Equilibrium Conditions for Tethered NanosatelliteConstellations

Denilson Paulo Souza dos Santos, Jorge Kennety Silva Formiga, Rita de Cássia Domingos

Resumo


This expanded summary describes a tethered spacecraft system modeled in three-dimensionalproblem with six smaller bodies connected by a cable of negligible mass and rigid. This allows themodel to be described by a Keplerian motion. [...]

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Referências


Belestsky, V. V., Levin, E. M., Dynamics of Space Tethers Systems. San Diego - California:Advances in the Astronautical Sciences, Vol. 83 - American Astronautical Society, 1993.

Pearson J., Anchored Lunar Satellites for Cislunar Transportation and Communication,Jour-nal of the Astronautical Sciences, Vol. XXVII, No. 1, 1979, pp. 39-62.

Santos, D. P. S., Ferreira, A. Three-dimensional two-body tether system – equilibrium so-lutions.Journal of Physics, v. 641, n. 1, p. 012009, 2015. http://dx.doi.org/10.1088/1742-6596/641/1/012009.

Moia. G. P., Santos, D. P. S., Formiga, J. K. S. Tension force in nanosatellite teth-ers systems.Journal of Physics, v.1365 p:012010, 2019. Doi:https://doi.org/10.1088/1742-6596/1365/1/012010.

Santos, D. P. S., Formiga, J. K. S. Analysis of stability for uniform rotationsof a dumbbellsystem in an elliptic orbit.International Journal of Advanced Engineering Research and Sci-ence (IJAERS), v.8(2), p.097–105, 2021. DOI:https://dx.doi.org/10.22161/ijaers.82.13


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