Abstract
We present a detailed investigation of the dramatic changes that occur in the \(\mathcal {L}_1\) halo family when radiation pressure is introduced into the Sun–Earth circular restricted three-body problem (CRTBP). This photo-gravitational CRTBP can be used to model the motion of a solar sail orientated perpendicular to the Sun-line. The problem is then parameterized by the sail lightness number, the ratio of solar radiation pressure acceleration to solar gravitational acceleration. Using boundary-value problem numerical continuation methods and the AUTO software package (Doedel et al. in Int J Bifurc Chaos 1:493–520, 1991) the families can be fully mapped out as the parameter \(\beta \) is increased. Interestingly, the emergence of a branch point in the retrograde satellite family around the Earth at \(\beta \approx 0.0387\) acts to split the halo family into two new families. As radiation pressure is further increased one of these new families subsequently merges with another non-planar family at \(\beta \approx 0.289\), resulting in a third new family. The linear stability of the families changes rapidly at low values of \(\beta \), with several small regions of neutral stability appearing and disappearing. By using existing methods within AUTO to continue branch points and period-doubling bifurcations, and deriving a new boundary-value problem formulation to continue the folds and Krein collisions, we track bifurcations and changes in the linear stability of the families in the parameter \(\beta \) and provide a comprehensive overview of the halo family in the presence of radiation pressure. The results demonstrate that even at small values of \(\beta \) there is significant difference to the classical CRTBP, providing opportunity for novel solar sail trajectories. Further, we also find that the branch points between families in the solar sail CRTBP provide a simple means of generating certain families in the classical case.
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P.V. acknowledges funding from the University of Portsmouth. The research of J.S. is supported by EPSRC Grant EP/J010820/1.
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Appendix
Appendix
In this appendix we present examples of the families discussed in Sects. 4–6. Examples of the L1, C2 and RS families for several values of \(\beta \) are shown in Figs. 12, 13 and 14. Examples of the H1, HR, H1B, H1C and H1R families for the Earth–Sun mass ratio in the RSCRTBP are shown in Figs. 15 and 16. A three-dimensional plot of the HR family for the Earth–Moon CRTBP (\(\mu =0.01215\), \(\beta =0\)) is shown in Fig. 17.
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Verrier, P., Waters, T. & Sieber, J. Evolution of the \(\mathcal {L}_1\) halo family in the radial solar sail circular restricted three-body problem. Celest Mech Dyn Astr 120, 373–400 (2014). https://doi.org/10.1007/s10569-014-9575-2
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DOI: https://doi.org/10.1007/s10569-014-9575-2