft with a solar sail, which take into account the translational and rotational motion of all parts of the structure, are considered. Equations for motion in a photogravitational field are used on the basis of the two-body problem, taking into account perturbations, or a more general model of the bounded three-body problem. The gravitational field is supplemented by the field of light pressure forces, which makes it possible to simulate real dynamics processes. When approximating the system of equations of perturbed motion for different orbits and parameters of the main bodies, control capabilities and stability conditions of motion are obtained at the specified orbits, as well as in the vicinity of libration points. Stability of orientation or rotation relative to the center of mass is provided by the moment of light pressure forces on the elements of the sail system or additional actions of special engines.
UR - http://www.scopus.com/inward/record.url?scp=85111984783&partnerID=8YFLogxK
U2 - 10.1088/1742-6596/1959/1/012038
DO - 10.1088/1742-6596/1959/1/012038
M3 - Conference article
AN - SCOPUS:85111984783
VL - 1959
JO - Journal of Physics: Conference Series
JF - Journal of Physics: Conference Series
SN - 1742-6588
IS - 1
M1 - 012038
T2 - International Scientific Conference on Mechanics "The Ninth Polyakhov's Reading", ISCM 2021
Y2 - 9 March 2021 through 12 March 2021
ER -
ID: 85844574