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Mathematical Models of a Solar Sail Spacecraft Controlled Motion. / Korolev, V. S.; Polyakhova, E. N.; Pototskaya, I. Yu; Stepenko, N. A.

Proceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020. ред. / Valentin N. Tkhai. Institute of Electrical and Electronics Engineers Inc., 2020. 9140472 (Proceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020).

Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › Рецензирование

Harvard

Korolev, VS, Polyakhova, EN, Pototskaya, IY & Stepenko, NA 2020, Mathematical Models of a Solar Sail Spacecraft Controlled Motion. в VN Tkhai (ред.), Proceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020., 9140472, Proceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020, Institute of Electrical and Electronics Engineers Inc., 15th International Conference on Stability and Oscillations of Nonlinear Control Systems , Москва, Российская Федерация, 2/06/20. https://doi.org/10.1109/STAB49150.2020.9140472

APA

Korolev, V. S., Polyakhova, E. N., Pototskaya, I. Y., & Stepenko, N. A. (2020). Mathematical Models of a Solar Sail Spacecraft Controlled Motion. в V. N. Tkhai (Ред.), Proceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020 [9140472] (Proceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/STAB49150.2020.9140472

Vancouver

Korolev VS, Polyakhova EN, Pototskaya IY, Stepenko NA. Mathematical Models of a Solar Sail Spacecraft Controlled Motion. в Tkhai VN, Редактор, Proceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020. Institute of Electrical and Electronics Engineers Inc. 2020. 9140472. (Proceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020). https://doi.org/10.1109/STAB49150.2020.9140472

Author

Korolev, V. S. ; Polyakhova, E. N. ; Pototskaya, I. Yu ; Stepenko, N. A. / Mathematical Models of a Solar Sail Spacecraft Controlled Motion. Proceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020. Редактор / Valentin N. Tkhai. Institute of Electrical and Electronics Engineers Inc., 2020. (Proceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020).

BibTeX

@inproceedings{54c147d8a0214c8ea7bce538e853f7cb,
title = "Mathematical Models of a Solar Sail Spacecraft Controlled Motion",
abstract = "The features of a solar sail Spacecraft control and the possibilities to take into account the translational and rotational motion are considered. Based on the approximation of the motion equations for various orbits and body parameters, control possibilities and conditions for the stability of motion in given orbits as well as in the vicinity of libration points are discussed.To control the Spacecraft motion you can change the size, shape, surface properties or orientation of the sail elements relative to the flow of sunlight. The equations of motion can be presented based on a model of the problem of two bodies moving in a Central gravitational field, taking into account perturbations. When creating geosynchronous orbits in the vicinity of the Earth or for placing the Sun-Earth-Spacecraft system at libration points, a more general model of the photogravitational restricted three-body problem should be used.To obtain control capabilities and stability conditions for the motion in the specified orbits, as well as in the vicinity of collinear or triangular libration points, we do approximation of the perturbed motion equations system for different orbits and parameters of the main bodies. The stability of the Spacecraft sails system orientation is provided by the forces moments relative to the center of mass.",
keywords = "control, light pressure, solar sail, stability",
author = "Korolev, {V. S.} and Polyakhova, {E. N.} and Pototskaya, {I. Yu} and Stepenko, {N. A.}",
note = "Funding Information: This work was carried out the financial support by Russian Foundation for Basic Research, project No. 18-08-00419. Publisher Copyright: {\textcopyright} 2020 IEEE. Copyright: Copyright 2020 Elsevier B.V., All rights reserved.; 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference) (STAB), STAB 2020 ; Conference date: 02-06-2020 Through 05-06-2020",
year = "2020",
month = jun,
doi = "10.1109/STAB49150.2020.9140472",
language = "English",
series = "Proceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
editor = "Tkhai, {Valentin N.}",
booktitle = "Proceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020",
address = "United States",

}

RIS

TY - GEN

T1 - Mathematical Models of a Solar Sail Spacecraft Controlled Motion

AU - Korolev, V. S.

AU - Polyakhova, E. N.

AU - Pototskaya, I. Yu

AU - Stepenko, N. A.

N1 - Conference code: 15

PY - 2020/6

Y1 - 2020/6

N2 - The features of a solar sail Spacecraft control and the possibilities to take into account the translational and rotational motion are considered. Based on the approximation of the motion equations for various orbits and body parameters, control possibilities and conditions for the stability of motion in given orbits as well as in the vicinity of libration points are discussed.To control the Spacecraft motion you can change the size, shape, surface properties or orientation of the sail elements relative to the flow of sunlight. The equations of motion can be presented based on a model of the problem of two bodies moving in a Central gravitational field, taking into account perturbations. When creating geosynchronous orbits in the vicinity of the Earth or for placing the Sun-Earth-Spacecraft system at libration points, a more general model of the photogravitational restricted three-body problem should be used.To obtain control capabilities and stability conditions for the motion in the specified orbits, as well as in the vicinity of collinear or triangular libration points, we do approximation of the perturbed motion equations system for different orbits and parameters of the main bodies. The stability of the Spacecraft sails system orientation is provided by the forces moments relative to the center of mass.

AB - The features of a solar sail Spacecraft control and the possibilities to take into account the translational and rotational motion are considered. Based on the approximation of the motion equations for various orbits and body parameters, control possibilities and conditions for the stability of motion in given orbits as well as in the vicinity of libration points are discussed.To control the Spacecraft motion you can change the size, shape, surface properties or orientation of the sail elements relative to the flow of sunlight. The equations of motion can be presented based on a model of the problem of two bodies moving in a Central gravitational field, taking into account perturbations. When creating geosynchronous orbits in the vicinity of the Earth or for placing the Sun-Earth-Spacecraft system at libration points, a more general model of the photogravitational restricted three-body problem should be used.To obtain control capabilities and stability conditions for the motion in the specified orbits, as well as in the vicinity of collinear or triangular libration points, we do approximation of the perturbed motion equations system for different orbits and parameters of the main bodies. The stability of the Spacecraft sails system orientation is provided by the forces moments relative to the center of mass.

KW - control

KW - light pressure

KW - solar sail

KW - stability

UR - http://www.scopus.com/inward/record.url?scp=85091697607&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/d4a8b876-96cb-39f2-98be-1186fac7b7b1/

U2 - 10.1109/STAB49150.2020.9140472

DO - 10.1109/STAB49150.2020.9140472

M3 - Conference contribution

AN - SCOPUS:85091697607

T3 - Proceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020

BT - Proceedings of 2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference), STAB 2020

A2 - Tkhai, Valentin N.

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference) (STAB)

Y2 - 2 June 2020 through 5 June 2020

ER -

ID: 64733132