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Structural features of photogravitational celestial mechanics. / Korolev, V.; Polyakhova, E.; Pototskaya, I.; Stepenko, N.; Tureshbaev, A.

In: Journal of Physics: Conference Series, Vol. 1959, No. 1, 012038, 01.07.2021.

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Korolev, V. ; Polyakhova, E. ; Pototskaya, I. ; Stepenko, N. ; Tureshbaev, A. / Structural features of photogravitational celestial mechanics. In: Journal of Physics: Conference Series. 2021 ; Vol. 1959, No. 1.

BibTeX

@article{422a1661f50c4aa9947a352b022943f4,
title = "Structural features of photogravitational celestial mechanics",
abstract = "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.",
author = "V. Korolev and E. Polyakhova and I. Pototskaya and N. Stepenko and A. Tureshbaev",
note = "Publisher Copyright: {\textcopyright} 2021 Published under licence by IOP Publishing Ltd.; International Scientific Conference on Mechanics {"}The Ninth Polyakhov's Reading{"}, ISCM 2021 ; Conference date: 09-03-2021 Through 12-03-2021",
year = "2021",
month = jul,
day = "1",
doi = "10.1088/1742-6596/1959/1/012038",
language = "English",
volume = "1959",
journal = "Journal of Physics: Conference Series",
issn = "1742-6588",
publisher = "IOP Publishing Ltd.",
number = "1",

}

RIS

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