Analysis of the Effects of Electromagnetic Forces on the Relative Motion of a Charged Spacecraft Formation Flying
Author:
Affiliation:
1. National Research Institute of Astronomy and Geophysics , Helwan , Cairo , Egypt
2. Faculty of Science Cairo University , Giza , Cairo , Egypt
Abstract
Publisher
Walter de Gruyter GmbH
Link
https://www.sciendo.com/pdf/10.2478/arsa-2020-0007
Reference19 articles.
1. Abdel-Aziz, Y. A. (2007). Lorentz force effects on the orbit of a charged artificial satellite: a new approach. In AIP Conference Proceedings (Vol. 888, No. 1, pp. 385–391). American Institute of Physics.10.1063/1.2711134
2. Abdel-Aziz, Y.A., and Khalil, K.I (2014). Electromagnetic effects on the orbital motion of a charged spacecraft. Research in Astronomy and Astrophysics, 14(5), p. 589.10.1088/1674-4527/14/5/008
3. Abdel-Aziz, Y.A., and Shoaib, M., (2015). Attitude dynamics and control of spacecraft using geomagnetic Lorentz force. Research in Astronomy and Astrophysics, 15(1), p. 127.10.1088/1674-4527/15/1/012
4. Bakhtiari, M., Daneshjou, K., & Fakoor, M. (2017). Long-term effects of main-body’s obliquity on satellite formation perturbed by third-body gravity in elliptical and inclined orbit. Research in Astronomy and Astrophysics, 17(4), 039.10.1088/1674-4527/17/4/39
5. Curtis, H.D., (2013). Orbital mechanics for engineering students. Butterworth-Heinemann.
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