Abstract
We use the numerical continuation package AUTO to investigate families of periodic orbits in the solar sail circular restricted three-body problem. For a sail orientated perpendicular to the Sun-line we find significant differences to the classical case for some families near the Earth, including the L Halo family and retrograde satellite family. Specifically, we expand on existing results and find that the change in the Halo family H1 is associated with a bifurcation of a branch point in the retrograde satellite family, which splits H1 in half. We also track regions of stability within the family, and find some large amplitude stable orbits. For a sail tilted relative to the Earth-Sun line only we find large amplitude families with some stable orbits. Interestingly there is also a small range of parameters for which L 1 bifurcates into three separate points in this system.
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This work was funded by the University of Portsmouth’s Faculty of Technology.
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Verrier, P., Waters, T., Sieber, J. (2014). Families of Periodic Orbits for Solar Sails in the CRBTP. In: Macdonald, M. (eds) Advances in Solar Sailing. Springer Praxis Books(). Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-34907-2_52
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DOI: https://doi.org/10.1007/978-3-642-34907-2_52
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