Y. Kawakatsu, K. Kuramoto, N. Ogawa, H. Ikeda, Y. Mimasu et al., Mission concept of Martian Moons eXploration (MMX), 2017.

S. Murchie, P. Thomas, A. Rivkin, and N. Chabot, Phobos and Deimos, Asteroid IV, pp.451-467, 2015.

H. Ikeda, S. Mitani, Y. Mimasu, G. Ono, K. Nigo et al., International Symposium of Space Flight Dynamics in Matsuyama, 2017.

M. Lara, Nonlinear librations of distant retrograde orbits: a perturbative approach-the Hill problem case, Nonlinear Dynamics, 2018.

A. I. Kogan, Distant satellite orbits in the restricted circular three-body problem, vol.26, pp.705-710, 1989.

K. Yamanaka and F. Ankersen, New state transition matrix for relative motion on an arbitrary elliptical orbit, Journal of Guidance, Control, and Dynamics, vol.25, pp.60-66, 2002.

A. Jorba, Orbital dynamics of a solar sail near L1 and L2 in the elliptic Hill problem, 2012.

G. Voyatzis, I. Gkolias, and H. Varvoglis, The dynamics of the elliptic Hill problem: Periodic orbits and stability regions, Celestial Mechanics and Dynamical Astronomy, vol.113, issue.1, pp.125-139, 2012.

R. A. Broucke, Stability of periodic orbits in the elliptic, restricted three-body problem, AIAA Journal, vol.7, issue.6, pp.1003-1009, 1969.

D. J. Scheeres, S. Van-wal, Z. P. Olikara, and N. Baresi, The dynamical environment for the exploration of phobos, the 28th International Symposium on Space Flight Dynamics, 2017.

G. Gómez and J. Mondelo, The dynamics around the collinear equilibrium points of the RTBP, Physica D: Nonlinear Phenomena, vol.157, issue.4, pp.283-321, 2001.

Z. P. Olikara and D. J. Scheeres, Numerical method for computing quasi-periodic orbits and their stability in the restricted three-body problem, AAS Astrodynamics Specialist Conference, 2012.

N. Baresi, Z. Olikara, and D. J. Scheeres, Fully numerical methods for continuing families of quasi-periodic invariant tori in astrodynamics, The Journal of the Astronautical Sciences, vol.65, issue.2, pp.157-182, 2018.

Z. P. Olikara, Computation of Quasi-periodic Tori and Heteroclinic Connections in Astrodynamics using Collocation Techniques, 2016.

N. Baresi, Spacecraft Formation Flight on Quasi-periodic Invariant Tori, 2017.

N. Baresi and D. J. Scheeres, Quasi-periodic invariant tori of time-periodic dynamical systems: Applications to small body exploration, 2016.

A. J. Sinclair, R. E. Sherrill, and A. T. Lovell, Geometric interpretation of the tschaunerhempel solutions for satellite relative motion, Advances in Space Research, vol.55, issue.9, pp.2268-2279, 2015.

F. Cabral, On the stability of quasi-satellite orbits in the Elliptic Restricted Three-Body Problem, 2011.

M. Abramowitz, Handbook of Mathematical Functions, 1974.

N. Baresi, L. Dell'elce, J. Cardoso, Y. Santos, and . Kawakatsu, On the long-term evolution of mid-altitude quasi-satellite orbits around phobos, Nonlinear Dynamics

M. Lara, J. Palacian, and R. P. Russell, Mission design through averaging of perturbed Keplerian systems: the paradigm of an Enceladus orbiter, Celestial Mechanics and Dynamical Astronomy, vol.108, pp.1-22, 2010.
URL : https://hal.archives-ouvertes.fr/hal-00568375

J. Cardoso, S. Santos, D. J. Ferrer, and . Scheeres, Study of the roto-translational motion using intermediaries: Numerical experiments, Celestial Mechanics and Dynamical Astronomy, 2018.

T. Ely, Transforming mean and osculating elements using numerical methods, paper AAS 10-139 presented at the 20th AAS/AIAA Space Flight Mechanics Meeting, 2010.
DOI : 10.1007/s40295-015-0036-2

H. Schaub, S. R. Vadali, J. L. Junkins, and K. T. Alfriend, J2 invariant relative orbits for spacecraft formations, Journal of the Astronautical Science, vol.48, issue.1, pp.69-87, 2000.