R. D. Arzelier, C. Louembet, and A. Théron, Etude bibliographique sur le problème du rendezvous, vol.93, 2008.

R. D. Arzelier, C. Louembet, and A. Théron, Deux algorithmes pour le problème du rendezvous impulsionnel, vol.87, 2009.

R. D. Arzelier, N. Jozefowiez, P. Lopez, and C. Louembet, Etude bibliographique sur la programmation linéraire, 2011.

R. D. Arzelier, N. Jozefowiez, P. Lopez, and C. Louembet, Evaluation des performances des solveurs de programmation linéaire sur le problème du rendez-vous orbital impulsionnel, 2011.

R. D. Arzelier and C. Louembet, Algorithmes de guidage en rendez-vous sous contraintes d'incertitudes et d'erreurs par programmation convexe robuste, Rapport LAAS-CNRS N ? 12359, vol.126, 2012.

R. D. Arzelier, C. Louembet, and A. Rondepierre, Algorithme indirect mixte pour le problème du rendezvous, Rapport LAAS-CNRS N ? 2433

, Convention CNES N ? 71372/00, 104 pages, 2012.

R. D. Arzelier, C. Louembet, P. Arantes-gilz, and L. S. Urbina, Méthode de survol pour le rendez-vous orbital, Rapport LAAS-CNRS N ? 15409, vol.104, 2015.

R. C. Louembet and F. Gouaisbaut, Optimal guidance and control for flexible and maneuvring spacecraft, Rapport LAAS-CNRS N ? 16247, vol.4500543955, 2016.

. , Représentation sous forme d'espace d'état

. , 2 La matrice de transition d'état

. .. , 130 D.2.1 Théorème de représentation de Riesz et établissement du problème dual, p.131

D. , 4 Reconstruction de la fonction mesure et la commande

, Alternatives à l'approche déterministe pour l'optimisation robuste, p.142

. , Approche par satisfaction des contraintes en probabilité

. , Modéliser des ensembles d'incertitudes

P. R. Arantes-gilz, M. M. Joldes, C. Louembet, and F. Camps, Model predictive control for rendezvous hovering phases based on a novel description of constrained trajectories, 20th IFAC World Congress, 2017.
URL : https://hal.archives-ouvertes.fr/hal-01484764

P. R. Arantes-gilz and C. Louembet, Predictive control algorithm for spacecraft rendezvous hovering phases, European Control Conference (ECC), 2015.
URL : https://hal.archives-ouvertes.fr/hal-01078506

P. R. Arantes-gilz, A non-linear simulator written in C for orbital spacecraft rendezvous applications, 2016.
URL : https://hal.archives-ouvertes.fr/hal-01410075

Y. Ariba, D. Arzelier, and L. Urbina, A new glideslope guidance algorithm for minimum-fuel fixedtime elliptic rendezvous using semidefinite programming, 20th IFAC World Congress, pp.9-14, 2017.
URL : https://hal.archives-ouvertes.fr/hal-01887913

Y. Ariba, D. Arzelier, L. S. Urbina, and C. Louembet, V-bar and r-bar glideslope guidance algorithms for fixed-time rendezvous : A linear programming approach, vol.49, pp.385-390, 2016.
URL : https://hal.archives-ouvertes.fr/hal-01358188

D. Arzelier, F. Bréhard, N. Deak, M. Joldes, C. Louembet et al., Linearized impulsive fixed-time fuel-optimal space rendezvous : A new numerical approach, 20th IFAC Symposium on Automatic Control in Aerospace, vol.49, pp.373-378, 2016.
URL : https://hal.archives-ouvertes.fr/hal-01275427

D. Arzelier, M. Kara-zaitri, C. Louembet, and A. Delibasi, Using polynomial optimization to solve the fuel-optimal linear impulsive rendezvous problem, Journal of Guidance, Control, and Dynamics, vol.34, issue.5, pp.1567-1576, 2011.

D. Arzelier, C. Louembet, A. Rondepierre, and M. Kara-zaitri, A new mixed iterative algorithm to solve the fuel-optimal linear impulsive rendezvous problem, Journal of Optimization Theory and Applications, vol.159, issue.1, pp.210-230, 2013.
URL : https://hal.archives-ouvertes.fr/hal-00687499

D. Arzelier, C. Louembet, and S. Urbina, Modélisation unifiée 6 degrés de liberté des problèmes de guidage/contrôle pour les opération spatiales de proximité. Rapport R&T n ? 15064, 2015.

U. Ascher, R. Mattheij, and R. R. , Numerical solution of boundary value problems in ordinary differential equations, 1988.

J. Aubin, Impulse differential equations and hybrid systems : A viability approach, Lecture Notes, 2000.

D. Bainov and P. Simeonov, Impulsive differential equations : periodic solutions and applications, Pitman Monographs and Surveys in Pure and Applied Mathematics, vol.66, 1993.

R. H. Battin, An introduction to the mathematics and methods of astrodynamics, 1999.

A. Ben-tal and A. Nemirovski, Robust solutions to uncertain linear programs, 1995.

A. Ben-tal and A. Nemirovski, Robust convex optimization, Mathematics of Operations Research, vol.23, issue.4, pp.769-805, 1998.

A. Ben-tal and A. Nemirovski, Robust solutions of uncertain linear programs, Operations Research Letters, vol.25, issue.1, pp.1-13, 1999.

A. Ben-tal, L. E. Ghaoui, and A. Nemirovski, Robust Optimization, 2009.

A. Ben-tal and A. Nemirovski, Robust solutions of linear programming problems contaminated with uncertain data, Mathematical Programming, vol.88, issue.3, pp.411-424, 2000.

J. C. Berges, P. Cayeux, A. Gaudel-vacaresse, and B. Meyssignac, Cnes approaching guidance experiment on ffiord, 20th. International Symposium on Space Flight Dynamics, 2007.

D. Bertsekas and S. Schreve, Stochastic Optimal Control : The Discrete-Time Case, 1978.

D. Bertsimas and J. Tsitsiklis, Introduction to linear optimization, 1997.

J. T. Betts, Optimal three-burn orbital transfer, Journal of Guidance, Control and Dynamics, vol.15, pp.861-864, 1977.

J. T. Betts, Survey of numerical methods for trajectory optimization, Journal of Guidance, Control and Dynamics, vol.21, issue.2, pp.193-207, 1998.

J. T. Betts, Practical methods for optimal control using nonlinear programming, Advances in Design and Control. SIAM, 2001.

P. Blanc-paques, E. Gogibus, C. Louembet, and M. Kara-zaitri, Evaluation of autonomous guidance techniques for rendezvous, 4 th International Conference on Astrodynamics Tools and Techniques, pp.3-6, 2010.

H. G. Bock and K. J. Plitt, A multiple shooting algorithm for direct solution of optimal control problems, IFAC 9 th World congress, 1984.

S. Boyd, L. Xiao, and A. Mutapcic, Subgradient methods. Lecture notes of EE392o, 2003.

L. Breger and J. How, Safe trajectories for autonomous rendezvous of spacecraft, Journal of Guidance, Control and Dynamics, vol.31, issue.5, pp.1478-1489, 2008.

L. Breger, G. Inalhan, M. Tillerson, and J. How, Modern Astrodynamics, chapter Coperative spacecraft formation flying : model predictive control with open and closed loop robustness, 2006.

M. Brentari, D. Arzelier, C. Louembet, L. S. Urbina, and L. Zaccarian, A hybrid control framework for impulsive control of satellite rendezvous, 2016.
URL : https://hal.archives-ouvertes.fr/hal-01741201

M. Brentari, S. Urbina, D. Arzelier, C. Louembet, and L. Zaccarian, A hybrid control framework for impulsive control of satellite rendezvous, 2017.
URL : https://hal.archives-ouvertes.fr/hal-01741201

C. Briat and A. Seuret, Convex dwell-time characterizations for uncertain linear impulsive systems, IEEE Transactions on Automatic Control, vol.57, issue.12, pp.3241-3246, 2012.
URL : https://hal.archives-ouvertes.fr/hal-00724546

R. A. Broucke, Solution of the elliptic rendezvous problem with the time as independent variable, Journal of Guidance, Control, and Dynamics, vol.26, issue.4, pp.615-621, 2003.

R. G. Brusch, Constrained impulsive trajectory optimization for orbit-to-orbit, Journal of Guidance, Control and Dynamics, vol.2, pp.204-212, 1979.

T. E. Carter, Optimal impulsive space trajectories based on linear equations, Journal of Optimization Theory and Applications, vol.70, issue.2, 1991.

T. E. Carter, State transition matrices for terminal rendez vous studies : Brief survey and new examples, Journal of Guidance, Control and Dynamics, vol.21, issue.1, pp.148-155, 1998.

T. E. Carter, Necessary and sufficient conditions for optimal impulsive rendezvous with linear equations of motion, Dynamics and Control, vol.10, pp.219-227, 2000.

T. E. Carter and S. A. Alvarez, Quadratic-based computation of four-imulse optimal rendezvous near circular orbit, Journal of Guidance, Control and Dynamics, vol.23, issue.1, pp.109-1117, 2000.

T. E. Carter and J. Brient, Fuel-optimal rendezvous for linearized equations of motion, Journal of Guidance, Control, and Dynamics, vol.15, issue.6, pp.1411-1416, 1992.

T. E. Carter and J. Brient, Linearized impulsive rendezvous problem, Journal of Optimization Theory and Applications, vol.86, issue.3, 1995.

S. Chevillard, J. Harrison, M. Jolde?, and C. Lauter, Efficient and accurate computation of upper bounds of approximation errors, Theoretical Computer Science, vol.412, issue.16, pp.1523-1543, 2011.
URL : https://hal.archives-ouvertes.fr/ensl-00445343

M. Claeys, D. Arzelier, D. Henrion, and J. Lasserre, Measures and LMI for impulsive optimal control with applications to space rendezvous problems, 2012.
URL : https://hal.archives-ouvertes.fr/hal-00633138

M. Claeys, D. Arzelier, D. Henrion, and J. Lasserre, Moment LMI approach to ltv impulsive control, 52nd IEEE Conference on Decision and Control, 2013.
URL : https://hal.archives-ouvertes.fr/hal-00797951

W. H. Clohessy, Terminal guidance system for satellite rendezvous, Journal of the Aerospace Sciences, vol.27, issue.9, pp.653-658, 1960.

S. Dashkovskiy, M. Kosmykov, A. Mironchenko, and L. Naujok, Stability of interconnected impulsive systems with and without time delays, using Lyapunov methods, Nonlinear Analysis : Hybrid Systems, vol.6, issue.3, pp.899-915, 2012.

G. Deaconu, On the trajectory design, guidance and control for spacecraft rendezvous and proximity operations. Theses, 2013.
URL : https://hal.archives-ouvertes.fr/tel-00919883

G. Deaconu, C. Louembet, and A. Théron, Constrained periodic spacecraft relative motion using non-negative polynomials, American Control Conference (ACC 2012), pp.6715-6720, 2012.
URL : https://hal.archives-ouvertes.fr/hal-00639905

G. Deaconu, C. Louembet, and A. Théron, Sécurisation passive du rendez-vous orbital par des polynômes non négatifs, Conférence Internationale Francophone d'Automatique (CIFA2012), pp.811-816, 2012.

G. Deaconu, C. Louembet, and A. Theron, A two-impulse method for stabilizing the spacecraft relative motion with respect to a periodic trajectory, IEEE 51st IEEE Conference on Decision and Control (CDC), 2012.
URL : https://hal.archives-ouvertes.fr/hal-01872905

G. Deaconu, C. Louembet, and A. Theron, Minimizing the effects of navigation uncertainties on the spacecraft rendezvous precision, Journal of Guidance, Control, and Dynamics, vol.37, issue.2, pp.695-700, 2014.
URL : https://hal.archives-ouvertes.fr/hal-01078527

G. Deaconu, C. Louembet, and A. Theron, Designing continuously constrained spacecraft relative trajectories for proximity operations, Journal of Guidance, Control, and Dynamics, vol.38, issue.7, pp.1208-1217, 2015.
URL : https://hal.archives-ouvertes.fr/hal-01078528

E. D. Dickmanns and H. K. Well, Approximate solution of optimal control problems using thirdorder hermite polynomial functions, Proceedings of the 6 th Technical Conference on Optimization Techniques, 1975.

L. E. Ghaoui, F. Oustry, and H. Lebret, Robust solutions to uncertain semidefinite programs, SIAM J. Optimization, vol.9, issue.1, pp.33-52, 1998.

G. Elnagar, M. Kazemi, and M. Razzaghi, The pseudospectral legendre method for discretizing optimal control problems, IEEE Transactions on Automatic Control, vol.40, issue.10, 1995.

P. Enright and B. Conway, Optimal finite-thrust spacecraft trajectories using collocation and nonlinear programming, Journal of Guidance, Control and Dynamics, vol.14, issue.5, pp.981-985, 1991.

P. Enright and B. Conway, Discrete approximations to optimal trajectories using direct transcription and non linear programming, Journal of Guidance, Control and Dynamics, vol.15, issue.4, pp.994-1002, 1992.

W. Fehse, Automated rendezvous and docking of spacecraft, vol.16, 2003.

M. Fiacchini, S. Tarbouriech, and C. Prieur, Exponential Stability for Hybrid Systems with Saturations, Hybrid systems with constraints, pp.179-212, 2013.
URL : https://hal.archives-ouvertes.fr/hal-00833678

S. L. Fraga and F. L. Pereira, Hamilton-jacobi-bellman equation and feedback synthesis for impulsive control, IEEE Transactions on Automatic Control, vol.57, issue.1, pp.244-249, 2012.

J. Garrison, T. G. Gardner, and P. Axelrad, Relative motion in highly elliptical orbits, Spaceflight mechanics, 1995.

C. Gazzino, D. Arzelier, D. Losa, C. Louembet, C. Pittet et al., Optimal control for minimum-fuel geostationary station keeping of satellites equipped with electric propulsion. IFACPapersOnLine, 20th IFAC Symposium on Automatic Control in Aerospace (ACA), vol.49, pp.21-25, 2016.
URL : https://hal.archives-ouvertes.fr/hal-01275305

C. Gazzino, C. Louembet, D. Arzelier, N. Jozefowiez, D. Losa et al., Integer programming for optimal control of geostationary station keeping of low-thrust satellites, 20th IFAC World Congress, 2017.
URL : https://hal.archives-ouvertes.fr/hal-01416694

J. Gerstmayr, A. Dorninger, R. Eder, P. Gruber, D. Reischl et al., Hotint : A script language based framework for the simulation of multibody dynamics systems, ASME 2013 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, pp.7-10, 2013.

R. Goebel, R. G. Sanfelice, and A. R. Teel, Hybrid Dynamical Systems : modeling, stability, and robustness, 2012.

P. J. Goulart, E. C. Kerrigan, and J. M. Maciejowski, Optimization over state feedback policies for robust control with constraints, Automatica, vol.42, issue.4, pp.523-533, 2006.

W. M. Haddad, V. Chellaboina, and S. G. Nersesov, Impulsive and hybrid dynamical systems, Princeton Series on Applied Mathematics, 2006.

C. Hargraves and S. Paris, Direct trajectory optimization using nonlinear programming and collocation, AIAA Journal of Guidance and Control, vol.10, 1987.

D. Henrion, J. B. Lasserre, and L. , Gloptipoly 3 : moments, optimization and semidefinite programming, Optimization Methods and Software, vol.24, issue.4-5, pp.761-779, 2009.
URL : https://hal.archives-ouvertes.fr/hal-00172442

G. W. Hill, Researches in the lunar theory, American Journal of Mathematics, vol.1, issue.1, pp.5-26, 1878.

B. Houska, H. J. Ferreau, and M. Diehl, ACADO Toolkit-An Open Source Framework for Automatic Control and Dynamic Optimization, Optimal Control Applications and Methods, vol.32, issue.3, pp.298-312, 2011.

J. P. How and M. Tillerson, Analysis of the impact of sensor noise on formation flying control, vol.5, pp.3986-3991, 2001.

D. G. Hull, Conversion of optimal control problems into parameter optimization problems, Journal of Guidance, Control and Dynamics, vol.20, issue.1, 1997.

D. G. Hull and J. L. Speyer, Optimal reentry and plane-change trajectories, Journal of Astronautical Sciences, vol.30, issue.2, pp.117-130, 1982.

L. Jaulin, M. Kieffer, A. E. Didrit, and O. Ben-tal, Applied Interval Analysis with Examples in Parameter and State Estimation, Robust Control and Robotics, 2001.
URL : https://hal.archives-ouvertes.fr/hal-00845131

D. Jezewski, Primer vector theory and applications. Note technique TR R-454, NASA, 1975.

D. Jezewski, Primer vector theory applied to the linear relative-motion equations, Optimal Control Applications and Methods, vol.1, pp.387-401, 1980.

M. Joldes, Rigorous Polynomial Approximations and Applications. Theses, 2011.
URL : https://hal.archives-ouvertes.fr/tel-00657843

T. Kailath, Linear systems, vol.156, 1980.

M. Kara-zaitri, D. Arzelier, A. Delibasi, and C. Louembet, Polynomial optimization for the solution of fuel-optimal impulsive rendezvous using primer vector theory, 49th IEEE Conference on Decision and Control (CDC), 2010.

M. K. Zaitri, D. Arzelier, and C. Louembet, Mixed iterative algorithm for solving optimal impulsive time-fixed rendezvous problem, AIAA Guidance, Navigation, and Control Conference, 2010.

S. Kerambrun, Evaluation des performances des algorithmes de guidage, Note technique N.T. 5 GNC-T.TCN.738703.ASTRv2, Astrium SAS, 2009.

S. Kerambrun, Evaluation des performances dez algorithmes de guidage, EADS Astrium, 2009.

L. Kos, T. Polsgrovet, R. Hopkins, D. Thomas, and J. Sims, Overview of the development for a suite of low-thrust trajectory analysis tools, AIAA/AAS Astrodynamics Specialist Conference and Exhibit, 2006.

P. Labourdette, E. Julien, F. Chemama, and D. Carbonne, ATV Jules Verne mission maneuver plan, 21 st International Symposium on space flight dynamics, 2008.

W. Langson, I. Chryssochoos, S. V. Rakovi?, and D. Q. Mayne, Robust model predictive control using tubes, Automatica, vol.40, issue.1, pp.125-133, 2004.

R. Larsson, S. Berge, P. Bodin, and U. Jönsson, Fuel efficient relative orbit control stategies for formation flying and rendezvous within prisma, 29 th Annual AAs Guidance and Control Conference, 2006.

R. Larsson, J. Mueller, S. Thomas, B. Jakobsson, and P. Bodin, Orbit constellation safety on the prisma in-orbit formation flying test bed, 3rd Int. Symp. on Formation Flying, Missions and Technologies, 2008.

J. B. Lasserre, A semidefinite programming approach to the generalized problem of moments, Mathematical Programming, vol.112, pp.65-92, 2008.

J. B. Lasserre, Moments, positive polynomials and their applications, World Scientific, vol.1, 2009.

K. Laßwitz, Auf zwei Planeten : Romanin zwei Büchern, 1897.

D. F. Lawden, Optimal trajectories for space navigation, Butterworths, 1963.

D. F. Lawden, Optimal transfer via tangential ellipses, Journal of the British Interplanetary Society, vol.11, issue.6, pp.278-289, 1952.

D. F. Lawden, Optimal transfer between circular orbits about two planets, Astronautica Acta, vol.1, pp.89-99, 1955.

D. F. Lawden, Transfer between circular orbits, Jet Propulsion, vol.26, issue.7, pp.555-558, 1956.

D. F. Lawden, Impulsive transfer between ellptical orbits, Optimization techniques with applications to aerospace systems, pp.323-350, 1962.

J. Lévine and D. V. Nguyen, Flat output characterization for linear systems using polynomial matrices, Systems & Control Letters, vol.48, issue.1, pp.69-75, 2003.

A. S. Lewis and M. L. Overton, Nonsmooth optimization via quasi-Newton methods, Mathematical Programming, vol.141, issue.1-2, pp.135-163, 2012.
DOI : 10.1007/s10107-012-0514-2
URL : http://www.cs.nyu.edu/faculty/overton/papers/pdffiles/nsoquasi.pdf

P. M. Lion and M. Handelsman, Primer vector on fixed-time impulsive trajectories, AIAA Journal, vol.6, issue.1, p.127, 1968.

J. S. Llorente, A. Agenjo, C. Carrascosa, C. De-negueruela, A. Mestreau-garreau et al., Proba-3 : Precise formation flying demonstration mission, Acta Astronautica, vol.82, issue.1, pp.38-46, 2013.
DOI : 10.1016/j.actaastro.2012.05.029

C. Louembet, D. Arzelier, and G. Deaconu, Robust rendezvous planning under maneuver execution errors, Journal of Guidance, Control, and Dynamics, vol.38, issue.1, pp.76-93, 2015.
DOI : 10.2514/1.g000391
URL : https://hal.archives-ouvertes.fr/hal-01078508

C. Louembet, D. Arzelier, G. Deaconu, and P. Blanc-paques, Robust rendezvous planning under navigation and maneuvering errors, 8th ESA International Conference on Guidance, Navigation and Control System, 2011.
DOI : 10.2514/1.g000391
URL : https://hal.archives-ouvertes.fr/hal-01078508/file/version_final.pdf

C. Louembet, F. Cazaurang, A. Zolghadri, C. Charbonnel, and . Pittet, Path planning for satellite slew manoeuvres : a combined flatness and collocation-based approach, IET control theory & applications, vol.3, issue.4, pp.481-491, 2009.
DOI : 10.1049/iet-cta.2008.0054

C. Louembet and F. Gouaisbaut, Optimal guidance and control for flexible and maneuvring spacecraft, Project ESA ITI. Contract Airbus defence & space #4500543955, 2016.

D. G. Luenberger, Optimization by vector space methods, 1969.

Y. Luo, Y. Tang, and . Lei, Optimal multi-objective linearized impulsive rendezvous, Journal of Guidance, Control, and Dynamics, vol.30, issue.2, pp.383-389, 2007.
DOI : 10.2514/1.21433

D. Q. Mayne, E. C. Kerrigan, and P. Falugi, Robust model predictive control : advantages and disadvantages of tube-based methods, IFAC Proceedings Volumes, vol.44, pp.191-196, 2011.
DOI : 10.3182/20110828-6-it-1002.01893

R. G. Melton, Time-explicit representation of relative motion between elliptical orbits, Journal of Guidance, Control, and Dynamics, vol.23, issue.4, pp.604-610, 2000.

R. Moore, Interval Arithmetic, 1966.

J. Mueller and R. Larsson, Collision avoidance maneuver planning with robust optimization, th International ESA Conference on Guidance, Navigation & Control Systems, pp.2-5, 2008.
DOI : 10.2514/6.2009-2051

P. Naghshtabrizi, J. P. Hespanha, and A. R. Teel, Exponential stability of impulsive systems with application to uncertain sampled-data systems, Systems & Control Letters, vol.57, issue.5, pp.378-385, 2008.

D. Nesic, A. R. Teel, and L. Zaccarian, Stability and performance of SISO control systems with first-order reset elements, IEEE Transactions on Automatic Control, vol.56, issue.11, pp.2567-2582, 2011.

Y. Nesterov, Squared Functional Systems and Optimization Problems, pp.405-440, 2000.
DOI : 10.1007/978-1-4757-3216-0_17

L. W. Neustadt, Optimization, a moment problem, and nonlinear programming, SIAM Journal of Control, vol.2, issue.1, pp.33-53, 1964.
DOI : 10.1137/0302004

F. Nilsson, P. Bodin, C. Chasset, B. Jakobsson, R. Larsson et al., Autonomous rendezvous experiments on the prisma in-orbit formation flying test bed, 3rd Int. Symp. on Formation Flying, Missions and Technologies, 2008.

S. W. Paris, J. P. Riehl, and W. K. Sjauw, Enhanced procedures for direct trajectory optimization using nonlinear programming and implicit integration, AIAA/AAS Astrodynamics Specialist Conference and Exhibit, 2006.

F. L. Pereira, G. N. Silva, and V. Oliveira, Invariance for impulsive control systems. Automation and Remote Control, vol.69, pp.788-800, 2008.

F. L. Pereira, F. A. Fontes, A. P. Aguiar, J. B. De, and . Sousa, An Optimization-Based Framework for Impulsive Control Systems, pp.277-300, 2015.

F. L. Pereira and G. N. Silva, Stability for impulsive control systems, Dynamical Systems, vol.17, issue.4, pp.421-434, 2002.

N. Petit, M. Milam, and R. Murray, Inversion based constrained trajectory optimization, 5th IFAC Symposium on Nonlinear Control Systems, vol.34, pp.4-6, 2001.

N. Petit, R. Milam, M. , and M. , Constrained trajectory generation for micro-satellite formation flying, AIAA Guidance, Navigation, and Control Conference and Exhibit, p.4030, 2001.

J. E. Prussing, Optimal multiple-impulse orbital rendezvous, 1967.

J. E. Prussing, Optimal four-impulse fixed-time rendezvous in the vicinity of a circular orbit, AIAA Journal, vol.7, issue.5, pp.928-935, 1969.

J. E. Prussing, Optimal two-and three-impulse fixed-time rendezvous in the vicinity of a circular orbit, Journal of Spacecraft and Rockets, vol.40, issue.6, pp.952-959, 2003.

R. Reemtsen and S. Görner, Numerical Methods for Semi-Infinite Programming : A Survey, pp.195-275, 1998.

A. Richards, . Schouwenaars, E. How, and . Feron, Spacecraft trajectory planning with avoidance constraints using mixed-integer linear programming, Journal of Guidance, Control, and Dynamics, vol.25, issue.4, pp.755-764, 2002.

J. A. Richards, Analysis of periodically time-varying systems, 2012.

A. Robertson, J. Inalhan, and . How, Spacecraft formation flying control design for the orion mission, American Control Conference, vol.6, pp.2-4, 1999.

A. J. Roenneke, C. Jänsch, and A. Markl, Advanced Launch and reentry Trajectory Optimization Software (ALTOS) documentation, European Space Science and Technology Center (ESA), 1995.

L. Ros, A. Sabater, and F. Thomas, An ellipsoidal calculus based on propagation and fusion. Systems, Man, and Cybernetics, Part B : Cybernetics, IEEE Transactions on, vol.32, issue.4, pp.430-442, 2002.

H. H. Rosenbrock, Multivariable and State-Space Theory, p.130, 1970.

A. L. Soyster, Convex programming with set-inclusive constraints and application to inexact linear programming, Operations Research, vol.21, pp.1154-1157, 1973.

R. G. Stern and J. E. Potter, Optimization of midcourse velocity corrections, First IFAC Symposium Peaceful Uses of Automatic Control in Outer Space, pp.70-83, 1966.

, Bocop : an open source toolbox for optimal control, Inria Saclay Team Commands, 2016.

M. Tillerson, Coordination and control of multiple spacecraft using convex optimization techniques, 2002.

M. Tillerson, G. Inalhan, and J. P. How, Co-ordination and control of distributed spacecraft systems using convex optimization techniques, International Journal of Robust and Nonlinear Control, vol.12, issue.23, pp.207-242, 2002.

E. Trélat, Contrôle optimal : théorie & applications. Vuibert, 2005.

J. Tschauner, The elliptic orbit rendezvous, AIAA 4th Aerospace Sciences Meeting, 1966.

K. E. Tsiolkovsky, Exploration of the universe with reaction machines, The Science Review, vol.5, 1903.

J. Verschelde, Algorithm 795 : Phcpack : A general-purpose solver for polynomial systems by homotopy continuation, ACM Transactions on Mathematical Software (TOMS), vol.25, issue.2, pp.251-276, 1999.

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, issue.1, 2002.