Abstract
The Augmented Hill Three-Body problem is an extension of the classical Hill problem that, among other applications, has been used to model the motion of a solar sail around an asteroid. This model is a 3 degrees of freedom (3DoF) Hamiltonian system that depends on four parameters. This paper describes the bounded motions (periodic orbits and invariant tori) in an extended neighbourhood of some of the equilibrium points of the model. An interesting feature is the existence of equilibrium points with a 1:1 resonance, whose neighbourhood we also describe. The main tools used are the computation of periodic orbits (including their stability and bifurcations), the reduction of the Hamiltonian to centre manifolds at equilibria, and the numerical approximation of invariant tori. It is remarkable how the combination of these techniques allows the description of the dynamics of a 3DoF Hamiltonian system.
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Notes
The frequency vector of a quasi-periodic trajectory is determined up to an unimodular transformation.
References
Allgower, E.L., Georg, K.: Numerical Continuation Methods. Springer Series in Computational Mathematics. Springer, Berlin (1990)
Broschart, S.B., Lantoine, G., Grebow, D.J.: Characteristics of Quasi-Terminator Orbits Near Primitive Bodies. Jet Propulsion Laboratory, National Aeronautics and Space Administration, Pasadena, CA (2013)
Broschart, S.B., Lantoine, G., Grebow, D.J.: Quasi-terminator orbits near primitive bodies. Celest. Mech. 120(2), 195–215 (2014)
Carr, J.: Applications of Centre Manifold Theory. Applied Mathematical Sciences, vol. 35. Springer, New York (1981)
Castellà, E., Jorba, À.: On the vertical families of two-dimensional tori near the triangular points of the bicircular problem. Celest. Mech. 76(1), 35–54 (2000)
Ceccaroni, M., Celletti, A., Pucacco, G.: Birth of periodic and artificial halo orbits in the restricted three-body problem. Int. J. Non-Linear Mech. 81, 65–74 (2016a)
Ceccaroni, M., Celletti, A., Pucacco, G.: Halo orbits around the collinear points of the restricted three-body problem. Phys. D 317, 28–42 (2016b)
Celletti, A., Pucacco, G., Stella, D.: Lissajous and halo orbits in the restricted three-body problem. J. Nonlinear Sci. 25(2), 343–370 (2015)
Dachwald, B., Seboldt, W., Macdonald, M., Mengali, G., Quarta, A.A., McInnes, C.R., et al.: Potential Solar sail degradation effects on trajectory and attitude control. In: AIAA Guidance, Navigation, and Control Conference and Exhibit, vol. 6172, (2005)
Dachwald, B., Boehnhardt, H., Broj, U., Geppert, U.R.M.E., Grundmann, J.-T., Seboldt, W., et al.: Gossamer roadmap technology reference study for a multiple NEO rendezvous mission. In: Macdonald, M. (ed.) Advances in Solar Sailing. Springer Praxis Books, pp. 211–226. Springer, Berlin (2014)
Farrés, A., Jorba, À.: A dynamical system approach for the station keeping of a solar sail. J. Astronaut. Sci. 56(2), 199–230 (2008a)
Farrés, A., Jorba, À.: Solar sail surfing along families of equilibrium points. Acta Astron. 63, 249–257 (2008b)
Farrés, A., Jorba, À.: On the high order approximation of the centre manifold for ODEs. Discrete Contin. Dyn. Syst. Ser. B 14(3), 977–1000 (2010a)
Farrés, A., Jorba, À.: Periodic and quasi-periodic motions of a solar sail close to \(SL_1\) in the Earth–Sun system. Celest. Mech. 107(1–2), 233–253 (2010b)
Farrés, A., Jorba, À.: Orbital dynamics of a solar sail near L1 and L2 in the elliptic Hill problem. In: Proceedings of the 63rd International Astronautical Congress (2012)
Farrés, A., Jorba, À.: Artificial Equilibria in the RTBP for a Solar Sail and Applications. Springer International Publishing, Cham (2016a)
Farrés, A., Jorba, À.: Dynamics, geometry and solar sails. Indag. Math. 27(5), 1245–1264 (2016b)
Farrés, A., Jorba, À, Mondelo, J.M.: Orbital dynamics for a non-perfectly reflecting solar sail close to an asteroid. In: Proceedings of the 2nd IAA Conference on Dynamics and Control of Space Systems, Rome, Italy (2014a)
Farrés, A., Jorba, À., Mondelo, J.M., Villac, B.: Periodic motion for an imperfect solar sail near an asteroid. In: Macdonald, M. (ed.) Advances in Solar Sailing, pp. 885–898. Springer, Berlin (2014b)
Giancotti, M., Funase, R.: Solar sail equilibrium positions and transfer trajectories close to a Trojan asteroid. In: Proceedings of the 63rd International Astronautical Congress (2012)
Giancotti, M., Campagnola, S., Tsuda, Y., Kawaguchi, J.: Families of periodic orbits in Hill’s problem with solar radiation pressure: application to hayabusa 2. Celest. Mech. 120(3), 269–286 (2014)
Giorgilli, A., Delshams, A., Fontich, E., Galgani, L., Simó, C.: Effective stability for a Hamiltonian system near an elliptic equilibrium point, with an application to the restricted three body problem. J. Differ. Equ. 77, 167–198 (1989)
Gómez, G., Mondelo, J.M.: The dynamics around the collinear equilibrium points of the RTBP. Phys. D 157(4), 283–321 (2001)
Gómez, G., Marcote, M., Mondelo, J.M.: The invariant manifold structure of the spatial Hill’s problem. Dyn. Syst. 20(1), 115–147 (2005)
Haro, A., Canadell, M., Luque, A., Mondelo, J.-M., Figueras, J.-L.: The Parameterization Method for Invariant Manifolds. From Rigorous Results to Effective Computations, volume 195 of Applied Mathematical Sciences. Springer, Berlin (2016)
Hénon, M.: Exploration numérique du problème restreint. II: Masses égales, stabilité des orbites periódiques. Ann. Astrophys. 28(6), 992–1007 (1965)
Hill, G.W.: Researches in the Lunar Theory. Amer. J. Math. 1(1):5–26, 129–147, 245–260 (1878)
Jorba, À.: A methodology for the numerical computation of normal forms, centre manifolds and first integrals of Hamiltonian systems. Exp. Math. 8(2), 155–195 (1999)
Jorba, À., Masdemont, J.: Dynamics in the centre manifold of the collinear points of the restricted three body problem. Phys. D 132, 189–213 (1999)
Jorba, À., Villanueva, J.: On the normal behaviour of partially elliptic lower dimensional tori of Hamiltonian systems. Nonlinearity 10, 783–822 (1997)
Kanavos, S.S., Markellos, V.V., Perdios, E.A., Douskos, C.N.: The photogravitational Hill problem: numerical exploration. Earth Moon Planets 91(4), 223–241 (2002)
Liu, K.Y.-Y., Villac, B.: Periodic orbits families in the Hill’s three-body problem with solar radiation pressure. Adv. Astronaut. Sci. 136, 285–300 (2010)
Markellos, V.V., Roy, A.E., Velgakis, M.J., Kanavos, S.S.: A photogravitational Hill problem and radiation effects on Hill stability of orbits. Astrophys. Space Sci. 271(3), 293–301 (2000)
McInnes, C.R.: Solar Sailing: Technology. Dynamics and Mission Applications. Springer-Praxis, Chichester (1999)
Meyer, K.R., Hall, G.R.: Introduction to Hamiltonian Dynamical Systems and the N-Body Problem. Springer, New York (1992)
Morrow, E., Scheeres, D.J., Lubin, D.: Solar sail orbit operations at asteroids. J. Spacecr. Rockets 38(2), 279–286 (2001)
Morrow, E., Scheeres, D.J., Lubin. D.: Solar sail orbit operations at asteroids: exploring the coupled effect of an imperfectly reflecting sail and a nonspherical asteroid. In: AIAA/AAS Astrodynamics Specialist Conference and Exhibit, August (2002)
Papadakis, K.E.: The planar photogravitational Hill problem. Internat. J. Bifurc. Chaos Appl. Sci. Eng. 16(06), 1809–1821 (2006)
Scheeres, D.J.: Orbital Motion in Strongly Perturbed Environments: Applications to Asteroid. Comet and Planetary Satellite Orbiters. Springer, Berlin (2012)
Siegel, C.L., Moser, J.K.: Lectures on Celestial Mechanics. Grundlehren Math, vol. 187. Wiss. Springer, New York (1971)
Sijbrand, J.: Properties of center manifolds. Trans. Am. Math. Soc. 289(2), 431–469 (1985)
Simó, C.: Estabilitat de sistemes Hamiltonians. Mem. Real Acad. Cienc. Artes Barcelona 48(7), 303–348 (1989)
Simó, C.: On the analytical and numerical approximation of invariant manifolds. In: Benest, D., Froeschlé, C. (eds.) Modern Methods in Celestial Mechanics. Frontières, Reprinted at. pp. 285–330 (1990) Ed http://www.maia.ub.es/dsg/2004/index.html
Stoer, J., Bulirsch, R.: Introduction to Numerical Analysis, volume 12 of Texts in Applied Mathematics, 3rd edn. Springer, New York (2002)
Szebehely, V.: Theory of Orbits. Academic Press, Cambridge (1967)
Vanderbauwhede, A.: Centre manifolds, normal forms and elementary bifurcations. In: Dynamics reported, Vol. 2, volume 2 of Dynam. Report. Ser. Dynam. Systems Appl. Wiley, Chichester, pp. 89–169 (1989)
Villac, B., Ribalta, G., Farrés, A., Jorba, À., Mondelo, J-M.: Using Solar arrays for orbital control near small bodies. trade-offs characterization. In: AIAA/AAS Astrodynamics Specialist Conference, Minneapolis, Minnesota (2012)
Yárnoz, D.G., Scheeres, D.J., McInnes, C.R.: On the a and and g families of orbits in the Hill problem with solar radiation pressure and their application to asteroid orbiters. Celest. Mech. 121(4), 365–384 (2015)
Acknowledgements
The research of A.F. and A.J. has been supported by the Spanish Grant MTM2015-67724-P (funded by MINECO/FEDER, UE) and the Catalan Grant 2014 SGR 1145. The research of J.M.M. has been supported by the Spanish Grants MTM2013-41168-P, MTM2014-52209-C2-1-P, MTM2016-80117-P.
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Farrés, A., Jorba, À. & Mondelo, JM. Numerical study of the geometry of the phase space of the Augmented Hill Three-Body problem. Celest Mech Dyn Astr 129, 25–55 (2017). https://doi.org/10.1007/s10569-017-9762-z
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DOI: https://doi.org/10.1007/s10569-017-9762-z