A multi-step method to calculate long-term quasi-periodic orbits around the Sun-Earth $L_{1}$/$L_{2}$
Author:
Funder
National Natural Science Foundation of China
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Astronomy and Astrophysics
Link
https://link.springer.com/content/pdf/10.1007/s10509-022-04135-5.pdf
Reference56 articles.
1. Akiyama, Y., Bando, M., Hokamoto, S.: Periodic and quasi-periodic orbit design based on the center manifold theory. Acta Astronaut. 160, 672–682 (2019)
2. Akp, A., Eia, B., Rk, C.: Effect of moon perturbation on the energy curves and equilibrium points in the Sun–Earth–Moon system. New Astron. 84 (2020)
3. Baresi, N., Olikara, Z.P., Scheeres, D.J.: Fully numerical methods for continuing families of quasi-periodic invariant tori in astrodynamics. J. Astronaut. Sci. 65(2), 157–182 (2018)
4. Davis, K.E., Anderson, R.L., Scheeres, D.J., et al.: Optimal transfers between unstable periodic orbits using invariant manifolds. Celest. Mech. Dyn. Astron. 109(3), 241–264 (2011). https://doi.org/10.1007/s10569-010-9327-x
5. DeFilippi, G. Jr: Station keeping at the l4 libration point: a three dimensional study. Thesis, Air Force Inst. Of Tech (1977)
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