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Attitude stabilization of a spacecraft equipped with large electrostatic protection screens. / Nikitin, D. Yu; Tikhonov, A. A.

EIGHTH POLYAKHOV'S READING. ed. / E Kustova; G Leonov; N Morosov; M Yushkov; M Mekhonoshina. Vol. 1959 1. ed. American Institute of Physics, 2018. (AIP Conference Proceedings).

Research output: Chapter in Book/Report/Conference proceedingConference contributionResearchpeer-review

Harvard

Nikitin, DY & Tikhonov, AA 2018, Attitude stabilization of a spacecraft equipped with large electrostatic protection screens. in E Kustova, G Leonov, N Morosov, M Yushkov & M Mekhonoshina (eds), EIGHTH POLYAKHOV'S READING. 1 edn, vol. 1959, AIP Conference Proceedings, American Institute of Physics, International Scientific Conference on Mechanics - Eighth Polyakhov's Reading, Saint Petersburg, Russian Federation, 29/01/18. https://doi.org/10.1063/1.5034614

APA

Nikitin, D. Y., & Tikhonov, A. A. (2018). Attitude stabilization of a spacecraft equipped with large electrostatic protection screens. In E. Kustova, G. Leonov, N. Morosov, M. Yushkov, & M. Mekhonoshina (Eds.), EIGHTH POLYAKHOV'S READING (1 ed., Vol. 1959). (AIP Conference Proceedings). American Institute of Physics. https://doi.org/10.1063/1.5034614

Vancouver

Nikitin DY, Tikhonov AA. Attitude stabilization of a spacecraft equipped with large electrostatic protection screens. In Kustova E, Leonov G, Morosov N, Yushkov M, Mekhonoshina M, editors, EIGHTH POLYAKHOV'S READING. 1 ed. Vol. 1959. American Institute of Physics. 2018. (AIP Conference Proceedings). https://doi.org/10.1063/1.5034614

Author

Nikitin, D. Yu ; Tikhonov, A. A. / Attitude stabilization of a spacecraft equipped with large electrostatic protection screens. EIGHTH POLYAKHOV'S READING. editor / E Kustova ; G Leonov ; N Morosov ; M Yushkov ; M Mekhonoshina. Vol. 1959 1. ed. American Institute of Physics, 2018. (AIP Conference Proceedings).

BibTeX

@inproceedings{c16a8f11a44947919ff5b56d57348d7e,
title = "Attitude stabilization of a spacecraft equipped with large electrostatic protection screens",
abstract = "A satellite with a system of three electrostatic radiation protection (ERP) screens is under consideration. The screens are constructed as electrostatically charged toroidal shields with characteristic size of order equal to 100 m. The interaction of electric charge with the Earth's magnetic field (EMF) give rise to the Lorentz torque acting upon a satellite attitude motion. As the sizes of ERP system are large, we derive the Lorentz torque taking into account the complex form of ERP screens and gradient of the EMF in the screen volume. It is assumed that the satellite center of charge coincides with the satellite mass center. The EMF is modeled by the straight magnetic dipole. In the paper we investigate the usage of Lorentz torque for passive attitude stabilization for satellite in a circular equatorial orbit. Mathematical model for attitude dynamics of a satellite equipped with ERP interacting with the EMF is derived and first integral of corresponding differential equations is constructed. The straight equilibrium position of the satellite in the orbital frame is found. Sufficient conditions for stability of satellite equilibrium position are constructed with the use of the first integral. The gravity gradient torque is taken into account. The satellite equilibrium stability domain is constructed.",
keywords = "ELECTRODYNAMIC STABILIZATION, GEOMAGNETIC-FIELD, LORENTZ-FORCE, SATELLITES, ORBITS, MOTION, SYSTEM, EARTH",
author = "Nikitin, {D. Yu} and Tikhonov, {A. A.}",
year = "2018",
doi = "10.1063/1.5034614",
language = "English",
volume = "1959",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics",
editor = "E Kustova and G Leonov and N Morosov and M Yushkov and M Mekhonoshina",
booktitle = "EIGHTH POLYAKHOV'S READING",
address = "United States",
edition = "1",
note = "International Scientific Conference on Mechanics - Eighth Polyakhov's Reading : 8th Polyakhov's Reading ; Conference date: 29-01-2018 Through 02-02-2018",
url = "https://events.spbu.ru/events/polyakhov_readings, http://nanomat.spbu.ru/en/node/175, http://nanomat.spbu.ru/ru/node/192, http://spbu.ru/news-events/calendar/viii-polyahovskie-chteniya",

}

RIS

TY - GEN

T1 - Attitude stabilization of a spacecraft equipped with large electrostatic protection screens

AU - Nikitin, D. Yu

AU - Tikhonov, A. A.

N1 - Conference code: 8

PY - 2018

Y1 - 2018

N2 - A satellite with a system of three electrostatic radiation protection (ERP) screens is under consideration. The screens are constructed as electrostatically charged toroidal shields with characteristic size of order equal to 100 m. The interaction of electric charge with the Earth's magnetic field (EMF) give rise to the Lorentz torque acting upon a satellite attitude motion. As the sizes of ERP system are large, we derive the Lorentz torque taking into account the complex form of ERP screens and gradient of the EMF in the screen volume. It is assumed that the satellite center of charge coincides with the satellite mass center. The EMF is modeled by the straight magnetic dipole. In the paper we investigate the usage of Lorentz torque for passive attitude stabilization for satellite in a circular equatorial orbit. Mathematical model for attitude dynamics of a satellite equipped with ERP interacting with the EMF is derived and first integral of corresponding differential equations is constructed. The straight equilibrium position of the satellite in the orbital frame is found. Sufficient conditions for stability of satellite equilibrium position are constructed with the use of the first integral. The gravity gradient torque is taken into account. The satellite equilibrium stability domain is constructed.

AB - A satellite with a system of three electrostatic radiation protection (ERP) screens is under consideration. The screens are constructed as electrostatically charged toroidal shields with characteristic size of order equal to 100 m. The interaction of electric charge with the Earth's magnetic field (EMF) give rise to the Lorentz torque acting upon a satellite attitude motion. As the sizes of ERP system are large, we derive the Lorentz torque taking into account the complex form of ERP screens and gradient of the EMF in the screen volume. It is assumed that the satellite center of charge coincides with the satellite mass center. The EMF is modeled by the straight magnetic dipole. In the paper we investigate the usage of Lorentz torque for passive attitude stabilization for satellite in a circular equatorial orbit. Mathematical model for attitude dynamics of a satellite equipped with ERP interacting with the EMF is derived and first integral of corresponding differential equations is constructed. The straight equilibrium position of the satellite in the orbital frame is found. Sufficient conditions for stability of satellite equilibrium position are constructed with the use of the first integral. The gravity gradient torque is taken into account. The satellite equilibrium stability domain is constructed.

KW - ELECTRODYNAMIC STABILIZATION

KW - GEOMAGNETIC-FIELD

KW - LORENTZ-FORCE

KW - SATELLITES

KW - ORBITS

KW - MOTION

KW - SYSTEM

KW - EARTH

UR - http://www.scopus.com/inward/record.url?scp=85047214743&partnerID=8YFLogxK

U2 - 10.1063/1.5034614

DO - 10.1063/1.5034614

M3 - Conference contribution

AN - SCOPUS:85047214743

VL - 1959

T3 - AIP Conference Proceedings

BT - EIGHTH POLYAKHOV'S READING

A2 - Kustova, E

A2 - Leonov, G

A2 - Morosov, N

A2 - Yushkov, M

A2 - Mekhonoshina, M

PB - American Institute of Physics

T2 - International Scientific Conference on Mechanics - Eighth Polyakhov's Reading

Y2 - 29 January 2018 through 2 February 2018

ER -

ID: 75338659