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Analysis of the Effects of Electromagnetic Forces on the Relative Motion of a Charged Spacecraft Formation Flying

Open Access
|Oct 2020

References

  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.
  6. Hill, G.W (1878). Researches in the lunar theory. American Journal of Mathematics, 1(1), pp. 5–26.10.2307/2369430
  7. Huang, X., Yan, Y., Zhou, Y., & Yi, T. (2014). Improved analytical solutions for relative motion of Lorentz spacecraft with application to relative navigation in low Earth orbit. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 228(11), 2138–2154.10.1177/0954410013511426
  8. Huang, X., Yan, Y. and Zhou, Y., (2015). Optimal Lorentz-augmented spacecraft formation flying in elliptic orbits. Acta Astronautica, 111, pp. 37–47.10.1016/j.actaastro.2015.02.012
  9. Kechichian, J. A. (1998). Motion in general elliptic orbit with respect to a dragging and precessingcoordinate frame. The Journal of the astronautical sciences, 46(1), 25–45.10.1007/BF03546191
  10. Melton, R.G., (2000). Time-explicit representation of relative motion between elliptical orbits. Journal of Guidance, Control, and Dynamics, 23(4), pp. 604–610.10.2514/2.4605
  11. Peck, M., (2005), August. Prospects and challenges for Lorentz-augmented orbits. In AIAA guidance, navigation, and control conference and exhibit (p. 5995)10.2514/6.2005-5995
  12. Peng, C., & Gao, Y. (2017). Formation-Flying Planar Periodic Orbits in the Presence of Intersatellite Lorentz Force. IEEE Transactions on Aerospace and Electronic Systems, 53(3), 1412–1430. Pollock, G.E., (2010). Propellantless spacecraft maneuvers using the electromagnetic Lorentz force (Doctoral dissertation, Purdue University)10.1109/TAES.2017.2671478
  13. Pollock, G.E., Gangestad, J.W., and Longuski, J.M., (2011). Analytical solutions for the relative motion of spacecraft subject to Lorentz-force perturbations. Acta Astronautica, 68 (1–2), pp. 204–217.10.1016/j.actaastro.2010.07.007
  14. Tsujii, S., Bando, M. and Yamakawa, H., (2012) Spacecraft formation flying dynamics and control using the geomagnetic Lorentz force. Journal of Guidance, Control, and Dynamics, 36(1), pp. 136–148.
  15. Ulaby, F.T., (2005) Electromagnetics for engineers (pp. 127–134). Pearson/Prentice Hall.
  16. Ulaby, F.T., Ravaioli, U., and Michielssen, E., (2014) Fundamentals of applied electromagnetics. 7 e. Prentice Hall.
  17. Vepa, R., (2018) Application of the Nonlinear Tschauner-Hempel Equations to Satellite Relative Position Estimation and Control. The Journal of Navigation, 71(1), pp. 44–64.
  18. Vokrouhlicky, D (1989). The geomagnetic effects on the motion of an electrically charged artificial satellite. Celestial Mechanics and Dynamical Astronomy, 46(1), pp. 85–104.10.1007/BF02426715
  19. WH Clohessy, (1960) Terminal guidance system for satellite rendezvous. Journal of the Aerospace Sciences, 27(9), pp. 653–658.10.2514/8.8704
DOI: https://doi.org/10.2478/arsa-2020-0007 | Journal eISSN: 2083-6104 | Journal ISSN: 1509-3859
Language: English
Page range: 87 - 99
Submitted on: Dec 13, 2019
Accepted on: Jun 29, 2020
Published on: Oct 8, 2020
Published by: Polish Academy of Sciences, Space Research Centre
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2020 Shafeeq Kaheal Tealib, Yehia Abdel-Aziz, Mervat El-Said Awad, Khalil Ibrahim Khalil, Mohmed Radwan, published by Polish Academy of Sciences, Space Research Centre
This work is licensed under the Creative Commons Attribution 4.0 License.