The Method of Zero Tangential Strengths in the Problem of Charge Distribution over the Surfaces of Two Interacting Tori

Document Type : Research Paper

Authors
Saint Petersburg State University, 7-9 Universitetskaya nab., Saint Petersburg, 199034, Russia
Abstract
In this paper, a system of two circular concentric non-touching tori is considered. An electrostatic charge can be applied to each of the tori. The problem is to find the density of charge distribution over the surfaces of the tori, taking into account the Coulomb interaction between the surfaces. The required density is found numerically by the method of successive approximations based on the fact that in the static case, the total tangential strength of the Coulomb forces is zero at each of the points on the surface of each of the tori. The corresponding functional is constructed, the problem of numerical minimization of which is solved by the gradient descent method.
Keywords
Subjects

Publisher’s Note Shahid Chamran University of Ahvaz remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

[1] Marov, M.Y., Radiation and space flights safety: An insight, Acta Astronautica, 176, 2020, 580–590.
[2] Ryabova, T.Y., Electrostatic protection from cosmic radiation (the current status and prospects), Kosmicheskaia Biologiia i Aviakosmicheskaia Meditsina, 17(2), 1983, 4–7.
[3] Akatov, Y., Dudkin, V., Kovalev, E., Benton, E., Frank, A., Watts, J. Jr, Parnell, T., Depth distribution of absorbed dose on the external surface of Cosmos 1887 biosatellite, International Journal of Radiation Applications and Instrumentation. Part D. Nuclear Tracks and Radiation Measurements, 17(2), 1990, 105–107.
[4] Sussingham, J.C., Watkins, S.A., Cocks, F.H., Forty years of development of active systems for radiation protection of spacecraft, Journal of the Astronautical Sciences, 47(3-4), 1999, 165–175.
[5] Metzger, P., Lane, J., Youngquist, R., Progress toward electrostatic radiation shielding of interplanetary spacecraft, in: Strategies, Concepts and Technical Challenges of Human Exploration Beyond Low Earth Orbit Paper Session II-B - 2004 (41st) Space Congress Proceedings, 6, 2004.
[6] Smith, J.G., Smith, T., Williams, M., Youngquist, R., Mendell, W., Potential polymeric sphere construction materials for a spacecraft electrostatic shield, Nasa Technical Memorandum, 2006, 214302.
[7] Joshi, R.P., Qiu, H., Tripathi, R.K., Configuration studies for active electrostatic space radiation shielding, Acta Astronautica, 88, 2013, 138–145.
[8] Metzger, P.T., Lane, J.E., Electric potential due to a system of conducting spheres, The Open Applied Physics Journal, 2, 2009, 32–48.
[9] Tashaev, Y.N., Modeling of the electrostatic field of the charged toroid, Uspekhi Prikladnoy Fiziki [Advances in Applied Physics] (in Russ.), 3(2), 2015, 126–132.
[10] Tikhonov, A.A., Natural Magneto-velocity Coordinate System for Satellite Attitude Stabilization: The Concept and Kinematic Analysis, Journal of Applied and Computational Mechanics, 7(4), 2021, 2113-2119.
[11] Aleksandrov, A.Yu., Tikhonov, A.A., Natural Magneto-velocity Coordinate System for Satellite Attitude Stabilization: Dynamics and Stability Analysis, Journal of Applied and Computational Mechanics, 9(2), 2023, 513-520.
[12] Landau, L., Bell, J., Kearsley, M., Pitaevskii, L., Lifshitz, E., Sykes, J., Electrodynamics of Continuous Media, Course of Theoretical Physics, Elsevier Science, 2013.
[13] Majic, M., A surface integral approach to Poisson’s equation and analytic expressions for the gravitational field of toroidal mass distributions, Applied Numerical Mathematics, 148, 2020, 98–108.
[14] Polyak, B.T., Introduction to Optimization, Optimization Software, Inc., Publications Division, New York, USA, 2020.
[15] Nocedal, J., Wright, S., Numerical Optimization, Springer, New York, 2006.