Balancing the effects of solar radiation pressure on the orbital elements of a spacecraft using Lorentz force

Abstract In this work, orbits of Lorentz spacecrafts and satellites are investigated under the perturbation of solar radiation pressure. An attempt is made to control the perturbation of the solar radiation pressure using the effect of Lorentz force that affects an electrically charged spacecraft. T...

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Main Authors: M. A. Yousef, M. I. El-Saftawy, A. Mostafa
Format: Article
Language:English
Published: Nature Portfolio 2022-09-01
Series:Scientific Reports
Online Access:https://doi.org/10.1038/s41598-022-20166-y
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author M. A. Yousef
M. I. El-Saftawy
A. Mostafa
author_facet M. A. Yousef
M. I. El-Saftawy
A. Mostafa
author_sort M. A. Yousef
collection DOAJ
description Abstract In this work, orbits of Lorentz spacecrafts and satellites are investigated under the perturbation of solar radiation pressure. An attempt is made to control the perturbation of the solar radiation pressure using the effect of Lorentz force that affects an electrically charged spacecraft. The charge per unit mass is the controlling parameter in this process. The redial, transverse and normal components of the mentioned forces are constructed. The Lagrange planetary equations for perturbations in the Keplerian orbital elements are formulated. The formula describing the charge per unit mass, as function of the physical parameter of the problem as well as the orbital elements, were derived. The effects of the combined forces are analytically and numerically studied.
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spelling doaj.art-23d32a5d200d437aadc3044c831caef02022-12-22T03:18:02ZengNature PortfolioScientific Reports2045-23222022-09-0112111510.1038/s41598-022-20166-yBalancing the effects of solar radiation pressure on the orbital elements of a spacecraft using Lorentz forceM. A. Yousef0M. I. El-Saftawy1A. Mostafa2Department of Astronomy and Space Science, Faculty of Science, King Abdulaziz UniversityDepartment of Astronomy and Space Science, Faculty of Science, King Abdulaziz UniversityDepartment of Mathematics, Faculty of Science, Ain Shams UniversityAbstract In this work, orbits of Lorentz spacecrafts and satellites are investigated under the perturbation of solar radiation pressure. An attempt is made to control the perturbation of the solar radiation pressure using the effect of Lorentz force that affects an electrically charged spacecraft. The charge per unit mass is the controlling parameter in this process. The redial, transverse and normal components of the mentioned forces are constructed. The Lagrange planetary equations for perturbations in the Keplerian orbital elements are formulated. The formula describing the charge per unit mass, as function of the physical parameter of the problem as well as the orbital elements, were derived. The effects of the combined forces are analytically and numerically studied.https://doi.org/10.1038/s41598-022-20166-y
spellingShingle M. A. Yousef
M. I. El-Saftawy
A. Mostafa
Balancing the effects of solar radiation pressure on the orbital elements of a spacecraft using Lorentz force
Scientific Reports
title Balancing the effects of solar radiation pressure on the orbital elements of a spacecraft using Lorentz force
title_full Balancing the effects of solar radiation pressure on the orbital elements of a spacecraft using Lorentz force
title_fullStr Balancing the effects of solar radiation pressure on the orbital elements of a spacecraft using Lorentz force
title_full_unstemmed Balancing the effects of solar radiation pressure on the orbital elements of a spacecraft using Lorentz force
title_short Balancing the effects of solar radiation pressure on the orbital elements of a spacecraft using Lorentz force
title_sort balancing the effects of solar radiation pressure on the orbital elements of a spacecraft using lorentz force
url https://doi.org/10.1038/s41598-022-20166-y
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